FINAL PROGRAM

48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit (JPC) www.aiaa.org/jpc2012

30 July–1 August 2012 Hyatt Regency Atlanta Atlanta, Georgia

10th International Energy Conversion Engineering Conference (IECEC) www.iecec.org

FINAL PROGRAM

Lead Government Sponsor

Lead Industry Sponsor

Awards Luncheon Sponsor

General Conference Sponsors USB Memory Stick Sponsor

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47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Synopsis AIAA, ASME, SAE, ASEE, and their industry partners proudly welcome you to Atlanta, Georgia, for the 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit (JPC), 30 July–1 August 2012. The design of our next-generation flight and space systems will be dependent more than ever on innovative technologies providing high-performance, increasingly efficient, sustainable, reliable, and affordable propulsion systems. Our ability to design, test, and fly new aircraft and spacecraft propulsion technologies will have farth reaching impacts on the revolutionary roles these complex systems play in our everyday lives.

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The objective of JPC 2012 is to identify and highlight how innovative aerospace propulsion technologies powering both new and evolving systems are being designed, tested, and flown. Flight applications include next-generation commercial aircraft, regional and business jets, military applications, supersonic/hypersonic high-speed propulsion applications, commercial and government-sponsored launch systems, and orbital insertion, satellite, and interstellar propulsion. Special panel sessions focus on advanced system applications that can be used to showcase propulsion systems and components, and the technologies that enable them.

48th AIAA/ASME/ SAE/ASEE Joint Propulsion Conference and Exhibit CONFERENCE THEME: Future Propulsion: Innovative, Affordable, Sustainable

JPC Organizing Committee Executive Chair (Government)

General Chair (Government)

Exhibits Chair

Executive Chair (Industry)

Technical Chair

ASME Technical Program Chair

Deputy Technical Chair

SAE Technical Program Chair

Jeff Morehouse Lockheed Martin Corporation

ASEE Technical Program Chair

Robert Lightfoot Acting Associate Administrator, NASA Bart Olson Vice President, Business Development ATK Missile Products Group

General Chair (Industry)

Gary Flinchbaugh VP Programs ATK Propulsion and Controls

Dale Thomas NASA Marshall Space Center

David McGrath ATK Propulsion and Controls Gerard E. Welch NASA Glenn Research Center

Academic Chair

Geraldine Kimball Pratt & Whitney Rocketdyne John W. Robinson The Boeing Company (Retired)

Ramon Chase Booze Allen Hamilton (Retired) Robert A. Frederick Jr. University of Alabama in Huntsville

Vigor Yang Georgia Institute of Technology

Topic Area Organizers Advanced Propulsion Concepts for Future Flight John W. Robinson The Boeing Company (Retired)

Air-Breathing Propulsion Systems Integration Michelle L. McMillan SynGenics Corporation

Gas Turbine Engines

Gerard E. Welch NASA Glenn Research Center

High Speed Air-Breathing Propulsion

Venkat Tangirala General Electric Global Research Center – Combustion Technologies

Hypersonic and Combined Cycle Propulsion Tim O’Brien Aerojet

Electric Propulsion

Propellants and Combustion

Emerging Commercial Space Propulsion

Propulsion Education

Eric Pencil NASA Glenn Research Center Bruce Pittman NASA Space Portal, NASA Ames Research Center

Energetic Components and Systems Steven F. Son Purdue University

Hybrid Rocket Propulsion

Madhan Bala Space Propulsion Group, Inc.

Liquid Rocket Propulsion

Ivett A. Leyva Air Force Research Laboratory

Nuclear and Future Flight Propulsion Greg Meholic The Aerospace Corporation

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Christopher Brophy Naval Postgraduate School

Robert A. Frederick Jr. University of Alabama in Huntsville

Public Policy

Carol Cash Carol Cash & Associates

Solid Rocket Propulsion

Mark T. Langhenry Raytheon Missile Systems

Space Transportation and Future Generation Space Transportation Sessions Leo Daniel Massachusetts Institute of Technology

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10th ConversionEngineering EngineeringConference Conference 10th International International Engergy Energy Conversion

Synopsis The 10th International Energy Conversion Engineering Conference (IECEC) provides a forum to present and discuss engineering aspects of energy conversion technology, advanced energy and power systems, devices for terrestrial energy systems and aerospace applications, and the policies, programs, and environmental impacts associated with the development and utilization of this technology. The IECEC is hosted by AIAA, which is joined this year by four Participating Organizations. These organizations are: • The Heat Transfer Society of Japan (HTSJ)

10th International Energy Conversion Engineering Conference (IECEC) CONFERENCE THEME:

• The IEEE Aerospace & Electronic Systems Society (AESS)

Aerospace Capabilities Applied to Solving Terrestrial Energy Problems—A Game Changer

• The Egyptian Society of Mechanical Engineers (ESME) • The Japan Society of Mechanical Engineers (JSME)

IECEC Organizing Committee General Chair

Technical Program Chair

Deputy General Chair

Deputy Technical Program Chair

Ramon Lugo Director, NASA Glenn Research Center

Michael Choi NASA Goddard Space Flight Center

Robert “Joe” Shaw NASA Glenn Research Center

Kenneth “Mark” Bryden Iowa State University

Topic Area Organizers Aerospace Power Systems

Terrestrial Energy-Efficient and Renewable Energy Systems

Mark Liffring The Boeing Company

Thomas Bradley Colorado State University

Abbas Salim Lockheed Martin Space Systems (Retired)

Essam Khalil Cairo University

Energy Conversion Device Technology

Terrestrial Fossil Energy Systems

Edward Lewandowski NASA Glenn Research Center

Ahsan Choudhuri University of Texas at El Paso

Energy Storage Technology

Richard Shaw Lockheed Martin Space Systems

Terrestrial Nuclear Energy Systems Pavel Tsvetkov Texas A&M University

Terrestrial Electricity Delivery and Grid Reliability

Thermal Management Technology

Bill Lear University of Florida

Michael Choi NASA Goddard Space Flight Center

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© 2012 Lockheed Martin Corporation

AS START-UP COMPANIES GO,

THEIRS REALLY TOOK OFF. It all started in a garage, with the backing of a local taxicab owner. Allan and Malcolm Lockheed. Two brothers who fell in love with aviation and didn’t mind getting their hands dirty. Little did they know, as their Model G swooped over the waters of San Francisco Bay, that one day the company that bore their name would help man touch down on the Moon’s Sea of Tranquility. Or that their stars would cross with that of a barnstormer named Glenn L. Martin. Their story is our story. One of many you’ll find at: www.lockheedmartin.com/100years

Special SessionsEngineering Conference 10th International Energy Conversion 1300–1400 hrs

Monday, 30 July 0800–0900 hrs

Centennial Ballroom I

Joint Opening Keynote – Overview of NASA major program thrusts and Technology Development Opportunities Robert Lightfoot, Acting Associate Administrator,

NASA

1000–1200 hrs


NASA MSFC National Institute for Rocket Propulsion Systems


The Role of Propulsion Technology in Commercial Space Applications Antonio L. Elias, Executive Vice President and

General Manager, Advanced Programs Group, Orbital Sciences Corporation

1400–1600 hrs


Commercial Space Development

Join this panel of commercial space leaders in an interactive discussion of commercial space developments and future space plans. We will address current issues and consider future strategies and opportunities.

MODERATOR: Dale Thomas, Associate Director, Technical, NASA Marshall Space Flight Center PANELISTS:

MODERATOR: Michael Griffin, AIAA President, Former NASA Administrator PANELISTS:

Vigor Yang, Professor, Georgia Tech Julie Van Kleeck, Vice President, Space & Launch

John Mulholland, Vice President & Program

Charlie Precourt, Vice President and General

Lisa Matthews, Business Development Director

John Vilja, Vice President, Strategy Innovation &

Brett Alexander, Director, Business Development &

George F. Sowers, Vice President, Business

Charles Precourt, Vice President & General

Systems, Aerojet

Manager, Space Launch Division, ATK Growth, Pratt & Whitney Rocketdyne

Development & Advanced Programs, United Space Alliance

Brett Alexander, Director, Strategy & Business Development, Blue Origin

1000–1200 hrs

Dunwoody

Shuttle Space Transportation Replacement Options and Progress

Manager, Commercial Programs, Space Exploration, The Boeing Company Propulsion, Space Systems Group, Sierra Nevada Strategy, Blue Origin

Manager, Space Launch Division, ATK

Frank Culbertson, Senior Vice President and

Deputy General Manager, Human Spaceflight Systems, Orbital Sciences

Adam Harris, Vice President, Government Sales, SpaceX

George Sowers, Vice President, Business Development, ULA

MODERATOR: Paul M. Anderson, Lockheed Martin Space Systems Company, Denver, Colorado The safe return of Space Shuttle Atlantis on 21 July 2011, marked the end of nearly 30 years of near-continuous American space exploration and achievements. Although this milestone marked the end of the shuttle era, the future of American human spaceflight is far from bleak. In April 2011, NASA awarded contracts to four commercial companies to continue development of commercial rockets and spacecraft capable of safely flying astronauts into orbit and to the International Space Station. In addition, NASA is making steady progress on building the Orion spacecraft, which is being designed to take astronauts deeper into space than ever before. The purpose of this session is to present the progress that is being made on several of these options, including highlighting the key technical drivers, achievements, and challenges that each is facing as America heads into its next era of human spaceflight.

1400–1600 hrs

Dunwoody

Micro/Nano Thermal Management Technology for Aerospace, Energy, and Environment The micro/nano-scale thermal management technologies in this panel session include, but are not limited to, heat and mass transport issues in the following materials, components or systems: carbon nanotubes, high temperature nanofibers, ceramics, aerogel insulation, thermal energy storage, microcoolers, nanopropellants, propulsion systems, in-space propulsion, solar-electrical conversion, solarfuel conversion, thermoelectric energy conversion, magnetocaloric energy conversion, pyroelectric energy conversion, piezoelectric energy conversion, electrochemical energy conversion and storage, chip scale spot cooling, and waste heat recovery. A panel of experts will discuss the emerging micro/nano-scale thermal management technologies for aerospace, energy and environment, and offer their vision for the future of these technologies. Focus will be placed on challenges and opportunities. PANELISTS:

Timothy Fisher, Purdue University Rama Venkatasubramanian, RTI International Theodorian Borca-Tasciuc, Rensselaer Polytechnic Institute

Gerald Mahan, Penn State University 1630–1830 hrs


Next Steps in Hypersonics – Turning Research into Reality

MODERATOR: Mark Lewis, Director, Science and Technology Policy Institute, Institute for Defense Analyses PANELISTS:

Chris Gettinger, ATK Kenneth Rock, NASA Langley Research Center Timothy O’Brien, Aerojet Rodney Bowersox, Texas A&M James Kenyon, Office of the Secretary of Defense Chiping Li, AFOSR 1630–1830 hrs

Dunwoody

Combustion Characteristics of High Hydrogen Content Fuels

MODERATOR: Ahsan Choudhuri, University of Texas at El Paso High hydrogen content (HHC) fuels impose significant combustor design challenges due to their different flame behavior and working fluid characteristics as compared with natural gas. The panel session summarizes HHC fuel issues in the context of robust, reliable, lowemission, and fuel flexible combustor technology development.

PANELISTS:

Merri Sanchez, Senior Director Space Exploration Systems, Sierra Nevada

Adam Harris, Vice President for Government Sales, SpaceX

Larry Price, Deputy Program Manager, CEV

Development, Lockheed Martin Space Systems Company

Paul Marshall, NASA Johnson Space Center Kent Rominger, VP Strategy and Business, Space Launch Systems, ATK Aerospace Systems Group

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10th International Energy Conversion Engineering Conference Special Sessions Tuesday, 31 July 0800–0900 hrs


Turbine Engines: Aviation Management and Technology

SPEAKER: David Garrison, Managing Director Engine and Component Maintenance for Delta Tech Ops Airlines are continuously looking for ways to lower costs and improve efficiency and reliability. Delta Air Lines currently maintains a fleet of more than 750 aircraft, plus provides maintenance for more than 150 other operators. The Delta fleet is one of the most reliable fleets in the world. Delta has developed an unparalleled level of experience and knowledge in the art of aircraft and engine maintenance. Delta must rely on new technology and develop new processes to make aircraft and engines more reliable and fuel-efficient. This in turn enables Delta to expand service to new cities, increase profits, and achieve industry-leading operational performance.

0800–0900 hrs

Dunwoody

IECEC KEYNOTE – AEROSPACE CAPABILITIES APPLIED TO SOLVING TERRESTRIAL ENERGY PROBLEMS ... A UNIVERSITY VIEW SPEAKER: Ronald Sega, Vice President of Energy and Environment, Institute of Energy and Environment, The Ohio State University

1000–1200 hrs


Challenges for Future Commercial Aircraft Propulsion

MODERATOR: Richard A. Wahls, Project Scientist, Subsonic Fixed Wing, NASA The panel will discuss NASA and U.S. industry perspective on propulsion technology required to meet the technical challenges envisioned for future commercial aircraft. Speakers will highlight the short-, mid-, and long-term perspectives of the visions: PANELISTS:

Rubén Del Rosario, Project Manager, Subsonic Fixed Wing, NASA

Alan Epstein, Vice President, Technology and Environment, Pratt & Whitney

Mark Wilson, Chief Operating Officer, Rolls-Royce North American Technologies, Inc. (LibertyWorks)

Richard Donaldson, Executive, Advanced Programs, GE Aviation

1000–1200 hrs

Dunwoody

Solar Assisted Absorption and Desiccant Cooling Technologies for Air Conditioning in Sunny Countries

MODERATORS: Thomas Bradley, Colorado State University, and Essam Khalil, Cairo University Air conditioning contributes a major consumption of electricity in many parts of the world, especially in sunny countries. As the demand for air conditioning increases, the electricity demand increases. Solar assisted absorption or desiccant cooling is a sustainable

solution. It reduces the demand for electricity. A panel of experts will present their views on solar assisted absorption and desiccant cooling technologies in sunny countries. They will focus on challenges and opportunities. PANELISTS:

Rhett Jeffries, Program Manager, Continuously

Eduardo A. Rincón, Autonomous University of the

1600–1830 hrs

State of Mexico

Ming Qu, Purdue University Jo Darkwa, University of Nottingham-Ningbo Nesreen Ghaddar, Associate Provost, Qatar Chair

Lower Energy, Emissions, and Noise, FAA

Diane Hooie, Senior Advisor, Energy Delivery

Technologies Division, National Energy Technology Laboratory, Department of Energy


Challenges for Future Rotorcraft Propulsion

in Energy Studies, Professor of Mechanical Engineering, American University of Beirut

MODERATOR: George A. Bobula, Chief Engineer, Propulsion Division Aviation Engineering Directorate, AMRDEC PANELISTS:

1000–1200 hrs

Susan Gorton, Project Manager, NASA Subsonic

Spring

Robust and Resilient System Design Approaches for Next Generation Terrestrial Nuclear Energy Systems.

MODERATOR: Piyush Sabharwall, Idaho National Laboratory Novel terrestrial nuclear energy systems are emerging for a broad range of potential applications from conventional electricity generation to process heat for energy-demanding industrial applications with an expectation of absolute safety and autonomy of operation. These requirements and trends lead to an amplified synergy between considerations for space systems and terrestrial systems within the realm of nuclear-driven configurations. This special session will offer a forum to discuss designs, requirements, methods, and trends for novel nuclear energy systems focusing on robust and resilient system design approaches needed for next-generation technology development to meet performance targets under competitive economics constraints.

1200–1400 hrs

Centennial Ballroom IV

IECEC AWARDS LUNCHEON (Tickets required for lunch)

Aerospace Capabilities Applied to Solving Terrestrial Energy Problems ... A Federal Laboratory View

SPEAKER: William Harrison III, Technical Advisor for Fuels and Energy, Air Force Research Laboratory Fellow, USAF

1300–1500 hrs


Interagency Propulsion Technology Development

MODERATOR: James Kenyon, Associate Director, Aerospace Technology, Office of the Secretary of Defense PANELISTS:

William Harrison, Technical Advisor for Fuels and Energy, Air Force Research Laboratory

Jennings Bryant, Senior Engineer, Advanced Development & Technology Transition Naval Air Systems Command

Fayette Collier, Project Manager, Environmentally Responsible Aviation, NASA

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Rotary Wing Project

Catherine Ferrie, Director, Xworx & Test and Evaluation, Bell Helicopter

Richard F. Spivey, Director, U.S. Army Aeroflightdynamics Directorate

Steve Weiner, Director, Engineering Sciences, Sikorsky Aircraft Corporation

Harold Rosenstein, Chief Engineer, Advanced Mobility, Boeing Phantom Works

1600–1830 hrs

Dunwoody

I. The Future of Smart Grid in the United States and Abroad. II. Robust and Resilient System Design Approaches for Next-Generation Terrestrial Nuclear Energy Systems MODERATORS: William Lear, University of Florida, and Michael Choi, NASA-Goddard Space Flight Center Smart Grid has become a critical agenda item around the globe. The speakers will present their views on the future of Smart Grid in the United States and abroad. They will focus on opportunities and challenges. PANELISTS:

Scott Duncan, Georgia Institute of Technology Takashi Hikihara, Kyoto University Reji Kumar Pillai, President, India Smart Grid Forum (a PPP initiative of Govt. of India)

José Eduardo Azarite, Director of Marketing, CPqD

Anh Vu, Smart Cities Program Manager, ERDF Distribution

Egon Ortjohann, Head of Power Systems and Power Economics Department, South Westphalia University of Applied Sciences

48th AIAA/ASME/SAE/ASEESpecial Joint Propulsion Sessions Conference and Exhibit 0930–1200 hrs

Wednesday, 1 August 0800–0900 hrs


Dunwoody

The Latest Advances in Radioisotope Power Systems – A Mission Perspective

SPEAKER: Wes Harris, Charles Stark Draper Professor of Aeronautics and Astronautics, Massachusetts Institute of Technology

MODERATOR: Edward Lewandowski, NASA Glenn Research Center Panelists will present their perspectives on radioisotope power systems, including MMRTG, ASRG and RTG, and on Mars Science Lab, New Horizons, and ASRG missions. PANELISTS:

0800–0900 hrs

Ralph McNutt, Applied Physics Laboratory, Johns

JPC Keynote – Flight Testing: Increasing Value and Demand

Dunwoody

IECEC Keynote – Aerospace Capabilities Applied to Solving Terrestrial Energy Problems ... An Aerospace Industry View

SPEAKER: David Parekh, Vice President of Research, Director, United Technologies Research Center

0930–1200 hrs

Hopkins University

Dave Woerner, Jet Propulsion Laboratory, California Institute of Technology Speakers:

1200–1400 hrs


JPC AWARDS LUNCHEON Sponsored by:


Clipped Wings: Assessing U.S. Aeronautical Flight Research

MODERATOR: Victor Lebacqz, VICC Associates, Principal PANELISTS:

Richard Christiansen, Vice President, Sierra Lobo Mark Anderson, Director Platform Performance Technology, The Boeing Company

Dale Carlson, General Manager, Technology Strategy, GE Aviation

Douglas Bowers (invited), Chief Propulsion Division, USAF AFRL

John Langford, CEO, Aurora Flight Sciences Thomas Irvine, NASA Deputy Associate Administrator, Aeronautics Research Mission Directorate

(Tickets required for lunch)

Air Mobility History and Flight Testing at Lockheed Martin

SPEAKER: Wayne Roberts, Lockheed Martin Fellow, Chief Test Pilot for Airlift Programs

1400–1700 hrs


NSTC Aeronautics S&T Subcommittee Public Outreach

The National Science and Technology Council’s (NSTC) Aeronautics Science and Technology Subcommittee will unveil and discuss the results of its recent assessment of progress under the National Aeronautics Research and Development Plan. In addition, the subcommittee will engage public stakeholders on key issues in aeronautics research and development and future subcommittee activities.

AIAA is the world’s largest technical society dedicated to the global aerospace profession. With more than 35,000 individual members worldwide, and nearly 100 corporate members, AIAA brings together industry, academia, and government to advance engineering and science in aviation, space, and defense.

American Institute of Aeronautics and Astronautics 1801 Alexander Bell Drive, Suite 500 Reston, VA 20191-4344 703.264.7500 or 800.639.AIAA (2422) Fax: 703.264.7657 [email protected] www.aiaa.org

www.aiaa.org

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Special Events Sunday, 29 July 2012

Tuesday 31 July 2012 Delta Museum Tour

Opening Reception

The opening reception will be held Sunday, 29 July, 1830–2000 hrs, in the exhibit hall. The cost is included in the registration fee where indicated. Additional tickets may be purchased upon registration or at the on-site registration desk, while supplies last.

Monday, 30 July 2012 1000–1100 hrs

Marietta Room

Accompanying Persons Program

Accompanying persons are invited to meet on Monday, 30 July, at 1000 hrs, in the Marietta Room at the Hyatt Regency Atlanta. Information about local attractions, activities, tours, shows, and restaurants will be available. Coffee and tea will be served. 1730–1900 hrs

Centennial III

Young Professional Networking Reception

The AIAA Young Professional Committee is hosting a networking reception for early career professionals on Monday, 30 July, from 1730 to 1900 hrs, in the Centennial III room. This is a great opportunity for young professionals age 35 and under to meet and make new contacts. Join the AIAA Young Professional Committee for light hors d’oeuvres, drinks, and relaxed socializing.

Buses will depart at 0830 hrs from the corner of Peachtree and Baker. The museum’s collections and facilities include: The Spirit of Delta, Delta’s first 767, bought by employees, retirees, and friends and donated to Delta in 1982; the archives maintain over 200,000 images, 1,000 films, and one of the world’s largest airline uniform collections in a museum; replica of the first Delta station in Monroe, Louisiana; and an 800-square-foot museum shop, housed in a redesigned section of the hull of the first L-1011 ever built. Tickets are $15, include transportation, and are available on a first-come, first- served basis. Limit 50. 1600–1730

Exhibit Hall

Corporate Member/Exhibitor Reception AIAA is hosting a reception for our exhibitors and corporate member representatives.

Wednesday, 1 August 2012 Lockheed Martin Facility Tour

Buses will depart at 0830 hrs from the corner of Peachtree and Baker. The tour will be conducted at the Lockheed Martin Marietta facility, home of the C-130J Super Hercules advanced tactical aircraft production line and the C-5 Super Galaxy modernization production line. Visitors will get to see both production lines. Additionally, visitors will get an overview of the site history and also see the F-35 JSF mid fuselage and P-3 wing production areas. Tickets are $15,

include transportation, and are available on a first-come, first-served basis. Limit 50. Those registering on site must be U.S. citizens and have proper identification. 0930–1130 hrs

Regency V

AIAA and ASME IGTI Student Design Competition Finalists in the AIAA/ASME IGTI engine design competition will be presenting their work and designs of a half-scale model of a Joint Strike Fighter aircraft. Winners will be announced at the end of the session. 1900–2200 hrs

Regency V

Engineers as Educators Workshop Do you want to interact with K-12 students? Do you want to share your passion and inspire others? Are you at a loss for where to start? This workshop will arm you with the tools, tips, and tricks to entrance your audience in a grade-level appropriate fashion by creating presentations and activities that will demonstrate the real-world applications of math and science taught in the classroom. You will learn how to construct presentations, use simple activities to demonstrate the engineering design process and scientific method, and learn how to approach an educator to share your experiences with their students. (The workshop is free and you can register on site.)

Award Luncheons For those registration types that include Awards Luncheon tickets, those registrants who selected IECEC as their primary conference will receive the Tuesday, 31 July IECEC Awards Luncheon ticket and those who selected JPC as their primary conference will receive the Wednesday, 1 August JPC Awards Luncheon ticket. Tickets are not exchangeable or refundable. The cost is included in the registration fee where indicated. Additional tickets may be purchased upon registration or at the on-site registration desk while supplies last. IECEC AWARDS LUNCHEON Energy Systems Award Darrell W. Pepper, University of Nevada-Las Vegas “For sustained development of novel computational modeling techniques related to new advanced energy concepts with exemplary innovations in research, education and consulting.” Aerospace Power Systems Award Robert Wiley, Office of Space and Defense Power Systems (Retired), U.S. Department of Energy “For over 40 years of outstanding contributions in space nuclear power systems, for efforts contributing to successful development and use of radioisotope power systems, and for efforts contributing to advancement and advocacy of space nuclear reactor technologies.”

JPC AWARDS LUNCHEON Sponsored by:

Air Breathing Propulsion Award Walter F. O’Brien, Virginia Polytechnic Institute and State University “For outstanding technical contributions, creativity, and generosity that have inspired hundreds of students to achieve bright careers in gas turbine and high speed propulsion.” Engineer of the Year Award John P. Clark, Aerospace Systems Directorate, Air Force Research Laboratory “For contributions to assessment and design of efficient gas turbine components, specifically for inventing optimization methods for shockinteraction reduction and improved film-cooling performance.”

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Propellants and Combustion Award Stephen B. Pope, Sibley School of Mechanical and Aerospace Engineering, Cornell University “For original and substantive contributions to the modeling of turbulent reactive flows, in particular for the development of probability density function methods.” Wyld Propulsion Award

Robert G. Jahn, Princeton University “For pioneering research and educational leadership in the field of electromagnetic plasma propulsion for spacecraft.” AIAA Sustained Service Award Ian Halliwell, Power Systems Manufacturing, Jupiter, Florida “For sustained service to AIAA at section, regional and national levels.”

General Conference Information

Registration and Information Center Hours Sunday, 29 July Monday, 30 July Tuesday, 31 July Wednesday, 1 August Thursday, 2 August (course only)

1500–1900 hrs 0700–1800 hrs 0700–1800 hrs 0700–1700 hrs 0700–0900 hrs

Conference Proceedings

Proceedings for this conference are available in online proceedings format. The cost is included in the registration fee where indicated. Attendees who register in advance for the online proceedings can access them now. Those registering on site will have access to the online proceedings 24 hours after registering.

Committee Meetings

AIAA committees provide incredible opportunities for networking, building your resume, and professional development. Scores of committees and subcommittees meet at JPC. Stop in to see how you can participate. A full committee schedule is located on page 15.

Networking Coffee Breaks

Networking coffee breaks for all attendees will take place in the exhibit hall. Times are designated in the Exhibit Guide on page 18. Coffee and other beverages will be served.

30% off on All Books at JPC/IECEC AIAA is offering a special discount on all titles featured at JPC/IECEC 2012. Attendees will be able to take advantage of a 30% discount on the list price of all books for sale at the AIAA bookstore. This special will only be available during the conference. Also featured will be the entire 2012 AIAA Book of the Month collection at their special month prices. Advanced Propulsion Systems and Technologies, Today to 2020, by Claudio Bruno and Antonio Accettura, has been selected as the featured conference book of JPC/IECEC, and is on sale for $71.47.A limited number of books are available at these prices, so make it a point to stop by the AIAA bookstore, located in the exhibit hall, while you are in Atlanta!

Frontier of Propulsion Science Information Session and Author Signing

Information Session – Presentation Stage Tuesday, 7/31 0915–0930 hrs Exhibit Hall Author Signing – AIAA Bookstore Tuesday, 7/31 0930–1000 hrs Exhibit Hall Come listen to Frontier of Propulsion Science authors Eric Davis and Marc Millis talk about their book at the Presentation Stage in the Exhibit Hall on Tuesday from 0915 to 0930. Then afterwards come by the AIAA Bookstore also in the in the Exhibit Hall from 0930-1000 to have your copy of Frontier of Propulsion Science signed by the authors. Frontier of Propulsion Science will be on sale for $90.97 (org. $129.95) at the AIAA Bookstore.

How to Access Online Proceedings • If you are preregistered and receive access to online proceedings as part of your conference registration, please visit www. aiaa.org and log in: v User Name: Email address that is registered with AIAA v Password: AIAA membership number • Click “My AIAA” at the top • Click “Conference Proceedings” under Access Publications & Materials • Scroll to the conference desired

Conference Certificate of Attendance Available Certificates of Attendance are available for attendees who request documentation at the conference itself. AIAA offers this service to better serve the needs of the professional community. Claims of hours or applicability toward professional education requirements are the responsibility of the participant. Please request your copy at the Registration and Information desk beginning Tuesday, 31 July.

SPEAKER AND SESSION CHAIR INFORMATION “No Paper, No Podium” and “No Podium, No Paper” Policies

If a written paper is not submitted by the final manuscript deadline, authors will not be permitted to present the paper at the conference. Also, if the paper is not presented at the conference, it will be withdrawn from the conference proceedings. It is the responsibility of those authors whose papers or presentations are accepted to ensure that a representative attends the conference to present the paper. These policies are intended to improve the quality of the conference for attendees.

4-JPC-15 you would sit at table 4). Please wear your conference badge and only attend on the day of your session(s). Continental breakfast will be served.

Speakers’ Practice

A speakers’ practice room will be available for speakers wishing to practice their presentations, in the Williams Room. A signup sheet will be posted on the door for halfhour increments.

Timing of Presentations

Each paper will be allotted 30 minutes (including introduction and question-andanswer period) except where noted.

Audiovisual

Each session room will be preset with the following: one LCD projector, one screen, and one microphone (if needed). AIAA does not provide computers or technicians to connect LCD projectors. Should presenters wish to use an LCD projector, it is their responsibility to bring or arrange for a computer on their own. Please note that AIAA does not provide security in the session rooms and recommends that items of value, including computers, not be left unattended. For additional audiovisual requests please come to the registration and information desk.

Sponsors AIAA would like to extend our thanks to this year’s Joint Propulsion Conference and International Energy Conversion Engineering Conference sponsors and supporters. Lead Industry Sponsor

Lead Government Sponsor

JPC Awards Luncheon Sponsor

USB Memory Stick Sponsor

Speakers’ Briefing

Authors who are presenting papers, keynote speakers, panelists, and session chairs will meet for a short briefing on the day of their presentation(s) at 0700 hrs in Centennial Ballroom at the Hyatt Regency Atlanta. Tables are labeled with the first number in your session number (e.g., if you are presenting 11

General Conference Sponsors

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General Conference General Information Conference Information

Journal Publication

Authors of appropriate papers are encouraged to submit them for possible publication in one of the Institute’s archival journals: AIAA Journal; Journal of Aircraft; Journal of Guidance, Control, and Dynamics; Journal of Propulsion and Power; Journal of Spacecraft and Rockets; Journal of Thermophysics and Heat Transfer; or Journal of Aerospace Computing, Information, and Communication. You may now submit your paper online at http://mc.manuscriptcentral.com/aiaa.

encouraged to have personnel who are attending an AIAA technical conference bring “open position” job postings. Individual AIAA members may post “available for employment” notices. AIAA cannot assume responsibility for notices forwarded to AIAA Headquarters. AIAA reserves the right to remove inappropriate notices. AIAA members can post and browse resumes, browse job listings, and access other online employment resources by visiting the AIAA Career Center at http://careercenter.aiaa.org.

Session Chair Forms

AIAA Membership

Session chairs are asked to complete a Session Chair Report for each session. To assist volunteers in compiling this information, this year we have moved to an electronic session chair form. Download the app on your smartphone or tablet or visit the reporting station and enter your session information. If you do not have a smartphone, simply fill out the form provided at the Speakers’ Briefing during your session and enter your results at the session chair reporting station located at the registration desk. Reports are collected and used for planning purposes, including future session topics and room allocations. Please submit your session information electronically before the end of the conference.

Messages and Information

Messages will be recorded and posted on a bulletin board in the registration area. It is not possible to page attendees.

AIAA Pavilion

Get connected at the AIAA Pavilion (in the exhibit hall) to the people, programs and products that can advance your career. Stop by to find out more about the bendfits of AIAA and browse top aerospace titles.

Employment Opportunities

AIAA assists members who are searching for employment by providing a bulletin board at technical meetings. This bulletin board is solely for “open position” and “available for employment” postings. Employers are

Attendees who pay the nonmember registration rate receive a free year of AIAA membership, including benefits like Aerospace America, AIAA Daily Launch, local section membership, and reduced fees for AIAA products and services. Renewing members must pay the nonmember rate in order for their AIAA membership to be renewed for another year. Those paying through group registration do not receive a free year of membership.

Nondiscriminatory Practices AIAA accepts registrations irrespective of race, creed, sex, color, physical handicap, sexual orientation, and national or ethnic origin.

Restrictions

Photography, video or audio recording of sessions or technical exhibits, as well as the unauthorized sale of AIAA-copyrighted material, is prohibited.

International Traffic in Arms Regulations (ITAR)

AIAA speakers and attendees are reminded that some topics discussed in the conference could be controlled by the International Traffic in Arms Regulations (ITAR). U.S. nationals (U.S. citizens and permanent residents) are responsible for ensuring that technical data they present in open sessions to non-U.S. nationals in attendance or in conference proceedings are not export restricted by the ITAR. U.S. nationals are likewise responsible for ensuring that they do not discuss ITAR

export-restricted information with non-U.S. nationals in attendance.

Regional Leadership Conference

The 2012 Regional Leadership Conference (RLC) is an opportunity to introduce new section officers and deputy directors to the institute’s resources and programs. In addition, it will provide sections and regions with information on upcoming events and new activities to increase member motivation and encourage member participation. The conference is open to all section officers and deputy directors. The conference will be Thurs–Fri, 2–3 Aug. It will begin with a combined luncheon with the AIAA Board of Directors where Mike Griffin, AIAA President, will address the attendees. The afternoon will have sessions helping officers have a rewarding experience. There will also be a reception so that attendees can mingle and discuss activities with other officers. Register for the conference at the AIAA website.

Continuing Education Course

Let AIAA Continuing Education courses pave the way to your continuing and future success! As the premier association representing aeronautics and astronautics professionals, AIAA has been a conduit for continuing education for more than 60 years. AIAA offers the best instructors and courses, and is committed to keeping aerospace professionals at their technical best. The following course will take place 2–3 August at the Hyatt Regency Atlanta from 0815–1700 hrs. Space is still available! To register please visit the conference registration and information center. Advanced Solid Rockets For full course description please visit the AIAA website. INSTRUCTORS: Course is taught by the distinguished members of the AIAA Solid Rockets Technical Committee, led by David Poe, Aerojet.

Connect online with AIAA

Tweeting during the conference Use #AIAAJPCIECEC Follow conference updates on our Facebook page: www.facebook.com/AIAAfan Find any after-conference videos at: www.youtube.com/wwwaiaaorg Members gain access to the AIAA LinkedIn Site at: www.linkedin.com/companies/aiaa 12

13

GeneralTAC Conference Information Structure

www.aiaa.org The Technical Activities Committee (TAC), led by AIAA’s Vice President for Technical Activities, is responsible for overseeing the operation of AIAA’s 69 Technical Committees (TCs) and 13 Program Committees (PCs). These committees are organized into seven Technical Groups, each of which is led by a Technical Director. These groups include Aerospace Design and Structures; Aerospace Sciences; Aircraft and Atmospheric Systems; Engineering and Technology Management; Information Systems; Propulsion and Energy; and Space and Missiles. AIAA TCs and PCs are a great way to get engaged, expand one’s professional network, and help the Institute deliver quality products and services to the aerospace community. AIAA TCs and PCs are responsible for many of the activities of the Institute, including conducting the many technical discipline and systems conferences, recognizing technical excellence through awards, generating standards, and presenting short courses. For more information about AIAA’s Technical and Program Committees, please visit www.aiaa.org/committees. AEROSPACE DESIGN AND STRUCTURES

ENGINEERING AND TECHNOLOGY MANAGEMENT

Adaptive Structures Design Engineering Materials Multidisciplinary Design Optimization Non-Deterministic Approaches Structural Dynamics Structures Survivability

Economics History Legal Aspects of Aeronautics and Astronautics Management Society and Aerospace Technology Systems Engineering

Space Colonization Space Logistics Space Operations and Support Space Resources Space Systems Space Tethers Space Transportation Weapon System Effectiveness

INFORMATION SYSTEMS

Communications Systems Computer Systems Digital Avionics Information and Command and Control Systems Intelligent Systems Sensor Systems Software

PROGRAM COMMITTEES

AEROSPACE SCIENCES

Aeroacoustics Aerodynamic Measurement Technology Applied Aerodynamics Astrodynamics Atmospheric and Space Environments Atmospheric Flight Mechanics Fluid Dynamics Ground Testing Guidance, Navigation and Control Meshing, Visualization and Computational Environments Modeling and Simulation Plasmadynamics and Lasers Thermophysics AIRCRAFT AND ATMOSPHERIC SYSTEMS

Aerodynamic Decelerator Systems Aircraft Design Aircraft Operations Air Transportation Systems Balloon Systems Flight Testing General Aviation Lighter-Than-Air Systems Product Support V/STOL Aircraft Systems

PROPULSION AND ENERGY

Aerospace Power Systems Air Breathing Propulsion Systems Integration Electric Propulsion Energetic Components and Systems Gas Turbine Engines High Speed Air Breathing Propulsion Hybrid Rockets Liquid Propulsion Nuclear and Future Flight Propulsion Propellants and Combustion Solid Rockets Terrestrial Energy Systems SPACE AND MISSILES

Life Sciences and Systems Microgravity and Space Processes Missile Systems Space Architecture Space Automation and Robotics

14

Aerospace Traffic Management Directed Energy Systems Energy Optimized Aircraft and Equipment Systems Gossamer Spacecraft Green Engineering Homeland Security HyTASP Reusable Launch Vehicles Space Environmental Systems Space Exploration Space Station Unmanned Systems Value Driven Design

General Conference Information Committee Meeting Schedule

SUNDAY, 29 JULY 2012 0800–1800 hrs

PAWs Workshop

Hanover CD

1500–1700 hrs

Propulsion and Energy Group Workshop

Regency V

1600–1800 hrs

SRTC Awards and Communications Subcommittees

Harris

1600–1800 hrs

SRTC History and Education Subcommittees

Edgewood

1700–1900 hrs

TAC Propulsion and Energy Group

Centennial III

MONDAY, 30 JULY 2012 0900–1000 hrs

ABPTCs Steering Committee

Edgewood

1000–1100 hrs

ABPSITC Steering Committee

Edgewood

1000–1100 hrs

GTETC Steering Committee

Auburn

1000–1100 hrs

HSABPTC Steering Committee

Harris

1000–1130 hrs

Accompanying Persons Program

Marietta

1100–1200 hrs

ABPTCs Membership Subcommittee

Harris

1200–1400 hrs

ASME Propulsion TC Annual Meeting

Executive Conference Room 222

1200–1400 hrs

Nuclear and Future Flight Propulsion TC

Auburn

1200–1800 hrs

ICW – Craft-tech Meeting


1300–1330 hrs

ABPTCs New Member Orientation

Harris

1300–1400 hrs

ABPTCs Communications Subcommittee

Edgewood

1400–1500 hrs

ABPTCs Working Groups

Harris

1400–1600 hrs

JPC Steering Committee


1500–1600 hrs

ABPTCs Honors and Awards Subcommittee

Edgewood

1600–1700 hrs

ABPTCs Education Subcommittee

Harris

1700–1900 hrs

LPTC Steering Committee


1730–1900 hrs

Young Professional Networking Reception

Centennial III

1900–2100 hrs

Air Breathing Propulsion Systems Integration TC

Baker

1900–2100 hrs

Gas Turbine Engines TC

Fairlie

1900–2100 hrs

High Speed Air Breathing Propulsion TC

Courtland

1900–2200 hrs

Electric Propulsion TC

Regency VI

1900–2200 hrs

Energetic Components and Systems TC

Hanover E

1900–2200 hrs

Hybrid Rockets TC

Regency VII

1900–2200 hrs

Propellants and Combustion TC

Regency V

1900–2200 hrs

Solid Rockets TC

Hanover FG

1900–2200 hrs

Terrestrial Energy Systems TC

Hanover D

TUESDAY, 31 JULY 2012 0800–1130 hrs

TAC New Initiatives Subcommittee

Marietta

0830–1700 hrs

Young Professional Committee

Harris

0830–1000 hrs

ABPTCs Conference Subcommittees


0900–1200 hrs

AIAA Hydrogen Committee on Standards


0930–1030 hrs

JPC 2013 Planning Meeting

Centennial III

0930–1130 hrs

Finance Committee Meeting

International South

1130–1400 hrs

TAC Executive Board Meeting

Marietta

1300–1400 hrs

Aerospace America Steering Committee

Heritage Board Room

1300–1400 hrs

GTETC Nominations Subcommittee


1300–1500 hrs

Emerging Technologies Committee


1330–1500 hrs

Exhibitor Advisory Committee

Edgewood

1400–1530 hrs

AIAA Propulsion and Energy Forum (JPC/IECEC) 2014

Centennial III

1500–1800 hrs

Summer Public Policy Committee Meeting

International South

1400–1800 hrs

TAC Conference Strategic Planning Initiative

Marietta

1600–1700 hrs

HSABP/HyTASP Committees Liaison Meeting

Centennial II 15

General Committee Conference Meeting Information Schedule 1600–1730 hrs

Corporate Member/Exhibit Reception

Grand Hall

1700–1800 hrs

IECEC 2013

Edgewood

1700–1830 hrs

ABPTCs Working Groups


1730–1830 hrs

DEFENSE Event Feedback Session


1800–1930 hrs

Aerospace Today and Tomorrow Planning Meeting

Harris

1830–2130 hrs

ABPTCs Dinner Meeting

Centennial IV

1900–2100 hrs

HRTC Student Meeting

Courtland

1900–2200 hrs

Aerospace Power Systems TC

Hanover A

1900–2200 hrs

Green Engineering PC

Hanover B

1900–2200 hrs

Liquid Propulsion TC

Hanover CD

1900–2200 hrs

Regional Directors Meeting

Hanover G

1900–2200 hrs

ICW – Sea-Based Aviation NNR

Regency VIII

WEDNESDAY, 1 AUGUST 2012 0800–1500 hrs

Region and Section Activities Meeting (RSAC)

Marietta

0800–1600 hrs

Technical Activities Committee Meeting

Embassy CD

1000–1200 hrs

ABPSITC Working Groups

Heritage Board Room

1000–1200 hrs

ABPTCs PAW

Centennial II

1000–1200 hrs

AIAA Foundation Board of Trustees


1000–1200 hrs

GTETC Working Groups

Harris

1000–1200 hrs

HSABPTC Working Groups

Auburn

1330–1730 hrs

IDC Meeting

Embassy F

1400–1500 hrs

HyTASP PC Liaisons Subcommittee

Auburn

1500–1600 hrs

HyTASP PC Honors and Awards Subcommittee

Auburn

1600–1700 hrs

HyTASP PC Public Policy Subcommittee

Auburn

1700–1800 hrs

HyTASP PC Steering Committee

Auburn

1700–1830 hrs

Board Chat Room


1715–1915 hrs

IECEC Steering Committee

Harris

1800–2100 hrs

AIAA Lockheed Martin Meeting

Marietta

1830–2000 hrs

Excomm Dinner

Sway Private Dining Room

1900–2200 hrs

Engineers as Educators Workshop

Regency V

1900–2200 hrs

HyTASP PC

Courtland

THURSDAY, 2 AUGUST 2012 0730–0800 hrs

AIAA Board of Directors Breakfast

Embassy CD

0800–1200 hrs

AIAA Board of Directors Meeting

Embassy CD

0800–1730 hrs

Space Transportation TC

Courtland

0815–1700 hrs

Advanced Solid Rockets

Baker

1000–1130 hrs

Engineers as Educators Local Section Version

Fairlie

1200–1400 hrs

Regional Leadership Conference/Board Combined Luncheon

Centennial IV

1330–1700 hrs

Nominating Committee Meeting


1400–1830 hrs


Learning Center

1830–2030 hrs

Regional Leadership Conference Reception

International South

FRIDAY, 3 AUGUST 2012 0700–1200 hrs


Learning Center

0815–1700 hrs

Advanced Solid Rockets

Baker

AIAA is developing a new DEFENSE event as part of its event strategy, starting in 2014. The event will be a forum that addresses technical, programmatic, and policy issues pertaining to aerospace in U.S. National Security. Help shape this event by attending a feedback session this week: Tuesday, 31 July 2012 • 1730–1830 hrs • Executive Conference Room 226 16

17

Exhibit Information and Floor plan

Exhibit Guide

Presentation Stage Schedule

The 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit will feature an impressive exhibit showcasing leading industry products and services relating to air-breathing, liquid, solid, nuclear, electric, and other forms of propulsion for aerospace.

0915–0930 hrs

1830–2000 hrs (Welcome Reception) 0900–1600 hrs 0900–1600 hrs 0700–1300 hrs

Pratt & Whitney Rocketdyne

TOPIC: The Future is Now

Communications and Tom Martin, NASA SLS Programs 0930–0945 hrs

Marotta

Computers with complimentary Internet access for conference attendees will be available at the AIAA Cyber Café, located in the exhibit hall. Hours of operation are as follows: Monday, 30 July 0700–1800 hrs Tuesday, 31 July 0700–1800 hrs Wednesday, 1 August 0700–1300 hrs

TOPIC: Marotta Controls – Committed to Space

Networking Coffee Break Hours

Technologist, Business Development, Hamilton Sundstrand Rocketdyne

Monday, 30 July Tuesday, 31 July Wednesday, 1 August

Tuesday, 31 July 0930–0945 hrs

Systems for the Worldwide Space Industry PRESENTER: Jay Hennig, President, Moog Space and Defense Group ANSA-USA

TOPIC: ANSA and MetaPost for Advanced CAE

Pre- and Post-Processin PRESENTER: Pravin Peddiraju, Senior Software Support Engineer, BETA CAE Systems, Inc.

Wednesday, 1 August

PRESENTER: Kurt Black, Business Development

Manager of Space and Aerospace

0910–0925 hrs

0945–1000 hrs

TITLE: The New Commercial NPSS™ Version

Hamilton Sundstrand Rocketdyne

PRESENTER: Paul Johnson, Head Simulation

Exploration PRESENTER:

Engineer, Wolverine Ventures

Dr. Cheng-Yi Lu, Chief

1610–1625 hrs

Wolverine Ventures

2.4.1-Features Overview

TOPIC: The Power for Science and Human

0900–1000 hrs 1600–1700 hrs 0900–1000 hrs 1600–1700 hrs 0900–1000 hrs

Moog Inc.

0945–1000 hrs

PRESENTER: Erin Dick, Director of

Cyber Café

and Defense, LMS North America

TOPIC: Developing New Motion-Control

Monday, 30 July 2012

Exhibit Hall Hours: Sunday, 29 July Monday, 30 July Tuesday, 31 July Wednesday, 1 August

PRESENTER: Paul Weal, Director of Aerospace

Please join us in the exhibit hall for additional learning and networking opportunities during your coffee breaks at the presentation stage. Full descriptions can be found online on the conference website.

LMS North America

TOPIC:Joint Jet Engine AuxiliaryConference Systems Integration 48th Propulsion & Exhibit

and Impact on Aircraft Thermal and Energy 2012 Management

Hyatt Regency Atlanta Atlanta, Georgia

WEST HALL EAST HALL

EXIT Ceiling height 11'8"

30

Wolverine Marotta

414

513

514

613

Sierra Nevada Corp

30

Ceiling height 11'8" Ceiling height 14'6"

512

AIAA Pavilion 206

410

LMCO LMS NA 30 307

Wyle 408

20

609

Moog

508

507

Cobham 815

713

714

NTS

813

816

915

814

913

916

1015

914

1013

Stanford Mu

607

Aisle 1100

715

Cambridge University Press

Boeing

Structural Aerojet Composites

ULA

409

616

L-3

Aisle 800

JASC 615

AFRL

Aisle 700

Reaction Engines 515

Aisle 600

416

10'

7'

Aisle 500

Presentation Stage

Aisle 400

Corporate Member Lounge

EXIT

EXIT

EXIT

Ceiling height 14'6"

Aisle1000

14'

Aisle 900

EXIT

EXIT

1011

610

709

Taber Ind. VACCO 809

608

707

708

Pointwise General Dynamics

Moog Mtg. Rm. 810 909

910

1009

ASME

10' 10'

EXIT

807

NASA 30110' NASA 303

15'

Concepts

NASA 302

10'

ATK 402

10'

Thales NREC 703 704

Pratt & Whitney 10' Rocketdyne

Valcor GA Ctr. 803'

804

RollsRoyce

801

802

901

Beta CAE US Army AEDC Metal Tech. Systems AMRDEC

502

701

702

EXIT

EXIT STORAGE

OFFICE

ENTRANCE 5'

10'

20'

30'

REGISTRATION

Electrical Service is from Ceiling and Columns

- 3'7" column

WOMEN

LOBBY

- 2'2" column

SERVICE

STORAGE

EXIT

Rev. 3/17/10 0'

30


9.5'

18

30

Cyber Cafe


8'

General Exhibit Conference GuideInformation

Aerojet

508

2001 Aerojet Road Rancho Cordova, CA 95742 www.aerojet.com [email protected]

BETA CAE Systems USA 29800 Middlebelt Road, Ste. 100 Farmington Hills, MI 48334 www.ansa-usa.com [email protected]

Aerojet, a world-recognized aerospace and defense leader, marks its 70th anniversary serving the missile and space propulsion markets. The company is the nation’s only provider of both liquid and solid rocket propulsion for launch vehicles; and in-space technologies that enable mission success for the nation’s defense, exploration, and commercial space missions.

Air Force Research Laboratory AFRL/RQ 2130 Eighth Street WPAFB, OH 45433 www.wpafb.af.mil/afrl/rz

BETA CAE Systems is an engineering services company that distributes & supports the industry leading ANSA & META software. ANSA is a CAE pre-processing tool for FE & CFD Analysis, for full-model build, from CAD to solver input file, in one integrated environment. META is a post-processor with for analyzing results from ANSYS, NASTRAN, ABAQUS, LS-DYNA, PAMCRASH, RADIOSS, MADYMO & other solvers.

514

The Boeing Company

AFRL is the Air Force’s only organization wholly dedicated to leading the discovery, development, and integration of warfighting technologies for our air, space, and cyberspace forces.

Boeing Defense, Space & Security combines manned and unmanned airborne capabilities, intelligence and security systems, communications architectures and extensive large-scale integration expertise across several diverse business areas.

Arnold Engineering Development Complex 701 100 Kindel Drive, Suite B212 Arnold AFB, TN 37289-2212 www.arnold.af.mil [email protected]

A $32 billion business with 61,000 employees worldwide, Boeing Defense, Space & Security’s strategy is to understand the enduring needs of customers and provide capability-based solutions to meet their rapidly evolving requirements. The strategy includes understanding the art of using current and emerging technologies to improve the capabilities of existing products and deliver new solutions.

Arnold Engineering Development Complex (AEDC) is the most advanced and largest complex of flight simulation test facilities in the world. The center operates aerodynamic and propulsion wind tunnels, rocket and turbine engine test cells, space environmental chambers, arc heaters, ballistic ranges, and other specialized units.

Cambridge University Press 32 Avenue of the Americas New York, NY 10013 www.cambridge.org/us/

807

625 The Corners Parkway Suite 115 Norcross, GA 30092 http://ogti.asme.org [email protected]

713

[email protected]

Cambridge University Press titles in engineering meet the needs of engineers at all levels of professional development and range from outstanding introductory textbooks to advanced-level references

IGTI provides international forums for the exchange of information related to gas turbines and turbo machinery. Upcoming events include Turbo Expo 2013 (www.turboexpo.org), the ASME Gas Turbine India Conference, and the 2013 Turbine Tip Blade Symposium and Course Week. IGTI also provides professional development training. Visit http://igti.asme.org

ATK

610

900 N. Sepulveda Boulevard MC S30-A402 El Segundo, CA 90245 www.boeing.com [email protected]

[email protected]

ASME – International Gas Turbine Institute

801

Cobham 2801 75th Street N St. Petersburg, FL 33710 http://www.cobham.com/

714

[email protected]

Cobham Life Support products have kept people safe on land, in the air, and under the water. We design and manufacture electroexplosively actuated devices for the aerospace and defense industries. Our customers consider us the prime choice in aircrew safety products, spacecraft propulsion valves, gas systems, and aerial delivery devices.

402

9160 North Highway 83 Corinne, UT 84307 www.atk.com [email protected] ATK is an aerospace, defense, and commercial products company specializing in solid rocket propulsion systems with extensive experience supporting human and space payload missions; small and micro-satellites, components, and subsystems; and lightweight and reliable composite aircraft structures. ATK has operations in 22 states, Puerto Rico, and internationally.

19

Exhibit Guide General Conference Information

Concepts NREC

704

LMS North America

409

217 Billings Farm Road White River Junction, VT 05001-9486 www.conceptsNREC.com [email protected]

5755 New King Street Troy, MI 48098 www.lmsintl.com [email protected]

Concepts NREC is an independent, full-service turbomachinery design/development organization offering Engineering Services (complete solution development from concept through performance testing), the Agile Engineering Design System® (turbomachinery-specific CAE/CAM design and analysis software) and Manufacturing Services (in-house machining center/mechanical assembly shop with 5-axis CNC mills) for turbochargers, fans, blowers, and pumps.

LMS International’s Model-Based Systems Engineering solutions and services support the development of propulsion and other complex mechatronics systems including design, plant modeling, systems simulation, controls development, and validation engineering. Talk to our experts and see how LMS can integrate the mechanical and software development processes and enable energy optimized systems.

General Dynamics – ATP

Lockheed Martin Aeronautics

707

1011 Lockheed Way Palmdale, CA 93559 www.lockheedmartin.com

4300 Industrial Avenue Lincoln, NE 68504 www.gdatp.com [email protected]

Marotta Controls, Inc. 78 Boonton Avenue P. O. Box 427 Montville, NJ 07045 www.marotta.com

Georgia Center of Innovation for Aerospace 804

The Georgia Center of Innovation for Aerospace, Georgia Department of Economic Development, and Metro Atlanta Chamber welcome you to Atlanta. Georgia is ranked in the top 5 among U.S. states in aerospace with over 500 companies and $5.4B in international aerospace exports on 2011. For more information visit Aerospace.georgiainnovation.org.

[email protected]

Metal Technology 173 Queen Avenue SE Albany, OR 97322 www.mtialbany.com

615

2303 W. Alameda Drive Tempe, AZ 85282 jasc-controls.com [email protected]

702

[email protected]

With more than forty years of experience, Metal Technology leads the way in the precision machining, forming, and forging of exotic matals. MTI works with materials such as Tantalum, Niobium, Titanium, Molybdenum, Tungsten, and their alloys. MTI is ISO9001 registered and supplies precission components to aerospace, defense, medical and scientific markets.

JASC specializes in the design and production of high-reliability components for pneumatic, hydraulic and fuel systems. Since its inception in 1990, JASC has been providing fluid control solutions and advanced products for the aircraft, spacecraft and power generation industries

L-3 Electron Technologies, Inc.

513

From the fuel control valves on the Saturn rocket to pressure relief valves for the Dragon Capsule, our qualified valves have proven their worth again and again in major space programs. We’re experts with high pressures, corrosive and challenging fluids such as hydrazine, hydrogen peroxide, and liquid oxygen, and cryogenic temperatures.

[email protected]

Jansen Aircraft Systems Controls

[email protected]

Lockheed Martin is a global security and aerospace company that employs about 123,000 people worldwide and is principally engaged in the research, design, development, manufacture, integration, and sustainment of advanced tecbnology systems, products, and services. The Corporation’s net sales for 2011 were $46.5 billion.

General Dynamics Armament and Technical Products provides reliable and affordable composite products to the defense and commercial aerospace markets. With more than 50 years of expertise, General Dynamics designs, develops, manufactures and tests a full range of composite missile and space structures, including rocket motors, pressure vessels, launch tubes and fuel tanks.

COI and GDEcD 75 Fifth Street NW, Ste. 1200 Atlanta, GA 30308 aerospace.georgiainnovation.org

307

Moog

613

507

300 Jamison Road, Plant 20 East Aurora, NY 14052 www.moog.com/space [email protected]

3100 W. Lomita Boulevard Torrence, CA 90505 www.l-3com.com/eti [email protected]

Moog designs and manufactures completely integrated fluid, motion control systems, and components. Moog’s solutions control flow of propellant to rocket engines, position satellite solar arrays and antennae, and perform thrust vector control to steer vehicles. In addition, Moog provides engineering analysis and complete design services to solve shock and vibration conditions.

L-3 Electron Technologies, Inc. (ETI) is a leading provider of electric propulsion systems for both commercial and scientific spacecraft. ETI has developed and delivered 13cm and 25cm Xenon Ion Propulsion Systems or XIPS® . ETI also delivered the 30cm XIPS® for NASA’s Deep Space 1 and DAWN spacecraft. ETI has developed an 8cm xenon thruster for small satellite and classified applications. 20

Exhibit Guide NASA 301/303

Reaction Engines Limited

300 E. Street SW Washington, DC 20546 www.nasa.gov [email protected]

Building D5, Culham Science Center OX14 3DB Abingdon OX14 3DB UNITED KINGDOM www.reactionengines.co.uk [email protected]

From advanced electric in-space propulsion to the liquid engines used in the Saturn V and Space Shuttle programs, developing to-space and in-space propulsion is nothing new for NASA. Now with the dawn of commercial access to the International Space Station, America’s Space Launch System (SLS) will provide the safe, affordable and sustainable heavy-lift capability needed to propel the next generation of human explorers and science missions beyond Earth’s orbit.

515

Driven by an extensive and pioneering technology programme, Reaction Engines Ltd has made a breakthrough in aerospace technology that is now allowing the development of engines that will propel aircraft at speeds of up to five times the speed of sound or directly into Earth orbit.

NASA 302

Rolls-Royce

300 E. Street SW Washington, DC 20546 www.nasa.gov [email protected]

2001 South Tibbs Avenue Indianapolis, IN 46241 www.Rolls-Royce.com [email protected]

NASA powers innovation in engineering and scientific research to develop advanced technologies for aerospace systems and space exploration. These achievements help contribute to the nation’s economic competitiveness and security as well as provide inspiration to encourage future generations to explore, learn, and build a better future.

LibertyWorks® vision is: Trusted to deliver the future by defining and demonstrating technologies and power-systems enabling customer focused solutions. LibertyWorks® focuses on increased capability and reduced fuel burn in advanced propulsion and power technologies and systems. Emphasis areas include highly efficient subsonic, supersonic and high Mach turbine propulsion systems, highly integrated inlet and exhaust systems, and innovative integrated power and thermal management systems.

NTS

709

24007 Ventura Blvd Calabasas, CA 91302 www.nts.com [email protected]

Sierra Nevada Corp.

Sierra Nevada Corporation’s Space Systems business area, headquartered in Louisville, Colorado, designs and manufactures advanced spacecraft, space vehicles, rocket motors and spacecraft subsystems and components for the U.S. government and commercial customers, as well as for the international market. SNC Space Systems has more than 25 years of space heritage in space and has participated in over 400 successful space missions through the delivery of over 4,000 systems, subsystems and components. During its history, SNC Space Systems has concluded over 70 programs for NASA and over 50 other clients.

608

213 S. Jennings Avenue Fort Worth, TX 76104 www.pointwise.com [email protected] Pointwise, Inc. is solving the top problem facing engineering analysts today: mesh generation for computational fluid dynamics. Manufacturing firms and research organizations use Pointwise’s mesh generation software to seamlessly bridge the gap between CAD and computational fluid dynamics analysis. Find more information at pointwise.com.

Pratt & Whitney Rocketdyne 6633 Canoga Ave. Canoga Park, CA 91309 www.PrattWhitneyRocketdyne.com

512

1722 Boxelder Street, Ste.102 Louisville, CO 80027 www.sncorp.com [email protected]

National Technical Systems’ advanced test and engineering capabilities have allowed our participation in every major space project since the inception of manned space exploration. NTS provides research and development, test and evaluation, systems integration, and precision cleaning on a wide range of aircraft, vehicles, systems, and components. Call 800.270.2516 or visit www.nts.com/aerospace.

Pointwise

901

Stanford Mu Corporation 20725 Annalee Avenue Carson, CA 90746 www.stanfordmu.com

607

[email protected]

Stanford Mu Corporation (SMC) is an accomplished aerospace company that is the worldwide leading provider of high quality aerospace products. SMC is comprised of Space and Airborne operating divisions. The Space and Airborne Divisions work hand in hand to provide exceptional products and engineering solutions to match the needs of our customers. SMC’s quality performance and knowledge in the aerospace industry dates back to 1993, and our customer satisfaction and accomplishments are well recognized internationally. Stanford Mu Corporation is committed to providing our customers with unparalleled, superior, reliable products.

502

[email protected]

Pratt & Whitney Rocketdyne, a recognized leader in propulsion for more than 55 years, engineers game-changing technologies that perform in the most extreme conditions on earth and in space. Our innovations power our nation’s space access to advance security, communication, and exploration while also providing sustainable solutions for the world’s toughest energy challenges. We are committed to delivering results that change the way we look at the planet and life on Earth itself. 21

22

Exhibit Guide General Conference Information

Structural Composites Industries LLC 336 Enterprise Place Pomona, CA 91768 wwww.scicomposites.com

609

VACCO Industries 10350 Vacco Street South El Monte, CA 91733 www.vacco.com [email protected]

wwww.scicomposites.com

Manufacturer of composite pressure vessels and structures.

Taber Industries

As your partner in propulsion, VACCO specializes in design and production of engineered fluid controls for human-rated, long duration and expendable space applications. Proven valves, regulators, filters, couplings, refueling mechanisms, welded manifolds, and highly integrated ChEMS™ Modules are available for applications ranging from cryogenic to high pressure and hazardous propellants.

809

455 Bryant Street North Tonawanda, NY 14120 www.taberindustries.com [email protected] Since 1948, Taber Industries has manufactured high-reliability pressure transducers to meet the critical requirements of our aerospace and satellite customers. Our transducers are designed for high accuracy and long life under adverse environments. Taber provides transducer’s featuring NASA Level 1 (Class S), NASA Level 2 (Class B), and Military Grade EEE Components. Heritage and unmatched quality is built into each transducer. Taber is compliant to AS9100B / ISO 9001-2008.

Thales Components 40G Commerce Way Totowa, NJ 07512 www.thalesgroup.com

Valcor

Valcor Aerospace specializes in the design and manufacture of custom valves and control components (solenoid, relief, check, fill and drain valves, pressure regulators, accumulators, actuators) for liquids (propellants, fuel, hydraulic fluid) and gases in critical aerospace (aircraft, launch vehicle, missile, spacecraft, etc.) applications.

[email protected]

Wolverine Ventures

The Thales propulsion system is based on HEMPr 3050 High Efficiency Multistage Plasma Thruster. It provides a cost effective solution to full in-orbit control of GEO Comsats Including: station keeping, momentum wheel off-loading, orbit topping, repositioning and transfer to graveyard orbit. Its modular concept allows “plug-and-play” integration on the satellite.

16593 121 Terrace N. Jupiter, FL 33458 www.wolverine-ventures.com

410

[email protected]

Wyle

United Launch Alliance is the nation’s rocket company, launching the most reliable and successful launch vehicles – Atlas and Delta – that have supported America’s presence in space for more than 50 years. Atlas and Delta expendable launch vehicles carry payloads to space ranging from weather, telecommunications and national security satellites to deep space and exploration missions.

Building 5400 Redstone Arsenal, AL 35898 www.redstone.army.mil/amrdec/

414

Wolverine Ventures, Inc. is an engineering software firm with more than 40+ years of combined experience in customized NPSS coding and complex systems modeling. As the exclusive distributor of NPSS software and the leading provider for NPSS related services, WVI is an unparalleled resource for NPSS sales, service, and training.

9501 E. Panorama Circle Cnetennial, CO 80112 www.ulalaunch.com [email protected]

U.S. Army AMRDEC

803

2 Lawrence Road Springfield, NJ 7081 www.valcor.com [email protected]

703

United Launch Alliance

708

408

128 Maryland Street El Segundo, CA 90245 www.wyle.com [email protected] Wyle’s San Bernardino, CA operations serves as a test facility for rocket engine development and qualification services. Wyle provides high energy flow testing with steam, water, gases, and cryogenic fluids using state-of-the-art data acquisition and control systems. Capabilities include: 50,000 lb. Multi-Axis Thrust Stand; Hydrocarbon and other fuels; Non-Reactives; Oxidizers; Cryogenics; Propellant Flows to Multiple Test Pads; Multiple Fluid Delivery Systems; MIL-STD-810 Testing; RTCA/DO-160D Testing; and dynamics.

802

[email protected]

The U.S. Army Aviation and Missile Research Development and Engineering Center (AMRDEC) is the Army’s focal point for providing research, development, and engineering technology and services for aviation and missile platforms across the lifecycle.

22

AeroengineTechnology JAXA’sAerospaceResearchDirectorate(ARD)isengagedinthe research and development of environmentally friendly aeroengine researchanddevelopmentofenvironmentallyfriendlyaeroengine technologies.

Hydrogenfueledhypersonic passengeraircraft

Hybridaeroenginepassengervehicle

Turbofanenginerelatedtechnologies

AerospacePowerSystems&Technologies AsthecentralresearchanddevelopmentbodywithinJAXA,ARDis committedtomaintainingandenhancingitstechnological capabilitieswhiledrivingforwardfundamentalresearchinaerospace fieldsincludingenergyconversion. g gy

LargeͲCapacityLithiumIonBattery

HighͲEfficiencyThin FilmSolarCell

http://www.jaxa.jp 23

UltraLightweightSolarPaddle

Program Overview General Conference Information

Sunday, 29 July 2012

Monday, 30 July 2012 IECEC

JPC “Space & High Speed Systems”

Introduction and Keynote Speaker

0800 hrs

Centennial Ballroom I Overview of NASA Major Program Thrusts and Technology Development Opportunities Robert Lightfoot, Acting Associate Administrator, NASA

0900 hrs

IECEC Technical Sessions

1100 hrs

1200 hrs

Panel Dunwoody Shuttle Space Transportation Replacement Options and Progress

Panel Centennial Ballroom I NASA MSFC National Institute for Rocket Propulsion Systems

Networking Lunch in Exhibit Hall Tickets Required Keynote Speaker

1300 hrs


1400 hrs

1500 hrs

Registration Open Networking Break in Exhibit Hall


1700 hrs

1800 hrs

1900 hrs

Panel Centennial Ballroom I Commercial Space Development

Opening Reception Tickets Required

24

Panel Dunwoody Combustion Characteristics of High Hydrogen Content Fuels

Panel Centennial Ballroom I Next Steps in Hypersonics – Turning Research into Reality

JPC Technical Sessions

1600 hrs

Panel Dunwoody Micro/Nano Thermal Management Technology for Aerospace, Energy and Environment


Centennial Ballroom I The Role of Propulsion Technology in Commercial Space Applications Antonio L. Elias, Executive Vice President and General Manager, Advanced Programs Group, Orbital Sciences Corporation

Exhibit Hall *See presentation stage schedule on page 18

1000 hrs


Networking Break in Exhibit Hall

General Conference Information Program Overview Tuesday, 31 July 2012 JPC

IECEC

IECEC Keynote Plenary Dunwoody Aerospace Capabilities Applied To Solving Terrestrial Energy Problems ... A University View Speaker: Ronald Sega, Vice President of Energy and Environment, Institute of Energy and Environment, The Ohio State University

“Commercial Aviation and Space Public Policy and Education” IECEC Keynote Plenary Panel Dunwoody Aerospace Capabilities Applied to Solving Terrestrial Energy Problems ... An Aerospace Industry View Speaker: David Parekh, Vice President of Research, Director, United Technologies Research Center

Keynote Speaker Centennial Ballroom I Turbine Engines: Aviation Management and Technology David Garrison, Managing Director, Engine and Component Maintenance for Delta Tech Ops


Aerospace Capabilities Applied to Solving Terrestrial Energy Problems ... A Federal Laboratory View Speaker: William Harrison III, Technical Advisor for Fuels and Energy, Air Force Research Laboratory Fellow, United States Air Force

Panel Centennial Ballroom I Interagency Propulsion Technology Development Moderator: James Kenyon, Associate Director, Aerospace Technology, Office of the Secretary of Defense




Panel Dunwoody I. The Future of Smart Grid in the United States and Abroad II. Robust and Resilient System Design Approaches for Next Generation Terrestrial Nuclear Energy Systems

Panel Centennial Ballroom I Challenges for Future Rotorcraft Propulsion

Panel Dunwoody The Latest Advances in Radioisotope Power Systems – A Mission Perspective







IECEC Awards Luncheon Tickets Required

Panel Centennial Ballroom I Challenges for Future Commercial Aircraft Propulsion


Panel Dunwoody Solar Absorption and Desiccant Cooling Technologies for Air Conditioning in Sunny Countries Panel Spring Robust and Resilient System Design Approaches for Next Generation Terrestrial Nuclear Energy Systems





Keynote Speaker Centennial Ballroom I Flight Testing: Increasing Value and Demand Wes Harris, Charles Stark Draper Professor of Aeronautics and Astronautics, Massachusetts Institute of Technology

Panel Centennial Ballroom I Clipped Wings: Assessing U.S. Aeronautical Flight Research


“Military and Commercial Aircraft Systems”

JPC


IECEC

Wednesday, 1 August 2012

JPC Awards Luncheon Tickets Required Air Mobility History and Flight Testing at Lockheed Martin Speaker: Wayne Roberts, Lockheed Martain Fellow, Chief Test Pilot for Airlift Programs

Panel Centennial Ballroom I NSTC Aeronautics S&T Subcommittee Public Outreach


Continuing Education Course Thursday–Friday 2–3 August 2012 0815–1700 hrs Hyatt Regency Atlanta

25

Event at a Glance General Conference Information

48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit Session ID

Session Title

Day

Start Time

Location

Special Sessions 1-RECPT-01

Sunday Opening Reception

Sunday

1830

Exhibit Hall

2-JPC-01/IECEC-01

JPC/IECEC Opening Keynote – Overview of NASA Major Program Thrusts and Technology Development Opportunities

Monday

0800


22-JPC-02

NASA MSFC National Institute for Rocket Propulsion Systems

Monday

1000


29-LNCH-01

Monday Exhibit Luncheon

Monday

1200

Exhibit Hall

30-JPC-03

Monday Afternoon Keynote

Monday

1300


36-JPC-04

Commercial Space Development

Monday

1400


71-JPC-05

Next Steps in Hypersonics - Turning Research into Reality

Monday

1630


85-JPC-06

Tuesday Opening Keynote

Tuesday

0800


91-JPC-07

Challenges for Future Commercial Aircraft Propulsion

Tuesday

1000


128-JPC-08

Interagency Propulsion Technology Development

Tuesday

1300


145-JPC-09


Tuesday

1600


166-JPC-10

Wednesday Opening Keynote

Wednesday

0800


173-JPC-11


Wednesday

0930


193-JPC-12

JPC Awards Luncheon

Wednesday

1200


212-JPC-13

NSTC Aeronautics S&T Subcommittee Public Outreach

Wednesday

1400


3-ABPSI-01/GTE-01

Turboelectric Distributed Propulsion I

Monday

1000

Hanover C

31-ABPSI-02/GTE-04 Turboelectric Distributed Propulsion II

Monday

1400

Hanover C

57-ABPSI-03

Monday

1630

Hanover B

59-ABPSI-04/GTE-08 Why Turboelectric Distributed Propulsion

Monday

1630

Hanover C

86-ABPSI-05

Propulsion Integration

Tuesday

1000

Hanover C

113-ABPSI-07

Inlet/Engine Performance Prediction Tools

Air-Breathing Propulsion Systems Integration

PDEs, ICEs, and Propellers

Tuesday

1300

Hanover C

114-ABPSI-08/GTE-13 The Impact of Engine Control Technologies on NASA Goals for Improved Aviation Safety, Environmental Compatibility and Performance

Tuesday

1300

Hanover E

199-ABPSI-13/GTE-23 Turbine Engine Control

Tuesday

1600

Hanover C

164-HSABP/HYP-08/ABPSI-10 High-Speed Inlets / Isolators I

Tuesday

1600

Regency VII

167-HSABP/HYP-09/ABPSI-11 High-Speed Inlets / Isolators II

Wednesday

0930

Regency VII

192-ABPSI-12

Wednesday

0930

Hanover C

Wednesday

1400

Hanover C

Nozzles and Thrust Reversers

139-ABPSI-09/HSABP/HYP-07 High Speed Integrated Inlets

Advanced Propulsion Concepts for Future Flight 7-APC-01

Advanced Propulsion Concepts I

Monday

1000

Hanover A

34-APC-02

Advanced Propulsion Concepts II

Monday

1400

Hanover A

141-APC-03

Advanced Propulsion Concepts III

Tuesday

1600

Hanover A

170-APC-04

Advanced Propulsion Concepts IV

Wednesday

0930

Hanover A

201-APC-05

Advanced Propulsion Concepts V

Wednesday

1400

Hanover A

14-ECS-01

Energetic Materials: Modeling and Experimental Studies

Monday

1000

University

Monday

1630

University

Energetic Components and Systems

Education 74-EDU-01


26

General Conference Information Event at a Glance

Session ID

Session Title

Day

Start Time

Location

Electric Propulsion 13-EP-01

Electric Propulsion Overview Panel

Monday

1000

Regency VI

15-EP-02

EP Facility Effects

Monday

1000

Baker

16-EP-03

Feed Systems

Monday

1000

Cortland

38-EP-04

Hall Thrusters I

Monday

1400

Regency VI

39-EP-05

Electrospray Propulsion I

Monday

1400

Baker

40-EP-06

Ion Thrusters I

Monday

1400

Cortland

58-EP-07

Electromagnetic Propulsion I

Monday

1630

Regency V

64-EP-08

Hall Thrusters II

Monday

1630

Regency VI

68-EP-09

Advanced Concepts I

Monday

1630

Baker

69-EP-10

Hall Thruster Physics I

Monday

1630

Cortland

89-EP-11

Electromagnetic Propulsion II

Tuesday

1000

Regency V

93-EP-12

Hall Thrusters III

Tuesday

1000

Regency VI

95-EP-13

Ion Thrusters II

Tuesday

1000

Cortland

97-EP-14

Advanced Concepts II

Tuesday

1000

Baker

120-EP-16

Electromagnetic Propulsion III

Tuesday

1300

Regency V

121-EP-17

Hall Thrusters IV

Tuesday

1300

Regency VI

123-EP-18

Ion Thrusters III

Tuesday

1300

The Learning Center

124-EP-19

Electrospray Propulsion II

Tuesday

1300

Baker

129-EP-20

Hall Thruster Physics II

Tuesday

1300

Cortland

140-EP-21

EP Systems and Mission Concepts

Tuesday

1600

Regency VI

144-EP-22

Cathodes

Tuesday

1600

The Learning Center

151-EP-23

Advanced Concepts III

Tuesday

1600

Baker

155-EP-24

Hall Thruster Physics III

Tuesday

1600

Cortland

169-EP-25

High Power Electric Propulsion Systems Panel

Wednesday

0930

Hanover E

179-EP-26

Hall Thrusters V

Wednesday

0930

Regency VI

180-EP-27

Ion Thrusters IV

Wednesday

0930

The Learning Center

182-EP-28

Advanced Concepts IV

Wednesday

0930

Baker

183-EP-29

Hall Thruster Physics IV

Wednesday

0930

Cortland

203-EP-30

Electromagnetic Propulsion IV

Wednesday

1400

Regency V

205-EP-32

Pulsed Plasma Thrusters

Wednesday

1400

Regency VI

215-EP-34

Hall Thruster Physics V

Wednesday

1400

Cortland

Wednesday

0930

Roswell

Green Energy 168-GEPC-01/GTE-19 Alternative Aviation Fuel Experiments (AAFEX) I & II

Gas Turbine Engines 3-ABPSI-01/GTE-01


Monday

1000

Hanover C

10-GTE-02

Compressors I

Monday

1000

Hanover F

20-GTE-03

Jet Noise I

Monday

1000

Hanover G

31-ABPSI-02/GTE-04 Turboelectric Distributed Propulsion II

Monday

1400

Hanover C

50-GTE-06

Jet Noise II

Monday

1400

Hanover G

56-GTE-07

Volcanic Ash

Monday

1400

Regency V

59-ABPSI-04/GTE-08 Why Turboelectric Distributed Propulsion

Monday

1630

Hanover C

73-GTE-09

Turbines

Manday

1630

Hanover F

82-GTE-10

Advanced Propulsion Architecture

Monday

1630

Hanover G

92-GTE-11

Compressors II

Tuesday

1000

Hanover F

27

Event at a Glance Session ID

Session Title

Day

Start Time

Location

Gas Turbine Engines continued 110-GTE-12/ABPSI-06 NASA Fundamental Aeronautics Program, Subsonic Fixed Wing Project, Efficient Propulsion and Power Research Tuesday

1000

Hanover G

114-ABPSI-08/GTE-13 The Impact of Engine Control Technologies on NASA Goals for Improved Aviation Safety, Environmental Compatibility and Performance Tuesday

1300

Hanover E

127-GTE-14

Innovations in Combustor Technology

Tuesday

1300

Hanover F

130-GTE-15

NASA Environmentally Responsible Aviation, propulsion technology

Tuesday

1300

Hanover G

162-GTE-17

Engine Performance

Tuesday

1600

Hanover G

163-GTE-18

Young Professionals’ Vision for the Future of Propulsion

Tuesday

1600

Regency V

168-GEPC-01/GTE-19 Alternative Aviation Fuel Experiments (AAFEX) I & II

Wednesday

0930

Roswell

171-GTE-20

Compressors III

Wednesday

0930

Hanover F

176-GTE-21

Pressure Gain Combustors

Wednesday

0930

Hanover G

187-GTE-22

AIAA and ASME IGTI Student Design Competition

Wednesday

0930

Regency V

199-ABPSI-13/GTE-23 Distributed Engine Controls

Wednesday

1400

Hanover C

202-GTE-24

Combustor Emissions

Wednesday

1400

Hanover F

206-GTE-25

Engine Compatibility, Testing, and CFD

Wednesday

1400

Hanover G

19-HR-01

Internal Ballistics Modeling I

Monday

1000

Inman

44-HR-02

Internal Ballistics Modeling II

Monday

1400

Inman

80-HR-03

Swirling Oxidizer Flows

Monday

1630

Inman

100-HR-04

Paraffin Fuels I

Tuesday

1000

University

122-HR-05

Ground Testing of Hybrid Motors

Tuesday

1300

University

152-HR-06

Fuel Regression Characterization

Tuesday

1600

University

184-HR-07

Novel Motor Operating Configurations I

Wednesday

0930

Inman

214-HR-08

Paraffin Fuels II

Wednesday

1400

Inman

211-HR-09

Novel Motor Operating Configurations II

Wednesday

1400

Piedmont

Hybrid Rocket Propulsion

High- Speed Air Breathing Propulsion 4-HSABP/HYP-01/PC-01

Constant Volume Combustion Engines

Monday

1000

Regency VII

32-HSABP/HYP-02

Numerical Simulation of Scramjets

Monday

1400

Regency VII

87-HSABP/HYP-03

Experimental Investigations in Supersonic Combustion

Tuesday

1000

Hanover E

88-HSABP/HYP-04

Supersonic Mixing / Injection I

Tuesday

1000

Regency VII

115-HSABP/HYP-05

Supersonic Mixing / Injection II

Tuesday

1300

Hanover D

116-HSABP/HYP-06

Supersonic Flameholding and Stability

Tuesday

1300

Regency VII

139-ABPSI-09/HSABP/HYP-07 High Speed Integrated Inlets

Tuesday

1600

Hanover C

164-HSABP/HYP-08/ABPSI-10 High-Speed Inlets / Isolators I

Tuesday

1600

Regency VII

167-HSABP/HYP-09/ABPSI-11 High-Speed Inlets / Isolators II

Wednesday

0930

Regency VII

200-HSABP/HYP-10

Numerical Modeling of Turbulent Combustion in Hypersonic Flows (Invited)

Wednesday

1400

Regency VII

18-LP-01

Injectors I

Monday

1000

Spring

21-LP-02

Monopropellants I

Monday

1000

Roswell

43-LP-04

Injectors II

Monday

1400

Spring

48-LP-05

Monopropellants II

Monday

1400

Roswell

55-LP-06

Turbopumps

Monday

1400 Piedmont

63-LP-07

Test Facility and Database Development

Monday

1630

Hanover A

65-LP-08

Injectors III

Monday

1630

Spring

70-LP-09

Control Methods for Liquid Rocket Engines

Monday

1630

Roswell

81-LP-10

Film Cooling

Monday

1630

Piedmont

Liquid Propulsion

28

General Conference Information Event at a Glance

Session ID

Session Title

Day

Start Time

Location

Liquid Propulsion continued 90-LP-11

CH4 Engines: Booster, Upper Stage, and Technology Demonstrators

Tuesday

1000

Inman

102-LP-12

Side Loads

Tuesday

1000

Vinnings

107-LP-13

Tanks I: Optimization and Control

Tuesday

1000

Roswell

109-LP-14

Transpiration Cooling and Cooling Channel Analysis

Tuesday

1000

Piedmont

119-LP-15

Cooling Techniques and Structural Analysis for Thermally Loaded Engines

Tuesday

1300

Spring

125-LP-16

Transient Processes in Orifices and Oxygen Dome

Tuesday

1300

Vinnings

132-LP-17

Tanks II: Optimization and Control

Tuesday

1300

Roswell

133-LP-18

Hydrogen Propulsion: Centaur-Saturn to J2X and Beyond

Tuesday

1300

Piedmont

146-LP-19

Combustion Instability I

Tuesday

1600

Spring

156-LP-20

Heat Tranfer, Cooling and Combustion of Methane Engines

Tuesday

1600

Vinnings

159-LP-21

Ignition of Methane and Hydrogen Engines

Tuesday

1600

Roswell

160-LP-22

Non-Conventional Concepts for Rocket Engines

Tuesday

1600

Piedmont

174-LP-23

Nozzle Design

Wednesday

0930

University

185-LP-24

Combustion Instability II

Wednesday

0930

Vinnings

209-LP-25

Tanks - Sloshing

Wednesday

1400

Vinnings

219-LP-26

In-Space and Upper Stage Propulsion Systems

Wednesday

1400

Roswell

Nuclear and Future Flight Propulsion 17-NFF-01

Future Flight Propulsion Systems I

Monday

1000

Hanover B

49-NFF-02

Nuclear Thermal Propulsion I: Fuels Development

Monday

1400

Hanover B

66-NFF-03

Future Flight Propulsion Systems II

Monday

1630

Regency VII

83-NFF-04

Future Flight Propulsion Systems III

Monday

1900

Hanover B

99-NFF-05

Nuclear Thermal Propulsion II: Engine Modeling

Tuesday

1000

Hanover D

154-NFF-06

Fusion and Alternative Nuclear Concepts

Tuesday

1600

Hanover E

186-NFF-07

Nuclear Thermal Propulsion III: Missions, Architectures and Affordability

Wednesday

0930

Piedmont

213-NFF-08

Nuclear Thermal Propulsion IV: Testing and Programmatics

Wednesday

1400

University

Propellants and Combustion 4-HSABP/HYP-01/PC-01


Monday

1000

Regency VII

5-PC-02

Spray Combustion I

Monday

1000

Hanover D

26-PC-03

Advanced Combustor Concepts I

Monday

1000

Hanover E

33-PC-04

Advanced Combustor Concepts II

Monday

1400

Hanover D

61-PC-06

Combustion Modeling I

Monday

1630

Hanover D

62-PC-07

Combustion Diagnostics

Monday

1630

Hanover E

94-PC-08

Rotating Detonation Engines

Tuesday

1000

Hanover A

101-PC-09

Fuels and Propellant Development

Tuesday

1000

Hanover B

118-PC-10

Combustion Studies I

Tuesday

1300

Hanover A

126-PC-11

Initation and Flame Characterization

Tuesday

1300

Hanover B

147-PC-12

Fundamental Combustion Processes

Tuesday

1600

Hanover B

153-PC-13

Combustion Modeling II

Tuesday

1600

Hanover D

175-PC-14

Combustion Studies II

Wednesday

0930

Hanover B

218-PC-15

Spray Combustion II

Wednesday

1400

Hanover B

117-SCP-01

Advanced Seal Technology I

Tuesday

1300

Inman

142-SCP-02

Advanced Seal Technology II

Tuesday

1600

Inman

System Concepts and Supporting Propulsion Technologies

29


Session Title

Day

Start Time

Location

System Concepts and Supporting Propulsion Technologies continued 177-SCP-03

Engineering and Analysis for Propulsion Systems I

Wednesday

0930

Hanover D

207-SCP-04

Engineering and Analysis for Propulsion Systems II

Wednesday

1400

Hanover D

210-SCP-05

Innovative Propulsion Systems

Wednesday

1400

Hanover E

11-SR-01

Solid Rocket Motor Combustion and Acoustic Instabilities I

Monday

1000

Techwood

25-SR-02

Controllable Solid Rocket Motors

Monday

1000

Vinnings

51-SR-03

Solid Rocket Motor Combustion and Acoustic Instabilities II

Monday

1400

Techwood

52-SR-04

Solid Fueled Scramjets and Ducted Rockets

Monday

1400

Vinnings

75-SR-05

Solid Rocket Motor Internal Ballistics Analysis

Monday

1630

Vinnings

104-SR-06

Solid Rocket Motor Propellant Combustion

Tuesday

1000

Techwood

131-SR-07

Solid Rocket Motor Ignition Evaluation and Design

Tuesday

1300

Techwood

161-SR-08

Solid Rocket Motor Burn Rate Analysis

Tuesday

1600

Techwood

188-SR-09

Solid Rocket Motor Development Experiences and History

Wednesday

0930

Spring

189-SR-10

Solid Rocket Motor Design and Optimization

Wednesday

0930

Techwood

216-SR-11

Solid Rocket Motor Nozzle and Case Design

Wednesday

1400

Spring

217-SR-12

Solid Rocket Motor Propellant Development

Wednesday

1400

Techwood

23-ST-01

NASA Space Launch System

Monday

1000

Regency V

76-ST-02

Space Transportation

Monday

1630

Techwood

Solid Rockets


10th International Energy Conversion Engineering Conference Special Sessions 1-RECPT-01


Sunday

1830

Exhibit Hall

2-JPC-01/IECEC-01

JPC/IECEC Opening Keynote Overview of NASA Major Program Thrusts and Technology Development Opportunities

Monday

0800


24-IECEC-02


Monday

1000

Dunwoody

29-LNCH-01


Monday

1200

Exhibit Hall

46-IECEC-03

Micro/Nano Thermal Management Technology for Aerospace, Energy and Environment

Monday

1400

Dunwoody

84-IECEC-05

IECEC Keynote Plenary: Aerospace Capabilities Applied To Solving Terrestrial Energy Problems...A University View Tuesday

0800 Dunwoody

103-IECEC-06

Solar Absorption and Desiccant Cooling Technologies for Air Conditioning in Sunny Countries

1000

111-IECEC-07

Robust and Resilient System Design Approaches for Next Generation Terrestrial Nuclear Energy Systems.

Tuesday

1000

Spring

112-IECEC-08

IECEC Awards Luncheon Keynote: Aerospace Capabilities Applied to Solving Terrestrial Energy Problems...A Federal Laboratory View

Tuesday

1200


158-IECEC-09

The Future of Smart Grid in the United States and Abroad

Tuesday

1600

Dunwoody

165-IECEC-10

IECEC Plenary Panel Aerospace Capabilities Applied to Solving Terrestrial Energy Problems...An Aerospace Industry View Wednesday 0800 Dunwoody

191-IECEC-11

The Latest Advances in Radioisotope Power Systems – A Mission Perspective

53-APS-01

Tuesday

Dunwoody

Wednesday

0930

Dunwoody

Spacecraft Solar Array Design

Monday

1400

Greenbriar

78-APS-02

Spacecraft Power System In-orbit Performance

Monday

1630

Greenbriar

105-APS-03

Spacecraft Power - Advanced Concepts and Designs

Tuesday

1000

Greenbriar

Aerospace Power Systems

30


Session Title

Day

Start Time

Location

Aerospace Power Systems continued 137-APS-04

Spacecraft Power System Design

Tuesday

1400

Greenbriar

190-APS-05

Spacecraft Power Electronics Design and Performance

Wednesday

0930

Greenbriar

196-APS-06

Power Technologies and Management for Aircraft and UAV

Wednesday

1300

Dunwoody

Energy Conversion Device Technology 6-EC-01

Advanced Energy Conversion Concepts

Monday

1000

Fairlie

79-EC-03

Sustainable Energy Conversion Systems

Monday

1630

Fairlie

106-EC-04

Stirling System Design and Optimization

Tuesday

1000

Fairlie

138-EC-05

Stirling/Radioisotope Power System Design, Modeling and Analysis

Tuesday

1400

Fairlie

198-EC-06

Stirling System Development

Wednesday

1300

Fairlie

Tuesday

1600

Fairlie

Energy Storage Technology 157-ES-01

High-Energy Storage for Space Application

12-EDGR-01

Demand Response and Smart Grid I

Monday

1000

Greenbriar

37-EDGR-02

Demand Response and Smart Grid II

Monday

1400

Lenox

Terrestrial Electricity Delivery & Grid Reliability

Terrestrial Energy-Efficient & Renewable Energy Systems 9-EERE-01

Combustion Systems

Monday

1000

Kennesaw

42-EERE-02

Energy-Efficient Systems I

Monday

1400

Kennesaw

67-EERE-03

Ground and Air Vehicle Systems

Monday

1630

Kennesaw

135-EERE-04

Fuels Production and Air Pollution Abatement

Tuesday

1400

Dunwoody

149-EERE-05

Energy-Efficient Systems II

Tuesday

1600

Greenbriar

197-EERE-06

Renewable Energy Generation Technologies

Wednesday

1300

Kennesaw

Terrestrial Fossil Energy Systems 8-TFES-01

Combustion Processes I

Monday

1000

The Learning Center

35-TFES-02

Combustion Processes II

Monday

1400

The Learning Center

96-TFES-03

Internal Combustion Engines

Tuesday

1000

Kennesaw

148-TFES-04

Emerging Fossil Energy Technologies

Tuesday

1600

Kennesaw

178-TFES-05

Fossil Energy Numerical Modeling

Wednesday

0930

Kennesaw

194-TFES-06

Gas Turbine Engines and Related Technologies

Wednesday

1300

Greenbriar

72-TNES-01

Nuclear Power Technologies and Fuels I

Monday

1630

The Learning Center

136-TNES-02

Nuclear Power Technologies and Fuels II

Tuesday

1400

Kennesaw

28-TM-01

Two Phase Thermal Control Technology

Monday

1000

Lenox

77-TM-02

Spacecraft and Lunar/Mars/Venus Surface Thermal Management

Monday

1630

Lenox

108-TM-03

Thermal Management of Machinery

Tuesday

1000

Lenox

134-TM-04

Aerospace and Terrestrial Power Systems Thermal Management I

Tuesday

1400

Lenox

143-TM-05

Aerospace and Terrestrial Power Systems Thermal Management II

Tuesday

1600

Lenox

172-TM-06

Aircraft, Aero-Engine and Hypersonic Vehicle Thermal Management

Wednesday

0930

Fairlie

181-TM-07

Heating and Cooling of Buildings

Wednesday

0930

Lenox

195-TM-08

Modeling, Simulation and Analysis of Thermal Systems

Wednesday

1300

Lenox

Terrestrial Nuclear Energy Systems

Thermal Management Technology

31

Convention CenterInformation Floor Plan General Conference

Hyatt Regency Atlanta

32

NASA Glenn Research Center, J. Felder, G. Brown, NASA Glenn Research Center, Cleveland, OH; J. Cleveland, OH Chu, NASA Langley Research Center, Hampton, VA; M. Tong, NASA Glenn Research Center, Cleveland, OH

East Lansing, MI; P. Akbari, Columbia University, New York, NY; J. Piechna, Warsaw University of Technology, Warsaw, Poland

York, NY; N. Mueller, Michigan State W. Stoddard, A. St. George, R. University, East Lansing, MI Driscoll, B. Romanchuk, E. Gutmark, University of Cincinnati, Cincinnati, OH

Chaired by: V. TANGIRALA, General Electric Company and D. DAUSEN, Naval Postgraduate School 1030 hrs 1100 hrs 1000 hrs AIAA-2012-3704 AIAA-2012-3705 AIAA-2012-3703 Development of a Wave Disk Thermodynamics of the Wave Experimental Optimization of Static Valveless Self-Aspiration Engine Experimental Facility Disk Engine N. Mueller, Michigan State University, P. Akbari, Columbia University, New of a Pulse Detonation Engine

Monday, 30 July 2012 4-HSABP/HYP-1/PC-1

JPC/IECEC Opening Monday Keynote

Monday


R. Driscoll, W. Stoddard, A. St. George, B. Romanchuk, D. Munday, E. Gutmark, University of Cincinnati, Cincinnati, OH

1130 hrs AIAA-2012-3706 Experimental Study of Shock Transfer in a Multiple Pulse Detonation-Crossover System


J. Chu, NASA Langley Research Center, Hampton, VA

1130 hrs Oral Presentation (Invited) Evaluation of the Propulsion Integration Aerodynamics on a Hybrid Wing Body Concept


Overview of NASA major program thrusts and Technology Development Opportunities Robert Lightfoot Associate Administrator NASA

Chaired by: H. KIM, NASA Glenn Research Center and A. GIBSON, Empirical Systems Aerospace LLC 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3700 AIAA-2012-3701 AIAA-2012-3702 Turboelectric Distributed Sensitivity of Mission Fuel Burn Hybrid Axial and Cross-Flow Propulsion System Modelling to Turboelectric Distributed Fan Propulsion for Transonic for Hybrid-Wing-Body Aircraft Propulsion Design Assumptions Blended Wing Body Aircraft C. Liu, Self, Cranfield, United on the N3-X Hybrid Wing Body J. Kummer, J. Allred, Propulsive Kingdom Wing, LLC, Elbridge, NY; J. Felder, Aircraft

Monday, 30 July 2012 3-ABPSI-1/GTE-1

Monday, 30 July 2012 2-JPC-1/IECEC-1 0800 - 0900 hrs

Sunday, 29 July 2012 1-RECPT-1 1830 - 2000 hrs

Sunday

Regency VII

Hanover C


Exhibit Hall

33

M. Briggs, M. Gibson, NASA Glenn Research Center, Cleveland, OH

C. Paiva, Self, California City, CA

California, Los Angeles, CA; M. Young, Air Force Research Laboratory, Edwards AFB, CA

Science Institute, Nagoya University, B. Dam, V. Ardha, M. de la Torre, Nagoya, Japan; A. Gupta, University N. Love, A. Choudhuri, University of of Maryland, College Park, College Texas, El Paso, El Paso, TX Park, MD

Chaired by: J. MEHTA and A. AGRAWAL, University of Alabama 1030 hrs 1000 hrs AIAA-2012-3718 AIAA-2012-3717 Effect of CO2 and H2O In-situ Spectroscopic Diluents on Radiative Heat Monitoring of Jatropha Oil Release Rates of Oxy-Fuel Combustion Properties N. Desmira, K. Kitagawa, Ecotopia Flames

Monday, 30 July 2012 8-TFES-1

H. Selim, A. Gupta, University of Maryland, College Park, College Park, MD; A. Al Shoaibi, Petroleum Institute, Abu Dhabi, United Arab Emirates

1100 hrs AIAA-2012-3719 Understanding the Quality of Sulfur Deposit Formation in a Claus Reactor

Chaired by: A. HOSANGADI, Combustion Research & Flow, Technology, Inc. 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3713 AIAA-2012-3714 AIAA-2012-3715 Nanopropulsion from HighUSAF High Energy Laser Phase-Change Thermal Energy Energy Particle Beams via (HEL) Systems: Multi-Spectral Storage and Conversion: Dispersion Forces in Nanotubes Algorithm Efficiencies Development and Analysis for F. Pinto, InterStellar Technologies Susceptibilities During Missile Solar Thermal Propulsion Corporation, Monrovia, CA D. Scharfe, ERC, Inc., Edwards AFB, Staging [Case: GHADR 110 CA; M. Gilpin, University of Southern MOD 2 (SEJIL-2)]

Monday, 30 July 2012 7-APC-1

Leighton, R. James, University of Minnesota, Minneapolis, Minneapolis, MN

Chaired by: D. WOLFORD, NASA Glenn Research Center and M. PISZCZOR, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3709 AIAA-2012-3710 AIAA-2012-3711 Energy Conversion by Multiferroic Concept of a Plasma-based Development Status of Phase Transformation Solar Cell the Fission Power System Y. Song, V. Srivastava, K. Bhatti, C. R. Adelhelm, Self, Freiburg, Germany Technology Demonstration Unit

Monday, 30 July 2012 6-EC-1

M. Raju, ASRC Aerospace C. Inoue, T. Watanabe, T. Himeno, Corporation, Cleveland, OH; D. S. Uzawa, University of Tokyo, Bulzan, NASA Glenn Research Center, Bunkyo, Japan Cleveland, OH

Chaired by: M. COIL, Orbital Technologies Corporation 1000 hrs 1030 hrs AIAA-2012-3707 AIAA-2012-3708 Theoretical Estimation Method Current Status of Superheat for Liquid Sheet Atomization Spray Modeling with NCC

Monday, 30 July 2012 5-PC-2

Combustion Processes I

G. Herdrich, R. Gabrielli, University of Stuttgart, Stuttgart, Germany

1130 hrs AIAA-2012-3716 Effect of Nuclear Side Reactions and Plasma Contamination on Magnetic Fusion Reactors in Space

Advanced Propulsion Concepts I

S. Moldenhauer, C. Holtmann, T. Stark, A. Thess, Ilmenau University of Technology, Ilmenau, Germany

1130 hrs AIAA-2012-3712 Theoretical and Experimental Investigations of the Pulse Tube Engine

Advanced Energy Conversion Concepts

Spray Combustion I

The Learning Center

Hanover A

Fairlie

Hanover D

34

and Technology, Fukuroi, Japan

J. Brossman, P. Ball, N. Smith, J. Methel, N. Key, Purdue University, West Lafayette, IN

B. Butler, V. Capece, University of Kentucky, Paducah, Paducah, KY

Q. Zhang, J. Li, W. Su, Y. Zhang, N. Wang, Beijing Institute of Technology, Beijing, China

Institute of Technology, Atlanta, GA

A. Blanquet, S. Duncan, D. Mavris, Georgia Institute of Technology, Atlanta, GA

Chaired by: T. HIKIHARA and S. DUNCAN 1030 hrs 1000 hrs AIAA-2012-3731 AIAA-2012-3730 A Game Theoretic Approach for A System Dynamics Model Smart Grid Demand Response of a Balancing Authority Using Demand Response as Using System Dynamics M. Miller, S. Duncan, D. Mavris, Georgia Contingent Energy Reserve

Monday, 30 July 2012 12-EDGR-1

D. Greatrix, Ryerson University, Toronto, Canada

T. Hikihara, K. Tashiro, Y. Kitamori, R. Takahashi, Kyoto University, Kyoto, Japan

1100 hrs AIAA-2012-3732 Power Packetization and Routing for Smart Management of Electricity

Chaired by: M. LANGHENRY, Raytheon Company and E. ORBEKK, Nammo AS 1000 hrs 1030 hrs AIAA-2012-3727 AIAA-2012-3729 Effect of Diminishing Studies on Effect of Head Particle Size on Solid Rocket Cavity on Resonance Damping Combustion Instability Characteristics in Solid Rocket Symptom Suppression Motors

Monday, 30 July 2012 11-SR-1

P. Schiffer, Technical University of Darmstadt, Darmstadt, Germany

1130 hrs AIAA-2012-3723 Experiments and Stochastic Simulations of Lignite Coal during Pyrolysis and Gasification

Demand Response and Smart Grid I

Solid Rocket Motor Combustion and Acoustic Instabilities I

Compressors I

Combustion Systems

S. Gollahalli, University of Oklahoma, I. Ahmed, A. Gupta, University of Norman, Norman, OK Maryland, College Park, College Park, MD

Chaired by: N. KEY, Purdue University and M. WOLFF, Wright State University 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3724 AIAA-2012-3725 AIAA-2012-3726 Shape of Characteristics of a The Sensitivity of Multistage Performance Measurements Transonic Compressor Compressor Performance to of a Low-Speed Single-Stage C. Pixberg, M. Müller, S. Leichtfuss, Inlet Boundary Conditions Axial-Flow Compressor

Monday, 30 July 2012 10-GTE-2

T. Ratul, R. Parthasarathy, S. Gollahalli, University of Oklahoma, Norman, Norman, OK

Chaired by: D. LILLEY, Oklahoma State University and A. GUPTA, University of Maryland 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3720 AIAA-2012-3721 AIAA-2012-3722 Experimental research on Combustion Characteristics Combustion Properties of biomass combustion by TGof Pool Fires of Biofuel/Jet Spray Flames of Butanol/ A Blends Jet A Blends at a Lean Global DTA/MS analysis N. Zhu, Shizuoka Institute of Science V. Tran, C. Morton, R. Parthasarathy, Equivalence Ratio

Monday, 30 July 2012 9-EERE-1

Greenbriar

Techwood

Hanover F

Kennesaw

35

High Power Electric Propulsion Systems Panel

Regency VI

Ground Test Requirements for High Power Electric Propulsion discussion led by Dr. Ira Katz, Ph.D. Electric Propulsion Group, Supervisor Jet Propulsion Laboratory

Power Electronics Requirements and Considerations for High Power Systems discussion led by Mr. Luis Pinero, P.E. Senior Engineer NASA Glenn Research Center

K. Kim, B. Kim, J. Yoh, Seoul National University, Seoul, South Korea

P. Giuliano, I. Boyd, University of Michigan, Ann Arbor, Ann Arbor, MI

North Ridgeville, OH; M. Swiatek, J. Yim, NASA Glenn Research Center, Cleveland, OH

K. Diamant, R. Spektor, E. Beiting, J. Young, T. Curtiss, The Aerospace Corporation, El Segundo, CA

Chaired by: K. DIAMANT, The Aerospace Corporation and V. KHAYMS, Lockheed Martin Corporation 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3735 AIAA-2012-3736 AIAA-2012-3737 The Effects of Background Analysis of a plasma test cell A Step Towards Electric Pressure on Hall Thruster including non-neutrality and Propulsion Testing Standards Operation complex collision mechanisms J. Dankanich, Gray Research, Inc.,

Monday, 30 July 2012 15-EP-2

L. Yang, Self, La Canada Flintridge, CA

Chaired by: B. POULSEN and K. RINK 1030 hrs 1000 hrs AIAA-2012-3733 AIAA-2012-3734 A particle level-set based Reaction Rate Analysis for Selected Solid-to-Solid-Reaction Eulerian method for simulating explosively driven metal pipe Pyrotechnic Compositions

Monday, 30 July 2012 14-ECS-1

EP Facility Effects

Energetic Materials: Modeling and Experimental Studies

Baker

University

The successful development and implementation of high power EP systems will necessitate closer coordination and communications among the Propulsion - Power - and Spacecraft Environmental Effects communities than historically has occurred. Bringing these communities together in this forum will initiate critical conversation, including: • Design considerations in implementation of SEP/Power Systems as related to potential SEP/array/spacecraft bus plasma interactions • Establishing ground test requirements for EP thrusters and systems that will ensure transportable results to the space environment • Ensuring a robust investment strategy in power electronics necessary to support high power EP systems development This Special Session provides the opportunity to facilitate the formulation of working groups in these key areas that may then provide advisory support to NASA and others as the community moves forward in SEP vehicle development and flight implementation.

SEP/High Voltage Arrays and Spacecraft Interactions discussion led by Dr. Thomas J. Curtiss, Ph.D. Propulsion Science Department, Director The Aerospace Corporation

The Panel Discussion will focus on the critical issues before us as related to the development of high power electric propulsion systems; in particular, considerations in the development and flight implementation of 30 kW class Solar Electric Propulsion (SEP) systems. These discussions will include:

Chaired by: M. PATTERSON, Seniro Technologist, NASA Glenn Research Center

Monday, 30 July 2012 13-EP-1 1000 - 1200 hrs

36

Research Center, Moffett Field, CA

B. Palaszewski, NASA Glenn Research Center, Cleveland, OH

C. Eberhart, D. Lineberry, R. Frederick, University of Alabama, Huntsville, Huntsville, AL

M. Faenza, M. Manente, D. Rondini, Y. Chen, National Space Organization University of Padova, Padova, Italy A. Bettella, D. Pavarin, University of Taiwan, Chubei, Taiwan Padova, Padova, Italy

Internal Ballistics Modeling I

V. Tian, B. McKeon, California Institute of Technology, Pasadena, CA; I. Leyva, Air Force Research Laboratory, Edwards AFB, CA

1130 hrs AIAA-2012-3807 Split Stream Flow Past a Blunt Trailing Edge with Application to Combustion Instabilities

Injectors I

S. Howe, Center for Space Nuclear Research, Idaho Falls, ID; D. Bedsun, D. Lee, M. Townsend, Nuclear Security Technologies, Las Vegas, NV; C. Cooper, J. Chapman, Desert Research Institute, Las Vegas, NV; M. Bulman, R. Samborsky, D. Brasuell, Aerojet, Sacramento, CA; S. Borowski, NASA Glenn Research Center, Cleveland, OH

Future Flight Propulsion Systems I 1130 hrs AIAA-2012-3743 Ground Testing a Nuclear Thermal Rocket: Design of a Subscale Demonstration Experiment

Chaired by: A. KARABEYOGLU, Space Propulsion Group, Inc. and J. MAJDALANI, University of Tennessee Space Institute 1030 hrs 1100 hrs 1000 hrs AIAA-2012-3749 AIAA-2012-3750 AIAA-2012-3748 Comparative CFD Simulations Combustion Modeling and Numerical Modeling of of Hybrid Rockets Flow Fields Analysis of Hybrid Rocket Paraffin-Based Fuels Behavior M. Lazzarin, N. Bellomo, F. Barato, Motor Internal Ballistics F. Barato, A. Bettella, D. Pavarin,

Monday, 30 July 2012 19-HR-1

University, Tainan, Taiwan S. Thakur, J. Wright, Streamline Numerics, Inc., Gainesville, FL; M. Ihme, University of Michigan, Ann Arbor, Ann Arbor, MI; K. Tucker, NASA Marshall Space Flight Center, Huntsville, AL

Chaired by: P. GLOYER, Gloyer-Taylor Laboratory and T. HINERMAN, Pratt & Whitney Rocketdyne 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3744 AIAA-2012-3745 AIAA-2012-3746 Simulation of a Shear Coaxial The impinging-type injector A Mechanistic Assessment of GO2/GH2 Rocket Injector with design of MMH/NTO liquid Swirl Injection and Atomization DES and LES Using Flamelet rocket engine by X-ray Radiographic and C. Chen, National Cheng Kung Models Optical Techniques

Monday, 30 July 2012 18-LP-1

Connecticut, Storrs, Storrs, CT

Chaired by: G. MEHOLIC, The Aerospace Corporation and B. PALASZEWSKI, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3740 AIAA-2012-3741 AIAA-2012-3742 Atmospheric Mining in the Power and Propulsion Options An Overview of the NASA Ames Millimeter-Wave Thermal Outer Solar System: Resource for Piloted Solar System Launch System Capturing, Storage, and Exploration B. Cassenti, University of D. Murakami, K. Parkin, NASA Ames Utilization

Monday, 30 July 2012 17-NFF-1

Inman

Spring

Hanover B

37

W. Neumaier, M. Wells, A. Brinkley, T. Talty, Dynetics, Huntsville, AL

T. Tachibana, Kyushu University, Kitakyushu, Japan

B. Henderson, J. Bridges, NASA Glenn Naval Research, Arlington, VA Research Center, Cleveland, OH

Monopropellants I

D. Long, Aero Systems Engineering, St. Paul, MN; R. Schlinker, R. Reba, United Technologies Research Center, East Hartford, CT

1130 hrs AIAA-2012-3753 The Structure of Near Field Pressure Fluctuations J. Doychak, B. Henderson, Office of Surrounding a Supersonic Jet

1100 hrs Oral Presentation (Invited) Department of Navy Jet Noise Reduction (JNR) Project

Jet Noise I

S. Nishikizawa, N. Suzuki, H. Sahara, Tokyo Metropolitan University, Tokyo, Japan; N. Miyashita, Y. Kuramoto, AXELSPACE, Tokyo, Japan

Monday, 30 July 2012 22-JPC-2 NASA MSFC National Institute for Rocket Propulsion Systems 1000 - 1200 hrs Moderator: Dr. Dale Thomas, Associate Director, Technical, NASA Marshall Space Flight Center Panelists: Julie Van Kleeck Charlie Precourt John Vilja Vigor Yang Vice President Vice President and General Manager Vice President Professor Space & Launch Systems Space Launch Division Strategy Innovation & Growth Georgia Institute of Technology Aerojet ATK Pratt & Whitney Rocketdyne

J. Aoyagi, H. Takegahara, Tokyo Metropolitan University, Hino, Japan; T. Nagata, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan

Chaired by: S. BUSHMAN, Johns Hopkins Uneiversity Applied Physics Laboratory and H. KAGAWA, Japan Aerospace Exploration Agency (JAXA) 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2012-3754 AIAA-2012-3755 AIAA-2012-3756 AIAA-2012-3757 Feasible Study on Low Frequency Development of a 90% One Newton thruster by Development of MonoPlasma Jet as Ignition System for Hydrogen Peroxide Monoplasma-assisted combustion of Propellant Propulsion System HAN Based Propellant Propellant Propulsion System HAN-based monopropellant for a Japanese Microsatellite T. Iizuka, M. Komatsu, T. Tajika, for the Warm Gas Test Article A. Kakami, K. Ideta, T. Ishibashi, ‘Hodoyoshi-1’


K. Kailasanath, Naval Research Laboratory, Washington, DC

Chaired by: B. KIEL, Air Force Reseach Laboratory 1000 hrs 1030 hrs AIAA-2012-3751 AIAA-2012-3752 Jet Noise Reduction Potential Fundamental Jet Noise from Emerging Variable Cycle Reduction Science and Technologies Technology


George F. Sowers, Ph.D. Vice President Business Development & Advanced Programs United Space Alliance


Roswell

Brett Alexander Director Strategy & Business Development Blue Origin

Hanover G

38

Garry M. Lyles SLS Chief Engineer NASA Marshcall Space Flight Center

Alex S. Priskos SLS Boosters Manager NASA Marshcall Space Flight Center

NASA Space Launch System

Michael (Mike) H. Kynard SLS Liquid Engines Manager NASA Marshcall Space Flight Center

Regency V


Dunwoody

C. Merkle, Purdue University, West H. Koizumi, Y. Masuda, University Lafayette, IN of Tokyo, Bunkyo, Japan; M. Nakano, Tokyo Metropolitan College of Industrial Technology, Arakawa, Japan; K. Komurasaki, Y. Arakawa, University of Tokyo, Bunkyo, Japan

Advanced Combustor Concepts I

Larry Price Deputy Program Manager, CEV Development Lockheed Martin Space Systems Company

Periagaram, J. Seitzman, T. Lieuwen, T. Zhang, Y. Yuan, J. Li, X. Fan, Georgia Institute of Technology, Chinese Academy of Sciences, Atlanta, GA Beijing, China

1130 hrs AIAA-2012-3762 Characteristics of a Supersonic Model Combustor with Two-Staged Injections of Supercritical Kerosene

Stephanie Bednarek Manager for Government Affairs SpaceX

Chaired by: E. LYNCH, Pratt & Whitney Rocketdyne and M. ANAND, Rolls-Royce Corporation 1030 hrs 1100 hrs 1000 hrs AIAA-2012-3760 AIAA-2012-3761 AIAA-2012-3759 Performance Improvement of Kinetic Modeling of Hypergolic Time-Averaged Characteristics Propellants Using Impinging of a Reacting Fuel Jet in a Laser-Ignition Micro Solid Element Injectors Vitiated Cross-Flow Rocket by Controlling the S. Sardeshmukh, S. Heister, G. Xia, R. Sullivan, B. Wilde, D. Noble, K. Combustion Wave Front


Dr. Merri Sanchez Senior Director Space Exploration Systems Sierra Nevada

Chris Singer Director of Engineering NASA Marshall Space Flight Center

Kent Rominger VP Strategy and Business, Space Launch Systems ATK Aerospace Systems Group, Utah Hanover E

The safe return of Space Shuttle Atlantis on July 21, 2011 marked the end of nearly 30 years of near-continuous American space exploration and achievements. Although this milestone marked the end of the Shuttle era, the future of American human spaceflight is far from bleak. In April, 2011, NASA awarded contracts to four commercial companies to continue development of commercial rockets and spacecraft capable of safely flying astronauts into orbit and to the International Space Station. In addition, NASA is making steady progress on building the Orion spacecraft, which is being designed to take astronauts deeper into space than ever before. The purpose of this session is to present the progress that is being made on several of these options, including highlighting the key technical drivers, achievements and challenges that each are facing as America heads into its next era of human spaceflight. Speakers:

Chaired by: P. ANDERSON, Lockheed Martin Space Systems

Monday, 30 July 2012 24-IECEC-2 1000 - 1200 hrs

Leaders from NASA’s Space Launch System (SLS) will participate in a panel discussing the progress made on the program’s propulsion systems. The SLS will be the nation’s next human-rated heavy-lift vehicle for entirely new missions beyond Earth’s orbit. With a first launch slated for 2017, the SLS Program is turning plans into progress, with the initial rocket being built in the U.S.A. today, engaging the aerospace workforce and infrastructure. Starting with an overview of the SLS mission and programmatic status, the discussion will then delve into progress on each of the primary SLS propulsion elements, including the boosters, core stage engines, and upper stage engines. Included will be a discussion of the 5-segment solid rocket motors (ATK), which are derived from Space Shuttle and Ares developments, as well as the RS-25 core stage engines from the Space Shuttle inventory and the J-2X upper stage engine now in testing (Pratt & Whitney Rocketdyne). The panel will respond to audience questions about this important national capability for human and scientific space exploration missions.

Todd A. May SLS Program Manager NASA Marshcall Space Flight Center

Moderator: Don Sauvageau, ATK Panelists:

Chaired by: D. SAUVAGEAU, ATK

Monday, 30 July 2012 23-ST-1 1000 - 1200 hrs

39

Empirical Systems Aerospace, Inc., Pismo Beach, CA

B. Schiltgen, M. Green, A. Gibson, D. Hall, D. Cummings, Empirical Systems Aerospace, Inc., Pismo Beach, CA; C. Hange, NASA Ames Research Center, Moffett Field, CA

P. Laskaridis, Cranfield University, Cranfield, United Kingdom

Chaired by: J. CHU, NASA Langley Research Center and P. PILIDIS, Cranfield 1430 hrs 1500 hrs 1400 hrs AIAA-2012-3769 AIAA-2012-3770 AIAA-2012-3768 Benefits and Concerns of Dynamic Response and High Analysis of a Distributed Cycle Fatigue Analysis of Fan Hybrid Propulsion System with Hybrid Electric Distributed Conventional Electric Machines Propulsion with Conventional Blades under Inlet Distortion M. Green, B. Schiltgen, A. Gibson, Electric Machines G. Doulgeris, G. Lelias, R. Singh,

Monday, 30 July 2012 31-ABPSI-2/GTE-4

Monday Afternoon Keynote

Monday, 30 July 2012 30-JPC-3 1300 - 1400 hrs

D. Trawick, C. Perullo, D. Mavris, Georgia Institute of Technology, Atlanta, GA

1530 hrs AIAA-2012-3771 Examining Non-Uniform Generator and Propulsor Control Schemes for a Hybrid Electric Propulsion Concept

Turboelectric Distributed Propulsion II

The Role of Propulsion Technology in Commercial Space Applications Antonio L. Elias Executive Vice President and General Manager Advanced Programs Group Orbital Sciences Corporation


Two Phase Thermal Control Technology

Monday, 30 July 2012 29-LNCH-1 1200 - 1300 hrs

S. Spencer, T. Hoang, R. Baldauff, R. Roberts, University of KwaZulu-Natal, M. Choi, NASA Goddard Space Flight Sutton, Naval Research Laboratory, Durban, South Africa Center, Greenbelt, MD Washington, DC

Chaired by: C. TARAU, Advanced Cooling Technologies and M. CHOI, NASA Goddard Space Flight Center 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3765 AIAA-2012-3766 AIAA-2012-3767 Progress on performance Phase Change Material for Performance Testing of validation of a steady-state Temperature Control of Loop Thermacore Loop Heat Pipe loop heat pipe model Heat Pipe Compensation in a 1kW Heat Transport/ M. Page, M. Brooks, C. Bemont, L. Chamber Rejection System

Monday, 30 July 2012 28-TM-1

Hanover C


Exhibit Hall

Lenox

40

P. Vogel, J. Edwards, North Carolina State University, Raleigh, NC

F. Malo-Molina, Air Force Research Laboratory, Wright-Patterson AFB, OH; H. Ebrahimi, FM&S, Reno, NV

B. Baird, S. Etemad, Precision Combustion, Inc., North Haven, CT

A. Ali, C. Rodriguez, A. Neely, J. Young, University of New South Wales at the Australian Defence Force Academy, Canberra, Australia

S. Verma, NAL Research Corporation, Bangalore, India; R. Stark, O. Haidn, German Aerospace Center (DLR), Hardthausen, Germany

Chaired by: T. CHEN and J. ROBINSON 1400 hrs 1430 hrs AIAA-2012-3780 AIAA-2012-3782 Combination of Fluidic Thrust Effect of Ambient Pressure Modulation and Vectoring in a Fluctuations on the Dual-Bell 2D Nozzle Transition Behavior

Monday, 30 July 2012 34-APC-2

S. Etheridge, J. Lee, University of Cincinnati, Cincinnati, OH; C. Carter, Air Force Research Laboratory, Wright-Patterson AFB, OH

Irvine, Irvine, CA

M. Fukunari, A. Arnault, T. Yamaguchi, K. Komurasaki, University of Tokyo, Kashiwa, Japan; H. Koizumi, Y. Arakawa, University of Tokyo, Bunkyo, Japan; I. Funaki, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; H. Katsurayama, Yamaguchi University, Ube, Japan

1500 hrs AIAA-2012-3783 Preliminary Trajectory Analysis of Microwave Rocket with Reed Valve Air Breathing System

Advanced Propulsion Concepts II

A. Briones, University of Dayton Research Institute, Dayton, OH; B. Sekar, Air Force Research Laboratory, Wright-Patterson AFB, OH; H. Thornburg, High Performance Technologies, Inc., Reston, VA

Advanced Combustor Concepts II

J. Liu, Taitech, Inc., Wright-Patterson AFB, OH; M. Brown, Air Force Research Laboratory, WrightPatterson AFB, OH

1530 hrs AIAA-2012-3775 Radiative Heating in Hydrocarbon-fueled Scramjet Engines

Numerical Simulation of Scramjets

Chaired by: K. MCMANUS, General Electric Company and P. VENKATESWARAN, Georgia Institute of Technology 1430 hrs 1500 hrs 1530 hrs 1400 hrs AIAA-2012-3776 AIAA-2012-3777 AIAA-2012-3778 AIAA-2012-3779 Characterization of Supersonic Novel Glow Plug for Compact Turbine-Burner Model: Cavity Modeling and Simulation of High Density Engine Flameholding in a Converging, Enhanced Reactant-Product Flow Interaction with Turning Channel Flow Mixing in Ultra Compact Shockwaves Using Laser-based Applications Operating on W. Sirignano, University of California, Combustors Diagnostics Heavy Fuels


University, Columbus, OH

Chaired by: F. MALO-MOLINA, Air Force Reseach Laboratory and L. MCKINNEY, McKinney Associates 1400 hrs 1430 hrs 1500 hrs AIAA-2012-3772 AIAA-2012-3773 AIAA-2012-3774 Exploratory Simulations of the Numerical Simulation of a High Fidelity Analysis of a HIFiRE 2 Scramjet Flowpath Hypervelocity Scramjet Engine Reacting Pulsed Supersonic R. Yentsch, D. Gaitonde, Ohio State Using Silane - Hydrogen Fuel Combustor

Monday, 30 July 2012 32-HSABP/HYP-2

Hanover A

Hanover D

Regency VII

41

H. Abdul-Rahman, F. Jaberi, Michigan Paso, El Paso, TX State University, East Lansing, MI; A. Khalil, A. Gupta, University of Maryland, College Park, College Park, MD

Combustion Processes II

J. Kim, S. Duncan, D. Mavris, Georgia Institute of Technology, Atlanta, GA

France (ERDF), Paris, France

Chaired by: S. DUNCAN and T. HIKIHARA 1400 hrs 1430 hrs AIAA-2012-3787 Oral Presentation (Invited) Deterioration Process Modeling Building of the European of a Multi-Component Complex SmartGrids : The European System for a Condition Based Electricity Grid Initiative (EEGI) A. Vu, Électricité Réseau Distribution Maintenance

Monday, 30 July 2012 37-EDGR-2

E. Ortjoahnn, P. Wirasanti, M. Hoppe, South Westphalia University of Applied Sciences, Soest, Germany

1500 hrs Oral Presentation (Invited) Multi-Level Cluster Approach - The Flexible and Adaptive Strategy for Smart Grid

Demand Response and Smart Grid II

Lenox


The Learning Center

Frank Culbertson Senior Vice President and Deputy General Manager Human Spaceflight Systems Orbital Sciences

John Mulholland Vice President & Program Manager Commercial Programs, Space Exploration The Boeing Company

Charles Precourt Vice President & General Manager Space Launch Division ATK

George Sowers Vice President Business Development ULA

Brett Alexander Director Business Development & Strategy Blue Origin, LLC

Adam Harris Vice President Government Sales SpaceX

Moderator: Michael Griffin, AIAA President, Former NASA Administrator Lisa Matthews Business Development Director Propulsion, Space Systems Group Sierra Nevada

Monday, 30 July 2012 36-JPC-4 Commercial Space Development 1400 - 1620 hrs Join this panel of commercial space leaders in an interactive discussion of commercial space developments and future space plans. We will address current issues and consider future strategies and opportunities

Love, A. Choudhuri, University of Texas, El Paso, El Paso, TX

Chaired by: N. LOVE, The University of Texas, El Paso and A. AGRAWAL, University of Alabama 1400 hrs 1430 hrs 1500 hrs AIAA-2012-3784 AIAA-2012-3785 AIAA-2012-3786 Numerical and Experimental Characterization of Oxy-Fuel Design and Development of Study of Turbulent Mixing and Flames in a Swirl Combustor an Optically Accessible High Reaction in Colorless Distributed V. Ardha, B. Dam, N. Love, A. Pressure Combustor Choudhuri, University of Texas, El S. Sarker, J. Nunez, C. Valdez, N. Combustion Systems

Monday, 30 July 2012 35-TFES-2

42

I. Mikellides, I. Katz, R. Hofer, D. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

Y. Hayakawa, K. Miyazaki, H. Nagano, Y. Ohkawa, T. Higuchi, S. Kitamura, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan

I. Funaki, H. Watanabe, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; M. Nakano, Tokyo Metropolitan College of Industrial Technology, Arakawa, Japan; Y. Kajimura, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; T. Miyasaka, Gifu University, Gifu, Japan; Y. Nakayama, National Defense Academy, Yokosuka, Japan; H. Kuninaka, I. Shinohara, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan

1500 hrs AIAA-2012-4291 Modeling of an Ionic Liquid Electrospray using Molecular Dynamics

B. Prince, S. Miller, Air Force A. Borner, R. Kumar, Z. Li, D. Levin, Research Laboratory, Kirtland AFB, Pennsylvania State University, NM; J. Rovey, Missouri University of University Park, PA Science and Technology, Rolla, MO

1430 hrs AIAA-2012-3738 Capillary Extraction of the Ionic Liquid [Bmim][DCA] for Variable Flow Rate Operations

Ion Thrusters I

Electrospray Propulsion I

N. Yamamoto, H. Nakashima, Kyushu University, Kasuga, Japan; A. Yalin, Colorado State University, Fort Collins, CO

1530 hrs AIAA-2012-3791 Dependence of lifetime on magnetic field configuration in a Hall thruster

Hall Thrusters I

J. Foster, S. Gucker, A. Hubble, University of Michigan, Ann Arbor, Ann Arbor, MI; P. Peterson, ElectroDynamic Applications, Inc., Ann Arbor, MI

M. Patterson, D. Herman, NASA Glenn Research Center, Cleveland, OH; J. Foster, University of Michigan, Ann Arbor, Ann Arbor, MI

Chaired by: D. GOEBEL, Jet Propulsion Laboratory, California Institute of Technology and L. KING, Michigan Technological Univers 1430 hrs 1500 hrs 1530 hrs 1400 hrs AIAA-2012-3796 AIAA-2012-3797 AIAA-2012-3798 AIAA-2012-3795 Performance Characterization An Experimental Study of Numerical Lifetime Evaluation Annular-Geometry Ion Engine: of a 50 cm Ion Thruster Single Cathode Gridded Ion of Ion Thruster’s Ion Optics Concept, Development Status, Discharge Chamber Thrusters Using the JIEDI Tool and Preliminary Performance


T. Coles, P. Lozano, T. Fedkiw, Massachusetts Institute of Technology, Cambridge, MA; N. Takahashi, German Aerospace Center (DLR), Stuttgart, Germany

Chaired by: V. HRUBY 1400 hrs AIAA-2012-3793 Investigating Ion Fragmentation in Electrospray Thruster Beams


I. Katz, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

Chaired by: H. KAMHAWI, NASA Glenn Research Center and W. HOSKINS, Aerojet 1400 hrs 1430 hrs 1500 hrs AIAA-2012-3788 AIAA-2012-3789 AIAA-2012-3790 Design of a Laboratory Hall Potential Contours in Ion Design of a Laboratory Hall Thruster with Magnetically Focusing Hall Thruster Thruster with Magnetically Shielded Channel Walls, Phase Shielded Channel Walls, Phase K. Xu, H. Dao, M. Walker, Georgia II: Experiments III: Comparison of Theory with Institute of Technology, Atlanta, GA R. Hofer, D. Goebel, I. Mikellides, Experiment


Cortland

Baker

Regency VI

43

W. Sanborn, R. McCoy, Pacific Scientific Energetic Materials Company, Chandler, AZ

A. Masoud, A. Ibrahim, E. Khalil, Cairo University, Cairo, Egypt

Gainesville, Gainesville, FL; E. Khalil, Cairo University, Cairo, Egypt

D. Bianchi, F. Nasuti, University of Rome “La Sapienza”, Rome, Italy

of Tennessee Space Institute, Tullahoma, TN

Chaired by: S. FROLIK, The Aerospace Corporation and B. EVANS, Space Propulsion Group, Inc. 1430 hrs 1400 hrs AIAA-2012-3810 AIAA-2012-3809 Numerical Analysis of Nozzle Linear Stability Study of Cylindrically-Shaped Hybrid Material Thermochemical Rockets Erosion in Hybrid Rocket T. Elliott, J. Majdalani, University Engines


M. Zirakssaz, I.A. University, Tehran, Iran; F. Ommi, Tarbiat Modares University, Tehran, Iran; D. Ganji, Babol University, Babol, Iran; M. Ashjaee, Tehran University, Tehran, Iran

Chaired by: T. HINERMAN, Pratt & Whitney Rocketdyne and P. GLOYER, Gloyer-Taylor Laboratory 1400 hrs AIAA-2012-3747 Experimental Evaluation of a Reverse Engineering Swirl Atomizer


Chaired by: J. DARKWA, University of Nottingham-Ningbo and T. BRADLEY, Colorado State University 1400 hrs 1430 hrs 1500 hrs AIAA-2012-3803 AIAA-2012-3804 AIAA-2012-3805 Energy Efficiency in Buildings: Improvement of Natural Pulsed Ejector Cooling System S. du Clou, M. Brooks, University of Think Pyramids Ventilation in South-Facing E. Khalil, Cairo University, Cairo, Egypt Rooms Located in Top Floors in KwaZulu-Natal, Durban, South Africa; W. Lear, S. Sherif, University of Florida, Cairo, Egypt


Tech, Pipersville, PA; R. Saulsberry, Texas Tech University, Lubbock, TX S. McDougle, NASA White Sands Test Facility, Las Cruces, NM

Chaired by: D. JACKSON, ATK and H. LEE, Chemring Energetic Devices 1400 hrs 1430 hrs 1500 hrs AIAA-2012-3799 AIAA-2012-3800 AIAA-2012-3801 Analyzing the Effects of The Investigation of a Low Failure Mode Analysis of Electromagnetic Exposure on Pressure Anomaly in a V-Shaped Pyrotechnically Energetic Compositions Pressure Cartridge Containing Actuated Valves J. Sachdev, A. Hosangadi, CRAFT C. Crane, M. Pantoya, B. Weeks, a Double-Base Propellant

Monday, 30 July 2012 41-ECS-2

Internal Ballistics Modeling II

Injectors II

N. Ghaddar, K. Ghali, M. Abiad, American University of Beirut, Beirut, Lebanon

1530 hrs AIAA-2012-3806 Feasibility Study of Localized Heating and Cooling Systems Totally Powered by Solar Energy

Energy-Efficient Systems I

T. Blachowski, J. Burchett, Naval Surface Warfare Center, Alexandria, VA

1530 hrs AIAA-2012-3802 2012 CAD/PAD Technology Roadmap Update

Energetic Material Applications

Inman

Spring

Kennesaw

University

44

Provence, France


Propulsion systems modeling and design

Dunwoody

Hanover F

Group, Solna, Sweden J. Lee, D. Jang, S. Kwon, Korea Advanced Institute of Science and Technology, Daejeon, South Korea

R. Masse, R. Spores, Aerojet, Redmond, WA

1500-1530 hrs Rama Venkatasubramanian RTI International, Research Triangle Park, NC Monopropellants II

1530 hrs AIAA-2012-4335 A New State-of-The-Art in AFM315E Thruster Technologies

1430-1500 hrs Theodorian Borca-Tasciuc Rensselaer Polytechnic Institute, Troy, NY

Chaired by: S. MILLER, Aerojet and S. BUSHMAN, Johns Hopkins University Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs AIAA-2012-3815 AIAA-2012-3817 AIAA-2012-3818 A Family of Thrusters for Life Test Results for a New 4N Performance Improvement ADN-Based Monopropellant (1 lbf) Thrust Class Hydrazine of Hydrogen Peroxide LMP-103S Monopropellant Engine Monopropellant by Blending M. Persson, K. Anflo, A. Dinardi, SSC O. Morgan, Aerojet, Redmond, WA Ethanol


1400-1430 hrs Timothy Fisher Purdue University, West Lafayette, IN


1530-1500 hrs Gerald Mahan Penn State University, State College, PA Roswell

The micro/nano-scale thermal management technologies in this panel session include, but are not limited to, heat and mass transport issues in the following materials, components or systems: carbon nanotube, high temperature nanofibers, ceramics, aerogel insulation, thermal energy storage, microcooler, nanopropellants, propulsion systems, in-space propulsion, solar-electrical conversion, solar-fuel conversion, thermoelectric energy conversion, magnetocaloric energy conversion, pyroelectric energy conversion, piezoelectric energy conversion, electrochemical energy conversion and storage, chip scale spot cooling and waste heat recovery. A panel of experts will discuss the emerging micro/nano-scale thermal management technologies for aerospace, energy and environment, and offer their vision for the future of these technologies. Focus will be placed on challenges and opportunities.

Chaired by: M. CHOI, NASA Goddard Space Flight Center

Monday, 30 July 2012 46-IECEC-3 1400 - 1600 hrs

J. Schutte, J. Tai, D. Mavris, Aerospace Systems Design Laboratory, Atlanta, GA N. Molino, J. Sands, S. Duncan, E. Osvalds, D. Mavris, Georgia Institute of Technology, Atlanta, GA

1500 hrs AIAA-2012-3814 Improved Pareto Optimal Engine Cycle Designs Through the Use of a New Pareto France; P. Basset, ONERA, Salon-de- Quality Indicator

Chaired by: J. TAI, Georgia Institute of Technology 1400 hrs 1430 hrs AIAA-2012-3812 AIAA-2012-3813 Turboshaft Engine Predesign Multi Design Point Cycle Design Incorporation into the and Performance Assessment Environmental Design Space S. Burguburu, ONERA, Meudon,


45

M. Trammell, L. Qualls, Oak Ridge National Laboratory, Oak Ridge, TN

S. Xing, W. Zhijun, Q. Zhang, Z. Yandong, L. Junwei, N. Wang, Beijing Institute of Technology, Beijing, China

R. Claus, NASA Glenn Research Center, Cleveland, OH

G. Kurth, MBDA, Aschau am Inn, Germany

D. MacInnis, Raytheon Company, Tucson, AZ

A. Kamisaka, K. Takahashi, T. Kuwahara, Nihon University, Funabashi, Japan

Chaired by: K. NAUMANN, Bayern-Chemie GmbH and D. MACINNIS, Raytheon Company 1430 hrs 1500 hrs 1400 hrs AIAA-2012-3828 AIAA-2012-3829 AIAA-2012-3827 Effects of Gas Generator Burn Effects of the Distance of High Development of a 6-DoF Rate Variability on Variable Temperature Metal Particles Simulation of a VFDR Flow Ducted Rocket Design in a Secondary Combustor of Propulsion System C. Bauer, N. Hopfe, P. Caldas-Pinto, and Performance Ducted Rockets


University of Rome “La Sapienza”, Estivalezes, ONERA, Toulouse, France Rome, Italy; F. Serraglia, ESA, Rome, Italy; M. Di Giacinto, University of Rome “La Sapienza”, Rome, Italy

Jet Noise II

Nuclear Thermal Propulsion I: Fuels Development

X. Pei, J. Liu, W. Zhijun, N. Wang, Beijing Institute of Technology, Beijing, China

1530 hrs AIAA-2012-3830 Numerical Investigation on Cavity Length for Solid Fuel Scramjet

Solid Fueled Scramjets and Ducted Rockets

Solid Rocket Motor Combustion and Acoustic Instabilities II

1500 hrs AIAA-2012-3823 Aeroacoustic and Performance Simulations of a Test Scale Open Rotor

Chaired by: D. GREATRIX, Ryerson University and J. SPURLING, Naval Air Warfare Center Weapons Division 1400 hrs 1430 hrs 1500 hrs AIAA-2012-3824 AIAA-2012-3825 AIAA-2012-3826 Pressure oscillation numerical Theoretical Investigation of the The Influence of Thermal simulation in solid propellant Parietal Vortex Shedding in Inhibitor Position on Pressure rocket motor Solid Rocket Motors Oscillations in Solid Rocket E. Cavallini, V. Ferretti, B. Favini, B. Germain, G. Casalis, J. Motors: Numerical Study


P. Morris, N. Sikarwar, Pennsylvania Z. Berger, K. Low, Syracuse State University, University Park, PA University, Syracuse, NY; S. Kostka, S. Gogineni, Spectral Energies, LLC, Dayton, OH; M. Glauser, Syracuse University, Syracuse, NY

Chaired by: B. KIEL, Air Force Reseach Laboratory 1400 hrs 1430 hrs AIAA-2012-3821 AIAA-2012-3822 Adjoint Design Methods for Investigation of an Axisymmetric Nozzles for Reduced Noise in Transonic Jet with High High-Speed Jets Resolution Time-Resolved PIV


R. Hickman, NASA Marshall Space Flight Center, Huntsville, AL; J. Broadway, O. Mireles,

Chaired by: J. WARREN, NASA Headquarters and S. BOROWSKI, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2012-3819 Oral Presentation (Invited) Recapturing Graphite-Based Fabrication and Testing of Fuel Element Technology for CERMET Fuel Materials for Nuclear Thermal Propulsion Nuclear Thermal Propulsion


Vinnings

Techwood

Hanover G

Hanover B

46

G. Lam, C. Su, D. Leland, Lockheed Martin Corporation, Sunnyvale, CA

Institute of Technology, Pasadena, CA; B. Smith, The Aerospace Corporation, El Segundo, CA

Charlie Stevens Air Force Research Laboratory

L. Oliveira, H. Muñoz, F. Catalano, M. Fukunari, R. Komatsu, S. Saitoh, University of São Paulo, São Carlos, T. Yamaguchi, K. Komurasaki, Brazil University of Tokyo, Chiba, Japan; Y. Oda, K. Sakamoto, Japan Atomic Energy Agency, Naka, Japan

Mike Dunn Ohio State University

M. Polanka, B. Smith, Air Force Institute of Technology, WrightPatterson AFB, OH

Chaired by: W. WESTPHAL, Rolls-Royce Corporation and D. BENCHERGUI, Bombardier Inc 1630 hrs 1700 hrs 1730 hrs AIAA-2012-3837 AIAA-2012-3838 AIAA-2012-3839 Scaling Study of Wave Rotor Aerodynamic Analysis of High Thrust Augmentation Using Turbo Normalization of an Rotation and Low Reynolds High Power Beam and Reed Internal Combustion Engine Number Propeller valve Air-breathing System

Monday, 30 July 2012 57-ABPSI-3

Panelists:

Chaired by: A. NIX, West Virginia University

Monday, 30 July 2012 56-GTE-7 1400 - 1600 hrs

Numerics, Inc., Gainesville, FL; E. Luke, P. Alliot, J. Vigouroux, SNECMA, Exploration Agency (JAXA), Tsukuba, Mississippi State University, Starkville, Vernon, France; B. Pouffary, French Japan; A. Okayasu, S. Shimizu, MS; J. West, NASA Marshall Space Space Agency (CNES), Paris, France ASIRI, Mitaka, Japan Flight Center, Huntsville, AL

Chaired by: B. WINTERS, Orbital Sciences Corporation and B. MARCU, SpaceX 1400 hrs 1430 hrs 1500 hrs AIAA-2012-3834 AIAA-2012-3835 AIAA-2012-3836 Development of a Robust and Major achievements reached Experimental Results of a Efficient Parallel Solver for through the LAPLACE-BCER Centrifugal Pump Using Unsteady Turbomachinery Flows cavitation test turbopump Hydrazine and MON-3 J. Wright, S. Thakur, Streamline H. Kagawa, Japan Aerospace program


Hopkins University Applied Physics Laboratory, Laurel, MD

Mark Zelesky Pratt & Whitney

PDEs, ICEs, and Propellers

Allan van de Wall GE Aviation

Operation of Gas Turbine Engines in Volcanic Ash Environments

Volcanic Ash

J. Smyth, J. Bindon, M. Brooks, G. Smith, University of KwaZulu-Natal, Durban, South Africa; G. Snedden, Council for Scientific and Industrial Research, Pretoria, South Africa

Turbopumps

Spacecraft Solar Array Design

1530 hrs AIAA-2012-3763 The Design of a Kerosene Turbopump for a South African Commercial Launch Vehicle

Chaired by: R. CHAMBERS, Lockheed Martin Corporation and A. ARASTU, The Boeing Company 1400 hrs 1430 hrs 1500 hrs AIAA-2012-3831 AIAA-2012-3832 AIAA-2012-3833 Solar Panel Design and JUNO Photovoltaic Power at Solar Probe Plus (SPP) Jupiter Autonomous Solar Array Angle Qualification for the Mars S. Dawson, P. Stella, W. McAlpine, Atmosphere and Volatile Control A. Baisden, L. Roufberg, Johns EvolutioN (MAVEN) Program Jet Propulsion Laboratory, California

Monday, 30 July 2012 53-APS-1

John Sordyl Williams International

John Fisher Federal Aviation Administration

Hanover B

Regency V

Piedmont

Greenbriar

47

F. Ebersohn, S. Girimaji, Texas A&M University, College Station, TX; J. Shebalin, NASA Johnson Space Center, Houston, TX; D. Staack, Texas A&M University, College Station, TX

J. Little, E. Choueiri, Princeton University, Princeton, NJ

Why Turboelectric Distributed Propulsion

Technical University of Madrid, Madrid, Spain

University of Tokyo, Tokyo, Japan

J. Schmidt, S. Kostka, S. Roy, Spectral Energies, LLC, Dayton, OH; J. Gord, B. Ganguly, Air Force Research Laboratory, Wright-Patterson AFB, OH

Chaired by: C. BROPHY, Naval Postgraduate School 1630 hrs 1700 hrs AIAA-2012-3846 AIAA-2012-3847 Effect of Electron Injection KHz particle-image velocimetry for Soot Suppression in and emission measurements Hydrocarbon Flames of induced turbulence in J. Suzuki, H. Horisawa, Y. premixed propane/air flame Matsuzawa, Tokai University, by millisecond pulsed currentKanagawa, Japan; I. Kimura, voltage


C. Sohn, H. Choi, Sejong University, Seoul, South Korea

Y. Yuan, M. Yang, T. Zhang, G. Yu, X. Fan, Chinese Academy of Sciences, Beijing, China

1730 hrs AIAA-2012-3848 Visualization of Vaporized Kerosene Combustion in a Supersonic Combustor Using Pulsed Schlieren System

Chaired by: T. NGUYEN, Aerojet and C. BRUNO, University ‘La Sapienza’ 1700 hrs 1630 hrs AIAA-2012-3844 AIAA-2012-3845 Surrogate Model Design for A Numerical Study on Combustion-Stability Rating GtL Kerosene of Impinging-Jet Injectors in a N. Slavinskaya, German Aerospace Center (DLR), Stuttgart, Germany Subscale Chamber


Combustion Diagnostics

Combustion Modeling I

Rich Ouellette Prof. Pericles Pilidis John Kinney Director, Advanced Programs Business Development Advanced Technology Concepts Project Manager Head of Power and Propulsion Department NASA Program Manager, GE Aviation Boeing Research & Technology Group,Huntington Cranfield University, United Kingdom Cincinnati, OH Beach, CA

Speakers:

Chaired by: H. KIM, NASA Glenn Research Center and N. MADAVAN, NASA Ames Research Center

Monday, 30 July 2012 59-ABPSI-4/GTE-8 1630 - 1830 hrs

J. Navarro, M. Merino-Martinez, E. Ahedo, Technical University of Madrid, Madrid, Spain

Electromagnetic Propulsion I

Chaired by: R. THOMAS, NASA Glenn Research Centernand K. POLZIN, NASA Marshall Space Flight Center 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2012-3840 AIAA-2012-3841 AIAA-2012-3842 AIAA-2012-3843 Towards Computation of Resistive Large-beta effects on the Magnetic Nozzle Far-Field Fluid and Hybrid-PIC Code Magnetohydrodynamic Magnetic magnetic detachment of a Simulation Comparison of the Plasma M. Merino-Martinez, E. Ahedo, Nozzle Plasma Flow supersonic plasma flow Plume in a Magnetic Nozzle


Andrew Gibson President, Empirical Systems Aerospace, Inc. Pismo Beach, CA

Hanover C

Hanover E

Hanover D

James Felder Aerospace Engineer NASA Glenn Research Center Cleveland, OH

Regency V

48

F. Pineda, J. Betancourt-Roque, A. Choudhuri, University of Texas, El Paso, El Paso, TX

H. Kamhawi, T. Haag, W. Huang, R. Shastry, T. Peterson, NASA Glenn Research Center, Cleveland, OH

L. Brieda, Particle In Cell Consulting, Falls Church, VA; M. Keidar, George Washington University, Washington, DC

Studies at Austin, Austin, TX

J. Woodward, California State University, Fullerton, CA

H. Brito, C. Dominguez, R. De Alessandro, E. Galian, Aeronautical University Institute, Cordoba, Argentina

Future Flight Propulsion Systems II

J. Yoon, Y. Yoon, Seoul National University, Seoul, South Korea

Chaired by: G. MEHOLIC, The Aerospace Corporation and M. MILLIS, Tau Zero Foundation 1700 hrs 1730 hrs 1630 hrs AIAA-2012-3861 AIAA-2012-3862 AIAA-2012-3860 Recent Results of an RAMA Experiment - Persistence Faster-Than-Light Space of Anomalous Thrusting Effects Warps, Status and Next Steps Investigation of Mach Effect E. Davis, Institute for Advanced Thrusters Using Laser Vibration Sensing


Sanchez, A. Choudhuri, University of D. Suslov, J. Deeken, German Aerospace University of Munich, Garching, Texas, El Paso, El Paso, TX Germany Center (DLR), Lampoldshausen, Germany; O. Haidn, Technical University of Munich, Garching, Germany

1800 hrs AIAA-2012-3859 Study on Self-Pulsation Characteristics of Gas/Liquid Shear Coaxial Injector with Annular Liquid Sheets

Injectors III

Hall Thrusters II

D. Sugimori, T. Ueda, H. Nanri, Japan Aerospace Exploration Agency R. Doreswamy, NASA Marshall Space (JAXA), Kakuda, Japan; T. Kanno, Flight Center, Huntsville, AL T. Shibasaki, KANNO Information System, Kakuda, Japan

Chaired by: J. LOCKE, United Technologies Research Center and D. PRECLIK, Astrium, an EADS Company 1630 hrs 1700 hrs 1730 hrs AIAA-2012-3856 AIAA-2012-3857 AIAA-2012-3858 High Pressure Optically Investigation of the APIInteraction of Acoustic Pressure Accessible Rocket Combustor Injection Concept in a LOX/LH2 Fluctuations with Supercritical Testing and Evaluation Combustion Chamber at GG/PB Nitrogen Jets C. Navarro, J. Betancourt-Roque, L. Operation Conditions M. Schmid, T. Sattelmayer, Technical


J. Szabo, B. Pote, M. Robin, S. Paintal, Busek Company, Inc., Bedford, MA

Test Facility and Database Development 1800 hrs AIAA-2012-3852 A review of Propulsion Industrial Base Studies and an Introduction to the National Institute of Rocket Propulsion Systems

Chaired by: M. NAKLES, Air Force Research Institute and M. COLETTI, University of Southampton 1630 hrs 1700 hrs 1730 hrs AIAA-2012-3853 AIAA-2012-3854 AIAA-2012-4015 High Density Hall Thruster Overview of the High Voltage Hall Thruster Analysis Using a Propellant Investigations Hall Accelerator Project Multiscale Approach


Aerospace Exploration Agency (JAXA), Kakuda, Japan

Chaired by: D. COOTE, NASA Stennis Space Center and D. LINEBERRY, University of Alabama, Huntsville 1630 hrs 1700 hrs 1730 hrs AIAA-2012-3849 AIAA-2012-3850 AIAA-2012-3851 Cryogenic Propellant Development and Utilization Conceptual Study on Rocket Engine Test Facility for Higher Delivery and Controls Facility of Rocket Engine Test Database Development for LOX/ (REDAK) in Japan Aerospace Operability T. Ueda, N. Nagao, H. Nanri, Japan Methane Propulsion Research Exploration Agency


Regency VII

Spring

Regency VI

Hanover A

49

Mira, M. Okamoto, Y. Kidaite, M. Hirota, Mie University, Tsu, Japan

George Washington University, A. Krishnamurthy, B. Ulmen, G. Washington, DC Chen, P. Keutelian, University of Illinois, Urbana-Champaign, Urbana, IL; M. Reilly, Starfire Industries, Champaign, IL; G. Miley, NPL Associates, Inc., Champaign, IL

K. Kambly, T. Bradley, Colorado State University, Fort Collins, CO

1730 hrs AIAA-2012-3865 Geographical and Temporal Variations in Plug-in Electric Vehicle HVAC Loads

D. Brown, B. Beal, Air Force Research Research Center, Cleveland, OH Laboratory, Edwards AFB, CA; J. Blakely, ERC, Inc., Edwards AFB, CA

Chaired by: J. DANKANICH, Gray Research, Inc. 1700 hrs 1630 hrs AIAA-2012-3870 AIAA-2012-3869 Experimental Assessment of Ion Current Density Study of Double Langmuir Probe Analysis the NASA-300M Hall Thruster W. Huang, R. Shastry, D. Herman, Techniques in a Hall Thruster G. Soulas, H. Kamhawi, NASA Glenn Plume


of Maryland, College Park, College Park, MD

G. Azarnia, W. Hargus, M. Nakles, Air Force Research Laboratory, Edwards AFB, CA

1730 hrs AIAA-2012-3871 A Comparison of Ion Acceleration Characteristics for Krypton and Xenon Propellants within a 600 W Hall Effect Thruster B. Prince, Air Force Research Laboratory, Kirtland AFB, NM; Y. Chiu, Busek Company, Inc., Natick, MA

Hall Thruster Physics I

Advanced Concepts I

Ground and Air Vehicle Systems

1800 hrs AIAA-2012-3872 Optical Emission Spectra of the Iodine Hall Thruster

Chaired by: M. BOSS, EADS Astrium GmbH and J. VAN NOORD, NASA Glenn Research Center 1630 hrs 1700 hrs 1730 hrs AIAA-2012-3866 AIAA-2012-3867 AIAA-2012-4103 Development of a Investigation of Plasma Micro-Cathode Arc Thruster Superconducting Helicon Properties in a Helicon Injected (?CAT) Performance and Thrust Thruster Inertial Plasma Electrostatic Vector Control J. Vitucci, R. Sedwick, University T. Zhuang, A. Shashurin, M. Keidar, Rocket (HIIPER)


O. Abdellatif, Benha University, Cairo, Egypt; S. ElDemerdash, E. Khalil, Cairo University, Cairo, Egypt

Chaired by: T. BRADLEY, Colorado State University 1630 hrs 1700 hrs AIAA-2012-3863 AIAA-2012-3864 Experimental and numerical Environmental Evaluation and investigations of aerodynamic Effectiveness of Electric-assist characteristics around buses Bicycle for a Local Transportation N. Maruyama, S. Hara, M. Torregrosa and trucks


Cortland

Baker

Kennesaw

50

A. Butt, C. Popp, F. Jernigan, NASA Marshall Space Flight Center, Huntsville, AL; L. Paseur, Teledyne Brown Engineering, Huntsville, AL; H. Pitts, The Boeing Company, Huntsville, AL

Kenneth Rock NASA Langley Research Center

Technology Bombay, Mumbai, India

Center, Cleveland, OH; P. Giel, ASRC Aerospace Corporation, Cleveland, OH

Turbines

B. Saracoglu, G. Paniagua, von M. Golsen, S. Mahadevan, G. Natsui, Kármán Institute for Fluid Dynamics, M. Ricklick, J. Kapat, University of Rhode-Saint-Genèse, Belgium Central Florida, Orlando, FL

1800 hrs AIAA-2012-4101 Heat Transfer and Film Effectiveness Study on a Pitchwise Curved Surface with Unsteady Wake Interaction

Rodney Bowersox Texas A&M University

Nuclear Power Technologies and Fuels I

Timothy O’Brien Aerojet

Chaired by: A. NIX, West Virginia University and G. PANIAGUA, von Karman Institute 1700 hrs 1730 hrs 1630 hrs AIAA-2012-3879 AIAA-2012-3880 AIAA-2012-3878 Heat Transfer Investigation on Application of Sweep to Low Aerodynamic Investigation of Pressure Turbine Blade for Tip Incidence Angle Effects in a Large a Transonic Turbine Cascade Scale Transonic Turbine Cascade with Pulsating Trailing Edge Flow Containment R. Trehan, B. Roy, Indian Institute of A. McVetta, NASA Glenn Research Cooling


of Technology, Atlanta, GA

Chaired by: R. BEHERA and M. HOUTS, NASA Marshall Space Flight Center 1700 hrs 1630 hrs AIAA-2012-3877 AIAA-2012-3876 A High Power-to-Weight Ratio Atomic Scale Investigation of Lanthanide Substitution in Liquid Metal MHD Concept Reactor for Space and Terrestrial Urania (UO2) R. Behera, C. Deo, Georgia Institute Needs

G. Rosaire, P. Tsvetkov, Texas A&M University, College Station, TX

Chris Gettinger ATK

Monday, 30 July 2012 72-TNES-1

Panelists:

Control Methods for Liquid Rocket Engines

Next Steps in Hypersonics - Turning Research into Reality

1730 hrs AIAA-2012-3875 Best Practices from the Design and Development of the Ares I Launch Vehicle Roll and Reaction Control Systems

Moderator: Dr. Mark Lewis, Director, Science and Technology Policy Institute, Institute for Defense Analyses

Monday, 30 July 2012 71-JPC-5 1630 - 1830 hrs

French Space Agency (CNES), Paris, V. Zmijanovic, V. Lago, National Center France for Scientific Research (CNRS), Orléans, France; P. Sandrine, J. Oswald, French Space Agency (CNES), Evry, France; A. Chpoun, University of Evry, Evry, France

Chaired by: S. FORDE, Aerojet and T. GIEL, Jacobs Technology 1630 hrs 1700 hrs AIAA-2012-3873 AIAA-2012-3874 Progress of the development Experimental and Numerical of an all-electric control system Study of Thrust-Vectoring Effects by Transverse Gas Injection into of a rocket engine P. Alliot, J. Chopinet, F. Lassoudiere, a Propulsive Axisymmetric C-D Snecma, Vernon, France; G. Sylvain, Nozzle


James Kenyon Office of the Secretary of Defense


Hanover F

The Learning Center

Chiping Li Air Force Office of Scientifc Research

Roswell

51

M. Bedard, ; T. Feldman, A. Rettenmaier, W. Anderson, Purdue University, West Lafayette, IN


R. Epenoy, French Space Agency (CNES), Toulouse, France; N. Berend, ONERA, Palaiseau, France; E. Cliquet, J. Ruault, French Space Agency (CNES), Paris, France

West Lafayette, IN

D. Pederson, University of Texas, Austin, Austin, TX; J. Hojnicki, NASA Glenn Research Center, Cleveland, OH


1800 hrs AIAA-2012-3758 Two-Mode Active Thrust Modulation of a Solid Propellant Rocket Motor

M. Tanaka, Y. Osawa, Y. Yokomine, E. Cavallini, D. Bianchi, B. Favini, M. National Defense Academy, Di Giacinto, University of Rome “La Yokosuka, Japan Sapienza”, Rome, Italy; F. Serraglia, ESA, Frascati, Italy

1730 hrs AIAA-2012-3887 Propellant Effects on SRM Upper Stage Internal Ballistics and Performance with Nozzle K. Park, S. Heister, Purdue University, Erosion Characterization

1700 hrs AIAA-2012-3886 Agglomeration/Breakup Studies on Radial Slot Flows in Solid Rocket Motor

Solid Rocket Motor Internal Ballistics Analysis

N. Robinson, Center for Space Exploration, El Paso, TX; A. Choudhuri, University of Texas, El Paso, El Paso, TX

Anderson, Advanced Cooling Technologies, Inc., Lancaster, PA

Technologies, Inc., Lancaster, PA

M. Choi, NASA Goddard Space Flight M. Choi, NASA Goddard Space Flight Center, Greenbelt, MD Center, Greenbelt, MD

1800 hrs AIAA-2012-3895 Three Canted Radiator Panels to Provide Adequate Cooling for Instruments on Slewing Spacecraft in LEO

Spacecraft and Lunar/Mars/Venus Surface Thermal Management

Chaired by: M. CHOI, NASA Goddard Space Flight Center and S. SPENCER, Naval Research Laboratory 1700 hrs 1730 hrs 1630 hrs AIAA-2012-3893 AIAA-2012-3894 AIAA-2012-3892 Diode Heat Pipes for Long Using Pre-melted Phase Long Lived Venus Lander Change Material to Keep Thermal Management System Lived Venus Landers M. Dechristopher, C. Tarau, W. Payload Warm without Power Design Anderson, Advanced Cooling R. Hay, A. Slippey, C. Tarau, W. for Hours in Space

Monday, 30 July 2012 77-TM-2

D. Jones, S. Koelfgen, NASA Dryden Flight Research Center, Edwards, CA; M. Barnes, R. McCauley, T. Wall, NASA Marshall Space Flight Center, Huntsville, AL; B. Reed, NASA Glenn Research Center, Cleveland, OH; C. Duncan, TASC, Inc., Kirtland AFB, NM

Chaired by: M. SIR, The Aerospace Corporation and B. ST GERMAIN, SpaceWorks Engineering, Inc. (SEI) 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2012-3888 AIAA-2012-3889 AIAA-2012-3890 AIAA-2012-3891 Large Solid Rocket Motors for How Fast Can We Go To Mars Analysis of Roll Steering Executive Summary of Future European Launcher Using High Power Electric for Solar Electric Propulsion Propulsion on the Orion Abort B. Didier, Snecma, Le Haillan, France Propulsion? Missions Flight-Test Vehicles

Monday, 30 July 2012 76-ST-2

T. Kibbey, Jacobs, Huntsville, AL

Chaired by: A. NERI, ESA/ESTEC 1630 hrs AIAA-2012-3885 One-Dimensional, Two-Phase Flow Modeling Toward Interpreting Motor Slag Expulsion Phenomena


of Alabama, Huntsville, Huntsville, AL B. Carruthers, S. Abernathy, M. Snyder, H. Driscoll, P. Clingan, Ohio State University, Columbus, OH

Chaired by: R. FREDERICK, University of Alabama, Huntsville and J. MILLER, NASA Marshall Space Flight Center 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2012-3881 AIAA-2012-3882 AIAA-2012-3883 AIAA-2012-3884 Design of a High Power Rocket Microfluidics in the First-Year Student Design/Build/Test of a Institution and Community Classroom: Understanding the Throttleable LOX-LCH4 Thrust Wide Approach to Engineering Aerodynamics DAQ Payload D. Cavender, B. Setayesh, University Foundation Chamber Workforce Development

Monday, 30 July 2012 74-EDU-1

Lenox

Techwood

Vinnings

University

52

Applied Physics Laboratory, Laurel, MD

Institute of Technology, Pasadena, CA

Sustainable Energy Conversion Systems

J. Castaldo, Aeroflex, Plainview, NY

Tani, Kyushu University, Fukuoka, N. Bellomo, F. Barato, M. Faenza, D. Saito, Y. Saburo, K. Hirata, Japan; T. Shimada, Institute of A. Bettella, D. Pavarin, University of T. Sakurai, N. Shiraishi, Tokyo Padova, Padova, Italy Metropolitan University, Hino, Japan Space and Astronautical Science, Sagamihara, Japan

Chaired by: J. MICHLITSCH, The Aerospace Corporation and S. CLAFLIN, Pratt & Whitney Rocketdyne 1700 hrs 1730 hrs 1630 hrs AIAA-2012-3904 AIAA-2012-3905 AIAA-2012-3903 A Study of Hybrid Rockets with The “Vortex Reloaded” project: Combustion Characteristics numerical investigation on fully of Paraffin-Fueled Swirling Multi-Section Swirl Injection tangential vortex injection in Oxidizer-Flow-Type Hybrid Method Y. Hirata, S. Ohyama, S. Aso, Y. Rocket Engines N2O - paraffin hybrid motors


B. Waxman, B. Cantwell, Stanford University, Stanford, CA; G. Zilliac, NASA Ames Research Center, Moffett Field, CA

1800 hrs AIAA-2012-3906 Effects of Injector Design and Impingement Techniques on the Atomization of SelfPressurizing Oxidizers

Swirling Oxidizer Flows

A. Srivastava, S. Shah, N. Komerath, E. Ogedengbe, ENERGHX, Ottawa, S. Kwankaomeng, King Mongkut’s Battelle Memorial Institute, Richland, Georgia Institute of Technology, Canada; E. Ogedengbe, University of Institute of Technology Ladkrabang, WA Atlanta, GA Lagos, Lagos, Nigeria Bangkok, Thailand; B. Kongtrakool, Srinakharinwirot University, Nakhonnayok, Thailand; B. Banterng Silpsakoolsook, Siam University, Bangkok, Thailand

Chaired by: J. FLEURIAL, Jet Propulsion Laboratory, California Institute of Technology and B. NESMITH, Jet Propulsion Laboratory, California Institute of Technology 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2012-3900 AIAA-2012-3901 AIAA-2012-3902 Oral Presentation (Invited) Thermoelectric and Feasibility Study of Cafeteria Investigation and Solar Thermochemical Power Thermophotovoltaic MicroEnergy Demand with Development on Performance and Fuels R. Wegeng, C. Pestak, Pacific Renewable Power Systems for Integration of a Downdraft of a Rice-Husk Powered Northwest National Laboratory, Home Use Bio-digester System Stirling Engine-Generator

Monday, 30 July 2012 79-EC-3

Applied Physics Laboratory, Laurel, MD

Spacecraft Power System In-Orbit Performance

Chaired by: M. PATEL, U.S. Merchant Marine Academy and A. BAISDEN, Johns Hopkins University Applied Physics Laboratory 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2012-3896 AIAA-2012-3897 AIAA-2012-3898 AIAA-2012-3899 The STEREO Spacecraft’s Power The TIMED Spacecraft Mission The Design and Operation of Aeroflex’s Space Qualified Lithium-Ion Battery Cell System Extended Mission Flight Orbital Performance Ten Years the Dawn Power System G. Cardell, A. Ulloa-Severino, M. Gross, Balancing and Protection in LEO Performance Jet Propulsion Laboratory, California M. Butler, Johns Hopkins University M. Butler, Johns Hopkins University Electronics

Monday, 30 July 2012 78-APS-2

Inman

Fairlie

Greenbriar

53

Schlieben, Technical University of Munich, Garching, Germany

Film Cooling

I. Halliwell, K. Justice, Power Systems Manufacturing, Jupiter, FL

L. Williams, Konfluence Research, Manitou Springs, CO

C. Perullo, B. Havrilesko, J. Tai, D. Mavris, Georgia Institute of Technology, Atlanta, GA

1730 hrs AIAA-2012-3913 An Integrated Assessment of an Advanced Open Rotor Configuration Using the Environmental Design Space

Chaired by: R. SHAW, NASA Glenn Research Center

Tuesday, 31 July 2012 84-IECEC-5 0800 - 0900 hrs

Hamburg, Germany

Tuesday

Future Flight Propulsion Systems III

Advanced Propulsion Architecture

G. Schlieben, C. Kirchberger, O. Haidn, Technical University of Munich, Garching, Germany

Ronald Sega Vice President of Energy and Environment, Institute of Energy and Environment Ohio State University

IECEC Keynote Plenary: Aerospace Capabilities Applied To Solving Terrestrial Energy Problems...A University View

Chaired by: M. MILLIS, Tau Zero Foundation and E. DAVIS, Institute for Advanced Studies at Austin 1900 hrs 1930 hrs AIAA-2012-3915 AIAA-2012-3916 On the Reality of Gravity-Like Physics of the Electromagnetic Fields Control of Spacetime and J. Hauser, HPCC-Space GmbH, Gravity


E. Hendricks, M. Tong, NASA Glenn Research Center, Cleveland, OH

Chaired by: J. TAI, Georgia Institute of Technology 1630 hrs 1700 hrs AIAA-2012-3911 AIAA-2012-3912 Performance and Weight Fuel Burn Benefits of a Estimates for an Advanced Variable-Pitch Geared Fan Open Rotor Engine Engine


Second University of Naples, Aversa, ESA, Noordwijk, The Netherlands; Italy; F. Nasuti, M. Onofri, University M. Onofri, University of Rome, of Rome “La Sapienza”, Rome, Italy Rome, Italy

Chaired by: E. BESNARD, California State University, Long Beach and R. BALLARD, NASA Marshall Space Flight Center 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2012-3907 AIAA-2012-3908 AIAA-2012-3909 AIAA-2012-3910 Modelling and Simulation of Assessment of Analytical Using Intra Cooling Channel Numerical Study of Heat Transfer in Film Cooled Thrust Film Cooling in Liquid Rocket Models for Film Cooling in a Measurements for Film Cooling Engine Propulsion Systems Hydrocarbon/GOX Rocket Investigations in a GOX/ Chambers B. Betti, University of Rome “La F. Di Matteo, M. Venanzi, University Combustion Chamber Kerosene Rocket Combustion Sapienza”, Rome, Italy; E. Martelli, of Rome, Rome, Italy; M. De Rosa, O. Haidn, C. Kirchberger, G. Chamber


Dunwoody

Hanover B

Hanover G

Piedmont

54

Turbine Engines: Aviation Management and Technology David Garrison Managing Director, Engine and Component Maintenance Delta Tech Ops

Tuesday Opening Keynote


J. Sands, J. Gladin, B. Kestner, D. Mavris, Georgia Institute of Technology, Atlanta, GA

Rolls-Royce Group plc, Indianapolis, IN

Hasegawa, M. Kodera, S. Ueda, Japan Y. Zhao, J. Liang, Y. Zhao, M. Sun, L. China; Y. Zhang, Nanyang Institute of Aerospace Exploration Agency (JAXA), Yang, National University of Defense Technology, Nanyang, China; L. Tian, Kimigaya, Japan G. Song, X. Xu, Beihang University, Technology, Changsha, China Beijing, China

Experimental Investigations in Supersonic Combustion

Aerospace Systems Design Laboratory, Atlanta, GA

Chaired by: C. MUNDT, University of the German Federal Armed Forces and S. POWELL, Aerospace Testing Alliance (ATA) 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3921 AIAA-2012-3922 AIAA-2012-3923 Performance of a Rocket-Ramjet Research on flow structure Experimental study on Combined-Cycle Engine Model of supersonic combustion combustion mode transition in under Ramjet-Mode Operations chamber based on cavity an aero-ramp based scramjet S. Tomioka, K. Kato, K. Tani, S. B. Wei, Beihang University, Beijing, strut flame holder

Tuesday, 31 July 2012 87-HSABP/HYP-3

Research Center, Cleveland, OH

Propulsion Integration

Chaired by: N. HERRING, United Technologies Research Center and R. SCHARNHORST, The Boeing Company 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2012-3917 AIAA-2012-3918 AIAA-2012-3919 AIAA-2012-3920 Optimal Inlet Shape Design Hybrid Wing Body Engine The UltraFan Engine and Parametric Heat Exchanger of N2B Hybrid Wing Body Cycle Design Exploration for Aircraft Based Thrust Design for Next Generation Configuration Boundary Layer Ingesting Reversing Advanced Vehicle and H. Kim, ASRC Aerospace Corporation, (BLI) Propulsion Systems B. McKay, Lockheed Martin Propulsion System Analysis Cleveland, OH; M. Liou, NASA Glenn Under Design Uncertainty Corporation, Marietta, GA; A. Barlow, P. Gray, B. Kestner, D. Mavris,

Tuesday, 31 July 2012 86-ABPSI-5

Hanover E

Hanover C

Airlines are continuously looking for ways to lower costs and improve efficiency and reliability. Delta Air Lines currently maintains a fleet of more than 750 aircraft, plus provides maintenance for more than 150 other operators. The Delta fleet is one of the most reliable fleets in the world. Delta has developed an unparalleled level of experience and knowledge in the art of aircraft and engine maintenance. Delta must rely on new technology and develop new processes to make aircraft and engines more reliable and fuel-efficient. This in turn enables Delta to expand service to new cities, increase profits, and achieve industry-leading operational performance.

Tuesday, 31 July 2012 85-JPC-6 0800 - 0900 hrs

55

F. Zhong, T. Chen, X. Fan, L. Chen, X. Chang, Chinese Academy of Sciences, Beijing, China

1130 hrs AIAA-2012-3931 A Method to Determine Any Damage to Structure Resulting B. Longmier, L. Cassady, J. Squire, from Recirculation of Particles M. Carter, A. Ilin, T. Glover, F. Chang in the VASIMR® VX-200 Diaz, Ad Astra Rocket Company, Plasma Engine Backfield

1100 hrs AIAA-2012-3930 VASIMR VX-200 Improved Throttling Range

Japan Aerospace Exploration Agency Matteis, Italian Aerospace Research Center (CIRA), Capua, Italy (JAXA), Ibaraki, Japan


Inman

Regency V

Regency VII

Rubén Del Rosario Project Manager Subsonic Fixed Wing NASA

Panelists:

Alan Epstein Vice President Technology and Environment, Pratt & Whitney

Mark Wilson Chief Operating Officer, Rolls-Royce North American Technologies, Inc. (LibertyWorks)

Richard Donaldson Executive, Advanced Programs, GE Aviation

The panel will discuss NASA and US industry perspective on propulsion technology required to meet the technical challenges envisioned for future commercial aircraft. Speakers will highlight the short-, mid- and long-term perspectives of the visions

Tuesday, 31 July 2012 91-JPC-7 Challenges for Future Commercial Aircraft Propulsion 1000 - 1200 hrs Moderator: Richard A. Wahls, Project Scientist Subsonic Fixed Wing, NASA Langley Research Center

R. Arnold, G. Obermaier, A. Goetz, Astrium, Munich, Germany

CH4 Engines: Booster, Upper Stage, and Technology Demonstrators

W. Meeks, J. Rovey, Missouri University of Science and Technology, Webster, TX; E. Bering, University of M. Martin, Texas A&M University, Houston, Houston, TX Rolla, MO College Station, TX

1030 hrs AIAA-2012-3929 Numerical and experimental efforts to explain delayed gas breakdown in ?-pinch devices with bias magnetic field

Electromagnetic Propulsion II

H. Hassan, J. Edwards, J. Fulton, North Carolina State University, Raleigh, NC

Supersonic Mixing / Injection I 1130 hrs AIAA-2012-3927 Role of Chemical Kinetic Models in Simulating Scramjet Flows

Chaired by: D. COOTE, NASA Stennis Space Center and D. PRECLIK, Astrium, an EADS Company 1030 hrs 1100 hrs 1000 hrs AIAA-2012-3933 AIAA-2012-3935 AIAA-2012-3932 An End-to-End High Fidelity Design and Development Current Status of the Technology Development Numerical Simulation of the of a LOX/LCH4 Technology Project for a New Storable LE-X Engine - Combustion Demonstrator V. Salvatore, F. Battista, R. Votta, Propellant Upper Stage Engine Chamber Risk Evaluation M. Di Clemente, M. Ferraiuolo, P. De N. Tani, N. Yamanishi, A. Kurosu, Demonstrator

Tuesday, 31 July 2012 90-LP-11

A. Hallock, Yetispace, Inc., Huntsville, AL; K. Polzin, NASA Marshall Space Flight Center, Huntsville, AL; G. Emsellem, Elwing Company, Wilmington, DE

Chaired by: J. GILLAND, OAI 1000 hrs AIAA-2012-3928 Thrust Stand Measurements of a Conical Pulsed Inductive Plasma Thruster

Tuesday, 31 July 2012 89-EP-11

Research Center, Hampton, VA; A. Wilhite, National Institute of Aerospace, Hampton, VA

Chaired by: D. MUSIELAK, University of Texas, Arlington and R. HARTFIELD, Auburn University 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3924 AIAA-2012-3925 AIAA-2012-3926 LES/RANS Simulations of Three-Dimensional Heat Study of Forebody Injection Turbulent Mixing in Gas Transfer Analysis and and Mixing with Application Optimized Design of Actively to Hypervelocity Airbreathing Plumes I. Zilberter, J. Edwards, North Propulsion Cooled Strut for Scramjet E. Axdahl, A. Kumar, NASA Langley Carolina State University, Raleigh, NC Applications


56

Y. Ito, N. Yamamoto, T. Nagasaki, Tokyo Institute of Technology, Yokohama, Japan

Snyder, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

Kailasanath, Naval Research Laboratory, Washington, DC

D. Dausen, C. Brophy, R. Wright, Naval Postgraduate School, Monterey, CA

Chaired by: C. BROPHY, Naval Postgraduate School 1030 hrs 1000 hrs AIAA-2012-3944 AIAA-2012-3943 Modeling Exhaust Effects in Design and Operation of an Rotating Detonation Engines Optically Accessible Rotating D. Schwer, A. Corrigan, K. Detonation Engine

Tuesday, 31 July 2012 94-PC-8

Glenn Research Center, Cleveland, OH; G. Williams, Ohio Aerospace Institute, Cleveland, OH

1130 hrs AIAA-2012-3739 Demonstration of an Automated Mass Flow Control System for Condensable Propellant Hall-effect Thrusters

L. Shijie, W. Liu, Z. Lin, National University of Defense Technology, Changsha, China; F. Zhuang, Academy of Equipment Command & Technology, Beijing, China; J. Zhou, J. Liang, National University of Defense Technology, Changsha, China

W. Yuhui, J. Wang, S. Tianyi, L. Yusi, L. Yongsheng, Peking University, Beijing, China

1130 hrs AIAA-2012-3946 Experimental Research on Transition Regions in Continuously Rotating Detonation Waves

Rotating Detonation Engines

R. Florenz, T. Liu, A. Gallimore, M. Hopkins, L. King, Michigan University of Michigan, Ann Arbor, Ann Technological University, Houghton, Arbor, MI; H. Kamhawi, NASA Glenn MI Research Center, Cleveland, OH; D. Brown, Air Force Research Laboratory, Edwards AFB, CA; R. Hofer, J. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

1100 hrs AIAA-2012-3945 Experimental Research on the H2/air Continuous Rotating Detonation Engine

Hall Thrusters III

1130 hrs AIAA-2012-3939 Impact of Engine Icing on Jet Engine Compressor Flow Dynamics

Compressors II

A. Suresh, General Electric Company, R. Kundu, J. Prasad, Georgia Institute Schenectady, NY of Technology, Atlanta, GA; P. Tiwari, General Electric Company, Niskayuna, NY; A. Breeze-Stringfellow, P. Szucs, T. Nakano, General Electric Company, Cincinnati, OH

1100 hrs AIAA-2012-3938 Stability of the Phase-Lag Boundary Condition in Turbomachinery Simulations

Chaired by: P. PETERSON, ElectroDynamic Applications, Inc. (EDA) and J. SZABO, Busek Co., Inc. 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3940 AIAA-2012-3941 AIAA-2012-3942 Performance of NASA’s Higher Thermal Behavior of High The Development and Initial Fidelity 50 kW Hall Thruster Power Hall Thrusters Characterization of the X3 G. Soulas, H. Kamhawi, D. Herman, J. Polk, B. Dotson, R. Hofer, D. 100-kW Class Laboratory T. Haag, W. Huang, R. Shastry, NASA Goebel, I. Katz, I. Mikellides, J. Model Nested Hall Thruster


Belgium

Chaired by: N. KEY, Purdue University 1000 hrs 1030 hrs AIAA-2012-3936 AIAA-2012-3937 Estimation of Heat Transfer Airfoil Base Region Control Performance for Compressor with Dielectric Barrier Stators Heat Exchangers Discharge G. Paniagua, P. Rocandio, Y. Babou, in a New Intercooled and von Kármán Institute for Fluid Recuperated Aviation GasDynamics, Rhode-Saint-Genèse, Turbine Engine

Tuesday, 31 July 2012 92-GTE-11

Hanover A

Regency VI

Hanover F

57

T. Matsuoka, I. Funaki, Japan Aerospace Exploration Agency (JAXA), Kanagawa, Japan; S. Satoh, T. Fujino, University of Tsukuba, Tsukuba, Japan; T. Nakamura, H. Nishida, S. Shinohara, Tokyo University of Agriculture and Technology, Koganei, Japan; T. Tanikawa, Tokai University, Hiratsuka, Japan; T. Hada, Kyushu University, Kasuga, Japan; K. Shamrai, Institute for Nuclear Research, Nauki, Ukraine

Purdue University, West Lafayette, IN

A. Krishnamurthy, B. Ulmen, G. Chen, P. Keutelian, University of Illinois, Urbana-Champaign, Urbana, IL; M. Reilly, Starfire Industries, Champaign, IL; G. Miley, NPL Associates, Inc., Champaign, IL

Advanced Concepts II

V. Kumar, P. Panda, H. Mongia, S. Naik, Purdue University, West Lafayette, IN

1130 hrs AIAA-2012-3954 Innovative Approaches for Reducing CO2 Emissions of Aviation Engines Part 1: Selection of Promising Approaches

Internal Combustion Engines

Y. Takao, K. Eriguchi, K. Ono, Kyoto University, Kyoto, Japan

1130 hrs AIAA-2012-3950 Miniature Ion Thruster Using a Cylindrical Micro ICP

Ion Thrusters II

Madrid, Madrid, Spain

J. Brackbill, ERC, Inc., Edwards AFB, CA; J. Cambier, Air Force Research Laboratory, Edwards AFB, CA; N. Gimelshein, S. Gimelshein, ERC, Inc., Edwards AFB, CA; A. Ketsdever, Air Force Research Laboratory, Edwards AFB, CA; T. Quiller, University of Colorado, Colorado Springs, Colorado Springs, CA

Chaired by: M. WALKER, Georgia Institute of Technology and R. WIRZ, University of California, Los Angeles 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2012-3955 AIAA-2012-3956 AIAA-2012-3957 AIAA-2012-4102 A fluiddynamic performance Laboratory Model Helicon Injected Inertial Ionization and Charge Exchange model of a helicon thruster Development of Lissajous Plasma Electrostatic Rocket Reactions in Neutral Entrainment E. Ahedo, J. Navarro, M. MerinoAcceleration for Electrodeless (HIIPER): Experimental Proof of a Field Reversed Configuration Martinez, Technical University of Helicon Plasma Thruster of Principle Thruster


Purdue University, West Lafayette, IN G. Chen, Gannon University, Erie, PA

1100 hrs AIAA-2012-3953 In-Cylinder Combustion and Output Performance and Emissions Influenced by Split Fuel Injection Input Parameters of CompressionP. Panda, V. Kumar, H. Mongia, S. Naik, Ignition Engines

Chaired by: S. GOLLAHALLI and J. MEHTA 1000 hrs 1030 hrs AIAA-2012-3951 AIAA-2012-3952 Innovative Approaches for Innovative Approaches for Reducing CO2 Emissions of Reducing CO2 Emissions of Aviation Engines Part 1: Selection Aviation Engines Part 5: Turbo of Promising Approaches Reaction-Controlled Internal H. Mongia, V. Kumar, P. Panda, S. Naik, Combustion System TRCS

Tuesday, 31 July 2012 96-TFES-3

Ehrbar, M. Robin, Busek Company, Inc., R. Wirz, S. Araki, University of H. Koizumi, K. Komurasaki, Y. Natick, MA; C. Farnell, Plasma Controls, California, Los Angeles, Los Angeles, Arakawa, University of Tokyo, LLC, Fort Collins, CO; R. Hofer, Jet CA Bunkyo, Japan Propulsion Laboratory, California Institute of Technology, Pasadena, CA

Chaired by: M. KEIDAR, The George Washington University and E. CARDIFF, NASA Headquarters 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3947 AIAA-2012-3948 AIAA-2012-3949 Near-Surface Cusp Development of the Miniature Micro Radio-Frequency Ion Confinement of Micro-Scale Ion Propulsion System for 50 Propulsion System M. Tsay, K. Hohman, N. Rosenblad, E. Plasma kg Small Spacecraft


Baker

Kennesaw

Cortland

58

J. McCulley, A. Bath, S. Whitmore, Utah State University, Logan, UT

C. Zaseck, T. Pourpoint, S. Son, Purdue University, West Lafayette, IN

M. Stewart, ASRC Aerospace J. Fittje, Analex Corporation, Corporation, Cleveland, OH; B. Cleveland, OH; B. Schnitzler, Idaho Schnitzler, Idaho National Laboratory, National Laboratory, Idaho Falls, ID Idaho Falls, ID

1100 hrs AIAA-2012-3960 Cycle Analysis of a 200MW Class CERMET Based NTR Engines

S. Arias Quintero, M. Ricklick, J. Kapat, University of Central Florida, Orlando, FL

T. Wang, J. Lin, J. Ruf, M. Guidos, NASA Marshall Space Flight Center, Huntsville, AL

E. Blades, ATA Engineering, Inc., Madison, AL; E. Luke, Mississippi State University, Starkville, MS; J. Ruf, NASA Marshall Space Flight Center, Huntsville, AL

R. Stark, C. Genin, German Aerospace Center (DLR), Hardthausen, Germany

Side Loads

1130 hrs AIAA-2012-3967 Recent Results on Thread Formation with an Impinging Jet Injector

Fuels and Propellant Development

S. Bonifacio, G. Festa, A. Russo M. Negri, German Aerospace Center Sorge, University of Naples “Federico (DLR), Lampoldshausen, Germany; II”, Naples, Italy M. Redaelli, Technical University of Milan, Milan, Italy; H. Ciezki, German Aerospace Center (DLR), Lampoldshausen, Germany

1100 hrs AIAA-2012-3966 Catalytic Ignition in Hydrogen Peroxide-based Space Propulsion Systems

Chaired by: D. PERIGO and J. SAUER, Orbital Technologies Corporation 1030 hrs 1100 hrs 1000 hrs AIAA-2012-3969 AIAA-2012-3970 AIAA-2012-3968 Transient Side Load Analysis Fully-Coupled Fluid-Structure Optimisation of a Rocket Nozzle Side Load Reduction of Out-of-Round Film-Cooled Interaction Simulations of Rocket Engine Side Loads Device Nozzle Extensions


Y. Gan, L. Qiao, Purdue University, West Lafayette, IN

Chaired by: B. CHEHROUDI, European Research Council (ERC) 1000 hrs 1030 hrs AIAA-2012-3964 AIAA-2012-3965 Enhanced Evaporation Synthetic Jet Fuels and Their of Nanofluid Fuels under Impact in Aircraft Performance Radiation and Elastomer Materials


A. Chandler, E. Jens, B. Cantwell, G. Hubbard, Stanford University, Stanford, CA

Paraffin Fuels I

T. Harrison, L. Qualls, Oak Ridge National Laboratory, Oak Ridge, TN

Nuclear Thermal Propulsion II: Engine Modeling 1130 hrs Oral Presentation (Invited) Power Profile Control in Graphite-Based Nuclear Thermal Propulsion Reactor Cores for Mitigation of MidBand Corrosion

Chaired by: S. WHITMORE, Utah State University and B. MADHANABHARATAM, Space Propulsion Group, Inc. 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3961 AIAA-2012-3962 AIAA-2012-3963 Visualization of the Liquid Layer Design and Testing of FDM Paraffin Fuel and Additive Combustion of Paraffin Fuel for Manufactured Paraffin-ABS Combustion in an Opposed Hybrid Rocket Applications Hybrid Rocket Motors Flow Burner Configuration

Tuesday, 31 July 2012 100-HR-4

B. Schnitzler, Idaho National Laboratory, Idaho Falls, ID; S. Borowski, NASA Glenn Research Center, Cleveland, OH

Chaired by: R. JOYNER and M. BULMAN, Aerojet 1000 hrs 1030 hrs AIAA-2012-3958 AIAA-2012-3959 Small Fast Spectrum Reactor Thermal, Fluid, and Structural Analysis of a Cermet Fuel Designs Suitable for Direct Element Nuclear Thermal Propulsion

Tuesday, 31 July 2012 99-NFF-5

Vinnings

Hanover B

University

Hanover D

59

Solar Absorption and Desiccant Cooling Technologies for Air Conditioning in Sunny Countries

Dunwoody

S. Oide, K. Takahashi, T. Kuwahara, Nihon University, Funabashi, Japan

T. Hoshino, H. Naito, K. Ogawa, T. Hashimoto, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan

Segundo, CA

R. Bertacin, F. Ponti, University of Bologna, Forlì, Italy; A. Annovazzi, Avio S.p.A., Colleferro, Italy

G. Miley, X. Yang, University of Illinois, Urbana-Champaign, Urbana, IL

J. Mankins, Artemis Innovation Management Solutions, Santa Maria, CA; N. Kaya, Kobe University, Kobe, Japan; M. Vasile, University of Strathclyde, Glasgow, United Kingdom

Spacecraft Power - Advanced Concepts and Designs

1130 hrs AIAA-2012-3978 SPS-ALPHA: The First Practical Solar Power Satellite via Arbitrarily Large Phased Array (A 2011-2012 NIAC Project)

1100 hrs AIAA-2012-3974 A New Three-Dimensional Ballistic Model for Solid Rocket Motor Non-Homogeneous Combustion

1100 - 1300 hrs Omar Abdelaziz Research and Development Staff Oak Ridge National Laboratory, Oak Ridge, TN, USA

Solid Rocket Motor Propellant Combustion

1030 - 1100 hrs Jo Darkwa Professor, Centre for Sustainable Energy Technologies University of Nottingham-Ningbo, China

Chaired by: J. HAINES, and L. ROUFBERG, Johns Hopkins University Applied Physics Laboratory 1030 hrs 1100 hrs 1000 hrs AIAA-2012-3976 AIAA-2012-3977 AIAA-2012-3975 Advances in Technologies for A Space Power Source Using Study on Technologies for Low Energy Nuclear Reactions Lunar Night Survival Powered High Power SEP Missions A. Arastu, The Boeing Company, El by Solar Arrays (LENRs)

Tuesday, 31 July 2012 105-APS-3

University, Funabashi, Japan

Chaired by: M. KAISERMAN, Raytheon Company and J. VILLARREAL 1030 hrs 1000 hrs AIAA-2012-3972 AIAA-2012-3973 Characteristics of aluminum Ignition and Combustion Characteristics of Liquid GAP agglomeration at burning surface in AP/AN composite with Metals and Oxidizer S. Yamauchi, T. Kuwahara, Nihon propellants

Tuesday, 31 July 2012 104-SR-6

1000 - 1030 hrs Nesreen Ghaddar Associate Provost, Qatar Chair in Energy Studies Professor of Mechanical Engineering, American University of Beirut, Beirut, Lebanon

1130 - 1200 hrs Essam Khalil Professor of Mechanical Engineering Cairo University, Cairo, Egypt

Greenbriar

Techwood

Air conditioning contributes a major consumption of electricity in many parts of the world, especially in sunny countries. As the demand for air conditioning increases, the electricity demand increases. Solar assisted absorption or desiccant cooling is a sustainable solution. It reduces the demand for electricity. A panel of experts will present their view on solar assisted absorption and desiccant cooling technologies in sunny countries. They will focus on challenges and opportunities.

Chaired by: T. BRADLEY, Colorado State University and E. KHALIL, Cairo University


60

N. Komerath, Georgia Institute of Technology, Atlanta, GA

Technology, Pasadena, CA

Center, Cape Canaveral, FL; S. G. Webster, NASA Goddard Space Flight Center, Greenbelt, MD; C. Toro, Chintalapati, D. Kirk, Florida Institute G. Falk, Cobham Pressure Technology of Technology, Melbourne, FL Solutions, Westminster, MD

A. Kustas, T. Cote, A. Jurgensmeyer, D. Williams, B. Minor, B. Dickman, T. Lipsey, T. Bradley, J. Willams, Colorado State University, Fort Collins, CO

E. Abdelghany, Aviation Institute, Cairo, Egypt; A. Alsayed, Zagazig University, Zagazig, Egypt; M. Fouad, E. Khalil, Cairo University, Cairo, Egypt

Hermann Hald, German Aerospace Center (DLR), Stuttgart, Germany

University of Rome, Rome, Italy

Transpiration Cooling and Cooling Channel Analysis

Thermal Management of Machinery

A. Herbertz, M. Selzer, German Aerospace Center (DLR), Stuttgart, Germany

College, Riverdale, NY; M. Pizzarelli, University of Rome, Rome, Italy

Chaired by: M. MEYER, NASA Glenn Research Center and E. BESNARD, California State University, Long Beach 1030 hrs 1100 hrs 1130 hrs 1000 hrs AIAA-2012-3990 AIAA-2012-3991 AIAA-2012-3992 AIAA-2012-3989 Transpiration Cooled Ceramic Analysis on the Effect of Improved Correlations for Systems Analysis of a LOX/ Thrust Chamber Applicability Channel Aspect Ratio on Curvature Effects in Cooling LH2 Rocket Engine with a Channels of Rocket Engines Transpiration-Cooled Ceramic for High-Thrust Rocket Engines Rocket Thermal Behavior A. Herbertz, M. Ortelt, I. Müller, I. M. Pizzarelli, F. Nasuti, M. Onofri, M. Naraghi, R. Dassonville, Manhattan Thrust-Chamber


E. Abdelghany, Aviation Institute, Cairo, Egypt; A. Alsayed, Zagazig University, Zagazig, Egypt; M. Fouad, E. Khalil, Cairo University, Cairo, Egypt

Chaired by: C. TARAU, Advanced Cooling Technologies and M. CHOI, NASA Goddard Space Flight Center 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3986 AIAA-2012-3987 AIAA-2012-3988 Effect of Shaped-Hole on Film High Efficiency Thermoelectric Effect of Film Cooling of HP and Cooling Effectiveness of Gas Coolers for Use in Firefighter IP Turbines on Performance of Turbine Blade Applications Triple Spool Turbofan Engines

Tuesday, 31 July 2012 108-TM-3

O. Kartuzova, M. Kassemi, NASA Glenn Research Center, Cleveland, OH

Tanks I: Optimization and Control

F. Wyczalek, Energy Independence Foundation, Bloomfield Hills, MI; M. Wyczalek, General Motors Corporation, Warren, MI; T. Wyczalek, Magna Exteriors and Interiors, Novi, MI

Stirling System Design and Optimization 1130 hrs AIAA-2012-3982 Passenger Vehicle Hill CoastDown Math Model

Chaired by: G. GRAYSON, The Boeing Company and V. AHUJA, Combustion Research & Flow Technology, Inc. 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3983 AIAA-2012-3984 AIAA-2012-3985 Modeling Active Pressure Contamination Control of Non-Dimensional Control in a Large Scale the Global Precipitation Parameterization of Tank Cryogenic Storage Tank in Measurement Mission Purge Behavior J. Roth, NASA Kennedy Space Normal Gravity Propellant Tank


M. Fox, Self, Fort Collins, CO

Chaired by: S. WILSON, NASA Glenn Research Center and S. ORITI, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3979 AIAA-2012-3980 AIAA-2012-3981 Dynamic Pitching Moment A Hydraulic Motor-Alternator A Simulation-Integrated System for Ocean-Submersible Decision Support System for Measurement of a Wing Executing Pitch and Plunge Vehicles Advanced Vehicle Design H. Aintablian, Jet Propulsion Demonstrated on Colorado Motion Laboratory, California Institute of K. Goal, V. Raghav, A. Srivastava, State’s EcoCAR

Tuesday, 31 July 2012 106-EC-4

Piedmont

Lenox

Roswell

Fairlie

61

R. Florea, C. Matalanis, L. Hardin, M. Stucky, A. Shabbir, United Technologies Research Center, East Hartford, CT

Robust and Resilient System Design Approaches for Next Generation Terrestrial Nuclear Energy Systems

Center, Cleveland, OH; T. Reddy, University of Toledo, Toledo, OH; A. Ferrar, W. O’Brien, Virginia G. Herrick, NASA Glenn Research Polytechnic Institute and State Center, Cleveland, OH; A. Shabbir, R. University, Blacksburg, VA Florea, United Technologies Research Center, East Hartford, CT

Spring

Hanover G

C. Lee, D. Mavris, Georgia Institute of Technology, Atlanta, GA

Technologies Research Center, East Hartford, CT

J. Mace, M. Lakebrink, M. Mani, The Boeing Company, St. Louis, MO; W. Steenken, BVS and Associates, Hamilton, OH

1400 hrs AIAA-2012-3999 Computational Simulation of Dynamic Total-Pressure Distortion in an S-Diffuser

Inlet/Engine Performance Prediction Tools

William Harrison III Technical Advisor for Fuels and Energy Air Force Research Laboratory Fellow United States Air Force

IECEC Awards Luncheon Keynote: Aerospace Capabilities Applied to Solving Terrestrial Energy Problems...A Federal Laboratory View

Chaired by: T. BERENS, Cassidian and K. BLODGETT, GE Aviation 1300 hrs 1330 hrs AIAA-2012-3997 AIAA-2012-3998 Bayesian Collaborative Nacelle External Sampling for Aero-Propulsion Drag Prediction Using Design of an Engine and Computational Fluid Dynamics J. Joo, G. Tillman, R. Lin, United Nacelle

Tuesday, 31 July 2012 113-ABPSI-7



Hanover C


Novel terrestrial nuclear energy systems are emerging for a broad range of potential applications spanning from conventional electricity generation to process heat for energy demanding industrial applications with an expectation of absolute safety and autonomy of operation. These requirements and trends lead to an amplified synergy between considerations for space systems and terrestrial systems within the realm of nuclear driven configurations. This special session will offer a forum to discuss designs, requirements, methods and trends for novel nuclear energy systems focusing on robust and resilient system design approaches needed for next generation technology development to meet performance targets under competitive economics constraints.

Chaired by: M. HOUTS, NASA Marshall Space Flight Center


L. Hardin, G. Tillman, O. Sharma, United Technologies Research Center, East Hartford, CT; J. Berton, D. Arend, NASA Glenn Research Center, Cleveland, OH

1130 hrs AIAA-2012-3996 Fan Response to Total Pressure Distortions Produced by Boundary Layer Ingesting Serpentine Inlets

NASA Fundamental Aeronautics Program, Subsonic Fixed Wing Project, Efficient Propulsion and Power Research

Chaired by: M. HATHAWAY, NASA Glenn Research Center and D. AREND, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs AIAA-2012-3993 AIAA-2012-3994 AIAA-2012-3995 Parametric Analysis and Aeromechanics Analysis of a Aircraft System Study of Design for Embedded Engine Boundary Layer Ingesting Fan Boundary Layer Ingesting M. Bakhle, NASA Glenn Research Inlets Propulsion

Tuesday, 31 July 2012 110-GTE-12/ABPSI-6

62 W. Gerstler, K. Huh, E. Ruggiero, F. Ghasripoor, A. El-Refaie, P. de Bock, X. Shen, J. Alexander, General Electric Company, Niskayuna, NY

Advanced Seal Technology I

Aeronautical Institute of Technology, Y. Gan, L. Qiao, Purdue University, São José dos Campos, Brazil West Lafayette, IN

Chaired by: T. JACKSON, University of Illinois 1300 hrs 1330 hrs AIAA-2012-4006 AIAA-2012-4007 Study of Hydrogen Combustion Combustion of Nanofluid Fuels in Homogeneous Reactor with the Addition of Boron and R. Gonçalves, J. Rocco, K. Iha, Iron Particles


Product Development Services, Ltd., Devizes, United Kingdom Solihull, United Kingdom

S. Gomes, Aeronautical Institute of Technology, São José dos Campos, Brazil; L. Rocco, Flowtest Aerospace Research, São Paulo, Brazil; J. Rocco, K. Iha, Aeronautical Institute of Technology, São José dos Campos, Brazil

1400 hrs AIAA-2012-4008 Combustion evaluation of PU solid fuel based on pre-polymer technology additivated with paraffin and Aluminum for hybrid rocket engines

Combustion Studies I

Chaired by: B. STEINETZ, NASA Glenn Research Center; P. DUNLAP, NASA Glenn Research Center and E. RUGGIERO, General Electric Company 1330 hrs 1400 hrs 1300 hrs AIAA-2012-4003 AIAA-2012-4004 AIAA-2012-4005 A Novel High Temperature Experimental Results of an Brush Seal Hysteresis A. Bowsher, P. Crudgington, T. Kirk, Non-Contact Dynamic Seal Aramid Fiber Brush Seal for HighCross Manufacturing Company, Ltd., P. Crudgington, R. Cross, E. Cross, Power Density, Liquid-Cooled, Devizes, United Kingdom; J. Walia, Cross Manufacturing Company, Ltd., Rotating Electric Machines

Tuesday, 31 July 2012 117-SCP-1

Beavercreek, OH; K. Hsu, Innovative Scientific Solutions, Inc., Dayton, OH; M. Hagenmaier, Air Force Research Laboratory, Wright-Patterson AFB, OH

Dr. George Kopasakis NASA Glenn Research Center Cleveland, OH

Supersonic Mixing / Injection II

Dr. Dan Bulzan NASA Glenn Research Center Cleveland, OH

A. Karimi, S. Wijeyakulasuriya, M. C. Gong, M. Sun, J. Liang, J. Zhou, Nalim, Indiana University-Purdue National University of Defense University Indianapolis, Indianapolis, Technology, Changsha, China IN

Dr. Michael Hathaway NASA Glenn Research Center Cleveland, OH

Mr. Jonathan Litt NASA Glenn Research Center Cleveland, OH

The Impact of Engine Control Technologies on NASA Goals for Improved Aviation Safety, Environmental Compatibility and Performance

Chaired by: B. MADHANABHARATAM, Space Propulsion Group, Inc. and S. BECKEL, ATK Mission Systems 1330 hrs 1400 hrs 1300 hrs AIAA-2012-4000 AIAA-2012-4001 AIAA-2012-4002 Numerical Study of Supersonic The non-reacting flow Effect of Flow Distortion on Cavity-Assisted Fuel Injection Flow over Backward-Facing characteristics of a model J. Boles, R. Milligan, Taitech, Inc., Step for Scramjet Application supersonic combustor


Panelists:

Chaired by: D. CULLEY, NASA Glenn Research Center

Tuesday, 31 July 2012 114-ABPSI-8/GTE-13 1300 - 1500 hrs

Hanover A

Inman

Hanover D

Hanover E

63

University, Yokohama, Japan; H. Koizumi, University of Tokyo, Bunkyo, Japan; T. Hyakutake, Yokohama National University, Yokohama, Japan; H. Kuninaka, Institute of Space and Astronautical Science, Sagamihara, Japan

Nammo Raufoss, Raufoss, Norway

A. Sasoh, D. Ichihara, T. Enoki, S. Yokota, Nagoya University, Nagoya, Japan

Moffett Field, CA; B. Waxman, E. Doran, F. Moretto, University of Padova, Stanford University, Stanford, CA; J. Padova, Italy Dyer, A. Karabeyoglu, Space Propulsion Group, Inc., Sunnyvale, CA; B. Cantwell, Stanford University, Stanford, CA

M. Cannella, B. Lesage, C. Snyder, University of Colorado, Boulder, Boulder, CO

Ground Testing of Hybrid Motors

Electromagnetic Propulsion III

1430 hrs AIAA-2012-4020 Overview of the University of Colorado at Boulder Hybrid Sounding Rocket Project (HySoR)

1400 hrs AIAA-2012-4276 Steady-State, AppliedField, Rectangular Magnetoplasmadynamics Thruster Using Hollow Cathode

Chaired by: D. MYRE, U.S. Naval Academy and B. EVANS, Space Propulsion Group Inc. 1330 hrs 1400 hrs 1300 hrs AIAA-2012-4018 AIAA-2012-4019 AIAA-2012-4017 Peregrine Hybrid Rocket Motor Experimental Characterization Development of a student Ground Test Results of a Hydrogen Peroxide hybrid rocket G. Zilliac, NASA Ames Research Center, Simulator J. Ronningen, R. Vesterås, M. Berger,


A. Boxberger, P. Bambach, G. Herdrich, P. Upadhyay, S. Fasoulas, H. Roser, University of Stuttgart, Stuttgart, Germany; M. MerinoMartinez, Technical University of Madrid, Madrid, Spain

Chaired by: D. KIRTLEY and J. HAAS, Air Force Research Laboratory 1300 hrs 1330 hrs AIAA-2012-4012 AIAA-2012-4013 Experimental Investigation Effect of Inter-electrode of Applied-Field Geometry on the Performance Magnetoplasmadynamic of an Applied-field 2D MPD Thrusters at Institute of Space Thruster M. Takubo, Yokohama National Systems


Y. Daimon, H. Negishi, N. Yamanishi, Herbertz, German Aerospace Center (DLR), Stuttgart, Germany Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; Y. Nunome, M. Sasaki, T. Tomita, Japan Aerospace Exploration Agency (JAXA), Kakuda, Japan

B. Betti, M. Pizzarelli, F. Nasuti, University of Rome “La Sapienza”, Rome, Italy

1430 hrs AIAA-2012-4123 Coupled Heat Transfer Analysis in Regeneratively Cooled Thrust Chambers

Cooling Techniques and Structural Analysis for Thermally Loaded Engines

Chaired by: T. POURPOINT, Purdue University and W. WANG, The Aerospace Corporation 1300 hrs 1330 hrs 1400 hrs AIAA-2012-4009 AIAA-2012-4010 AIAA-2012-4011 Cyclic laser heating and optical Combustion and Heat Transfer Structural Investigations on Cryogenically Operated and measurement of combustion Modeling in Regeneratively Transpiration Cooled Fibre chamber wall structures Cooled Thrust Chambers J. Riccius, A. Gernoth, S. (Optimal Solution Procedures Reinforced Rocket Thrust Schlechtriem, German Aerospace for Heat Flux Estimation of A Chambers Center (DLR), Hardthausen, Germany M. Ortelt, I. Hermann Hald, A. Full-Scale Thrust Chamber)


University

Regency V

Spring

64

University of Tokyo, Bunkyo, Japan; R. Shastry, D. Herman, NASA Glenn H. Kuninaka, Institute of Space and Research Center, Cleveland, OH Astronautical Science, Sagamihara, Japan; Y. Yamagiwa, Shizuoka University, Hamamatsu, Japan

L. Perna, P. Lozano, Massachusetts Institute of Technology, Cambridge, MA

Alabama, Huntsville, Huntsville, AL

J. Anderson, J. Ziemer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; A. Bulit, ESA, Noordwijk, The Netherlands

1400 hrs AIAA-2012-4293 Cesium Exposure Test of the Colloid Micro-Newton Thruster for the LISA Pathfinder Mission

M. Gauffre, H. Neau, O. Simonin, Fluid Mechanics Institute of Toulouse (IMFT), Toulouse, France; R. Ansart, Laboratory of Chemical Engineering (LGC), Toulouse, France; N. Meyers, Snecma, Vernon, France; S. Petitot, French Space Agency (CNES), Evry, France

Chaired by: D. LINEBERRY, University of Alabama, Huntsville and S. CHIANESE, SpaceX 1330 hrs 1400 hrs 1300 hrs AIAA-2012-4028 AIAA-2012-4029 AIAA-2012-4027 Numerical simulation of a 3D A Streamlined Approach to Experimental Investigation of unsteady two-phase flow in Venturi Sizing Cavitation Induced Feedline the filling cavity in oxygen of a A. Scroggins, NASA Goddard Space Instability from an Orifice Flight Center, Greenbelt, MD M. Hitt, D. Lineberry, University of cryogenic rocket-engine


Institute of Technology, Neuchatel, Switzerland; C. Ryan, J. Stark, Queen Mary, University of London, London, United Kingdom

Chaired by: W. HARGUS, Air Force Reseach Laboratory 1300 hrs 1330 hrs AIAA-2012-4024 AIAA-2012-4289 Progress Towards a Miniaturized Demonstration of Remote, Electrospray Thruster for Flexible Autonomous Attitude Control Propulsion of Small Spacecraft of a CubeSat Using Ion S. Dandavino, C. Ataman, S. Electrospray Propulsion Chakraborty, H. Shea, Swiss Federal Systems


CA

Chaired by: J. BROPHY, Jet Propulsion Laboratory and I. FUNAKI, Japan Aerospace Exploration Agency 1300 hrs 1330 hrs 1400 hrs AIAA-2012-4021 AIAA-2012-4022 AIAA-2012-4023 Performance of Miniature Status of the NASA’s Plasma Loss through Evolutionary Xenon Thruster Permanent Magnet Cusps in Microwave Discharge Ion Thruster for Drag-free Control (NEXT) after 42,100 Hours, Miniature Ion Thrusters H. Mao, R. Wirz, University of T. Izumi, Shizuoka University, 738 kg Throughput, and 28.2 California, Los Angeles, Los Angeles, Hamamatsu, Japan; H. Koizumi, MN-s Total Impulse


Transient Processes in Orifices and Oxygen Dome

Electrospray Propulsion II

Ion Thrusters III

Vinnings

Baker

The Learning Center

65

V. McDonell, E. Sullivan-Lewis, R. Hack, University of California, Irvine, Irvine, CA

J. Kim, H. Seo, S. Lee, Pukyong National University, Busan, South Korea

1400 hrs AIAA-2012-4032 An Evolution of the Premixed Flame Precipitated by Ultrasonic Standing Wave

Innovations in Combustor Technology

Initation and Flame Characterization

W. Huang, A. Gallimore, University of G. Williams, Ohio Aerospace Institute, Michigan, Ann Arbor, Ann Arbor, MI Cleveland, OH; W. Huang, D. Herman, NASA Glenn Research Center, Cleveland, OH

B. Prince, Air Force Research Laboratory, Kirtland AFB, NM; Y. Chiu, Busek Company, Inc., Natick, MA

Chaired by: W. HUANG and R. HOFER, Jet Propulsion Laboratory, California Institute of Technology 1330 hrs 1400 hrs 1300 hrs AIAA-2012-4036 AIAA-2012-4037 AIAA-2012-4035 Luminescence Measurements A Low-Cost Optical Approach to Optical Diagnostic Evaluate the Lifetime of Hall Characterization of High-Power of the Kr+/Kr2+ + Kr Hall Thruster Wear and Operation Collision Systems Thruster Discharge Channel


Hall Thruster Physics II

Tuesday, 31 July 2012 128-JPC-8 Interagency Propulsion Technology Development 1300 - 1500 hrs Moderator: James Kenyon, Associate Director, Aerospace Technology, Office of the Secretary of Defense Panelists: Jennings Bryant Fayette Collier Rhett Jeffries William Harrison Technical Advisor for Fuels and Energy Advanced Development & Technology Transition Project Manager, Environmentally Responsible Program Manager, Continuously Lower Energy, Air Force Research Laboratory Senior Engineer Aviation (ERA) Emissions, and Noise (CLEEN) Naval Air Systems Command NASA FAA

of Maryland, College Park, College Park, MD

Chaired by: D. BLUNCK, Air Force Reseach Laboratory and J. TAI, Georgia Institute of Technology 1300 hrs 1330 hrs AIAA-2012-4033 AIAA-2012-4034 Fuel Flexible Distributed Performance Assessment of Combustion for Gas Turbine a Gas Fired RQL Combustion Engines System Operated in a Vitiated A. Khalil Hasan, A. Gupta, University Air Stream


L. Wei, J. Zhou, H. Xu, Z. Lin, J. Liang, F. S. Park, A. Ghosh, K. Yu, University Zhuang, National University of Defense of Maryland, College Park, College Technology, Changsha, China Park, MD

Chaired by: K. KAILASANATH, Naval Research Laboratory 1300 hrs 1330 hrs AIAA-2012-4030 AIAA-2012-4031 Active Control of Fuel-Flexible Experimental Investigation Combustor Using Alternative on Detonation Initiation Fuels Mechanism by Hot Jets



Hanover F

Cortland

Diane Hooie Senior Advisor, Energy Delivery Technologies Division National Energy Technology Laboratory Department of Energy

Hanover B

66

Glenn Research Center, Cleveland, OH

1400 hrs AIAA-2012-4044 Analysis on Micro-Solid Propellant Motor’s Size Effect

Inc., Pasadena, CA; R. Estes, NASA R. Estes, NASA Goddard Space Flight Goddard Space Flight Center, Center, Greenbelt, MD; J. Harris, Cobham Pressure Technology Solutions, Greenbelt, MD Westminster, MD; N. Moore, Angeles Crest Engineering, Inc., Pasadena, CA

Chaired by: A. LOPEZ, The Boeing Company and G. GRAYSON, The Boeing Company 1330 hrs 1400 hrs 1300 hrs AIAA-2012-4046 AIAA-2012-4047 AIAA-2012-4045 Cryogenic Propellant Summary of the Development Development and of a Demiseable Composite Implementation of a Process Management during Ballistic Overwrapped Hydrazine Tank for Producing a Highly Flight Phases Wettable Aluminum PMD for P. Behruzi, J. Klatte, N. Fries, G. for the Global Precipitation Netter, Astrium, Bremen, Germany; the GPM Hydrazine Tank Measurement Mission from N. Moore, Angeles Crest Engineering, A. Sirbi, ESA, Paris, France Concept to Delivery


Tanks II: Optimization and Control

Solid Rocket Motor Ignition Evaluation and Design

1430 hrs AIAA-2012-4041 Generation after Next Propulsor Research: Robust Design for Embedded Engine Systems

D. Arend, NASA Glenn Research Center, Cleveland, OH; G. Tillman, United Technologies Research Center, M. Celestina, J. Fabian, S. Kulkarni, NASA Glenn Research Center, Cleveland, East Hartford, CT; W. O’Brien, Virginia Polytechnic Institute and State OH; D. Althausen, ASRC Aerospace University, Blacksburg, VA Corporation, Cleveland, OH

1400 hrs AIAA-2012-4040 NASA Environmentally Responsible Aviation High Overall Pressure Ratio Compressor Research - Pre-Test CFD

NASA Environmentally Responsible Aviation, propulsion technology

Y. Wang, S. Li, Beijing Institute of A. Kakami, H. Taketoshi, S. Ishihara, V. Sanal Kumar, Kumaraguru College Technology, Beijing, China T. Tachibana, Kyushu University, of Technology, Coimbatore, India; Kitakyushu, Japan R. Basavanahalli, Indian Institute of Science, Bangalore, India

Chaired by: M. LANGHENRY, Raytheon Missile Systems 1300 hrs 1330 hrs AIAA-2012-4042 AIAA-2012-4043 Laser assisted combustion of solid Ignition Transient of Dualpropellant for a 100 mN class Thrust Solid Propellant Rocket variable thrust rocket motor Motors - A Review


K. Suder, NASA Glenn Research Center, Cleveland, OH

Chaired by: K. SUDER, NASA Glenn Research Center 1300 hrs 1330 hrs AIAA-2012-4038 AIAA-2012-4039 Tip Vortex and Wake Overview of the NASA Environmentally Responsible Characteristics of a Aviation Project’s Propulsion Counterrotating Open Rotor D. Van Zante, M. Wernet, NASA Technology Portfolio


Roswell

Techwood

Hanover G

67

Hydrogen Propulsion: Centaur-Saturn to J2X and Beyond

Piedmont

Suntan to Centaur and Beyond, Evolution of Hydrogen Propulsion Joaquin Castro Pratt & Whitney-Rocketdyne

S. Spencer, P. Jaffe, B. Nguyen, Naval Research Laboratory, Washington, DC

1500 hrs AIAA-2012-4050 Thermal Analysis of Spacebased Solar Power System Study Photovoltaic RF to DC Antenna Module (PRAM)

AIAA-2012-4053 Hydrogen Production by Using Circulating Fluidized-Bed Reactor

1430 hrs

A. Ingenito, F. Gamma, A. Agresta, University of Rome “La Sapienza”, Rome, Italy; R. Andriani, Technical University of Turin, Turin, Italy

1500 hrs AIAA-2012-4054 A Comparative Study of Combustion between Biofuels and Fossil Fuels

Fuels Production and Air Pollution Abatement

M. Gibson, D. Jaworske, NASA Glenn Research Center, Cleveland, OH; J. Sanzi, Sest, Inc., Middleburg Heights, OH; D. Ljubanovic, Gilcrest Electric, Elyria, OH

1430 hrs AIAA-2012-4049 Thermosyphon Flooding Limits in Reduced Gravity Environments

H. Molintas, University of Maryland, Y. Achawangkul, Mie University, College Park, College Park, MD Tsu, Japan

AIAA-2012-4052 Thermal Cracking of Tars in a Continuously Fed Reactor with Steam

1400 hrs

Chaired by: A. KARABEYOGLU, Space Propulsion Group Inc. and W. LEAR, University of Florida

Tuesday, 31 July 2012 135-EERE-4

K. Saviers, S. Hodson, Purdue University, West Lafayette, IN; J. Salvador, General Motors Corporation, Warren, MI; L. Kasten, Air Force Research Laboratory, Wright-Patterson AFB, OH; T. Fisher, Purdue University, West Lafayette, IN

AIAA-2012-4048 Carbon Nanotube Arrays for Enhanced Thermal Interfaces to Thermoelectric Modules

1400 hrs

Hydrogen-Based Propulsion at Aerojet, M-1 and NERVA to Next Generation Systems John M. Cramer Project Engineering, Aerojet-Sacramento

A. Karabeyoglu, B. Evans, B. Cantwell, Space Propulsion Group, Inc., Sunnyvale, CA; D. Micheletti, Montana Aerospace Development Association, Butte, MT

1530 hrs AIAA-2012-4055 Development of Ammonia Based Fuels for Environmentally Friendly Power Generation

J. Mehta, J. Charneski, M. Sampson, BELCAN Corporation, Cincinnati, OH

1530 hrs AIAA-2012-4051 Unmanned Aerial Systems (UAS) Thermal Management Needs, Current Status, and Future Innovations

Aerospace and Terrestrial Power Systems Thermal Management I

Moon to the Solar System, Evolution of Hydrogen Rocket Engines Brian Anderson Advanced Programs, Rocketdyne

Chaired by: C. TARAU, Advanced Cooling Technologies and S. SPENCER, Naval Research Laboratory


Taming Liquid Hydrogen Lawrence J. Ross, Retired Director, NASA Lewis/Glen

Lessons Learned in the Early Days of Liquid Rocketry - Detonation is Not Preferred. Chuck Ehresman Professor Emeritus Purdue University B47 ATO, Aerobee, BOMARC, Curtiss-Wright XLR25 on Bell X-2, liquid fueled RATOs. (Video with commentary by B. J. Austin)

Introduction and Comments Robert L. Sackheim

Dunwoody

Lenox

Hydrogen Propulsion: Mission Enabling, Going Forward, Handle With Care Lawrence Dale Thomas NASA MSFC Associate Director - Technology

More than a “history session:” The U.S. liquid propulsion capability is at a crossroads, i.e., do we rest on prior laurels with our present systems and depend on other countries for major parts of what we need in the future? Or do we pay the price and make the long-term commitments for an effective U.S. internal capability that satisfies our national and commercial requirements? What succeeded in the 1960s and 1970s established a level of excellence in hydrogen propulsion, a capability which has been maintained and added upon. These lessons learned are the stepping-stones to a greater capability for U.S. propulsion and will help shape our nation’s future directions. -- Dr. Leonard Caveny

Chaired by: K. PUGMIRE, Spincraft and B. AUSTIN, IN Space LLC

Tuesday, 31 July 2012 133-LP-18 1300 - 1500 hrs

68

P. Tsvetkov, Texas A&M University, College Station, TX

California Institute of Technology, Pasadena, CA; S. Oleson, NASA Glenn Research Center, Cleveland, OH

X. Wang, W. Fabanich, NASA Glenn Research Center, Cleveland, OH; P. Schmitz, Power Computing Solutions, Inc., Cleveland, OH

J. Snyder, J. Brophy, R. Hofer, D. Goebel, I. Katz, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

S. Laughery, M. Butler, Johns Hopkins University Applied Physics Laboratory, Laurel, MD

1500 hrs AIAA-2012-4059 The RBSP Spacecraft Power System Design and Development

North Ridgeville, OH; T. Kerslake, NASA Glenn Research Center, Cleveland, OH

S. Hutchison, Reaction Engines, Ltd., Oxford, United Kingdom

Bennett, Teledyne Energy Systems, Inc., Hunt Valley, MD

T. Hammel, R. Bennett, Teledyne Energy Systems, Inc., Hunt Valley, MD; W. Otting, Pratt & Whitney, Canoga Park, CA; S. Keyser, R. Sievers, Teledyne Energy Systems, Inc., Hunt Valley, MD

1530 hrs AIAA-2012-4063 Multi-Mission Radioisotope Thermoelectric Generator (MMRTG): Proven Power for W. Otting, L. Gard, Pratt & Whitney, Next Generation Radioisotope Canoga Park, CA; T. Hammel, R. Power Systems

AIAA-2012-4062 Preparation of the MMRTG for the Mars Science Laboratory Mission

1500 hrs

EP Mission Analysis and Concepts

S. Wilson, NASA Glenn Research Center, Cleveland, OH

AIAA-2012-4061 Performance of an Advanced Stirling Convertor Based on Heat Flux Sensor Measurements

1430 hrs

Chaired by: C. GARNER, Joint Propulsion Laboratory, California Institute of Technology and J. SNYDER, Jet Propulsion Laboratory, California Institute of Technology 1630 hrs 1700 hrs 1600 hrs AIAA-2012-4067 AIAA-2012-4068 Oral Presentation (Invited) End-of-Life Power Implication Spacecraft Conceptual Design Experimental Investigation of for Returning Entire Neara Direct-Drive Hall Thruster of Low-Thrust Geocentric Earth Asteroids and Solar Array System at Transfer J. Dankanich, Gray Research, Inc., J. Brophy, Jet Propulsion Laboratory, Power Levels up to 10 kW


G. Carr, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

1430 hrs AIAA-2012-4058 Mars Science Laboratory (MSL) Power System Architecture

1530 hrs Oral Presentation (Invited) Revolutionary Reaction Engines: SABRE and Skylon

An Overview of the Interagency Advanced Power Group (IAPG)

1500 hrs Panel Discussion

Spacecraft Power System Design

M. Cuvelier, P. Tsvetkov, Texas A&M University, College Station, TX

1430 hrs AIAA-2012-4056 U-235 Prompt Neutron Fission Spectrum Data Sensitivity/ Uncertainty Effects in Fuel Cycle Performance Parameters

Nuclear Power Technologies and Fuels II

Stirling/Radioisotope Power System Design, Modeling and Analysis

L. Roufberg, A. Baisden, Johns Hopkins University Applied Physics Laboratory, Laurel, MD

1400 hrs AIAA-2012-4057 Solar Probe Plus (SPP) Spacecraft Power System

Chaired by: P. CORNELL, NASA Glenn Research Center and T. REID, NASA Glenn Research Center 1400 hrs AIAA-2012-4060 Advanced Stirling Radioisotope Generator thermal power model in Thermal Desktop SINDA/FLUINT analyzer

Tuesday, 31 July 2012 138-EC-5

Chaired by: J. WITCHER, Sandia National Labs and A. SALIM

Tuesday, 31 July 2012 137-APS-4

Chaired by: R. BEHERA and M. HOUTS, NASA Marshall Space Flight Center 1400 hrs Oral Presentation (Invited) TRU-Fueled HTRs for Advanced Power Applications

Tuesday, 31 July 2012 136-TNES-2

Regency VI

Fairlie

Greenbriar

Kennesaw

69

Niskayuna, NY; W. Adis, M. Mack, General Electric Company, Schenectady, NY

B. Khandelwal, Cranfield University, Cranfield, United Kingdom

1630 hrs AIAA-2012-4070 Preliminary Study of a Novel Gas Turbine Combustor Concept based on Hydrogen Synthesis from Kerosene Reformation

Rabigh, Saudi Arabia N. Maruyama, Y. Masuda, Mie University, Tsu, Japan; K. Nagata, Kouwakougyo Company, Ltd., Yokkaichi, Japan; Y. Ito, M. Hirota, Mie University, Tsu, Japan

Heights, OH

Chaired by: J. MEHTA, President and M. CHOI, NASA Goddard Space Flight Center 1630 hrs 1700 hrs 1600 hrs AIAA-2012-4077 AIAA-2012-4078 AIAA-2012-4076 Temperature Stabilization of Forced Convection Heat Titanium-Water Thermosyphon Pulsating Flow in High Pressure Transfer for Falling Film over Gamma Radiation Exposure Field Using Coaxial Tube Heat Hot Horizontal Tubes and Results Exchanger with Liquid Oil Tuner H. Sait, King Abdul Aziz University, J. Sanzi, Sest, Inc., Middleburg


Niskayuna, NY

Advanced Seal Technology II

M. Gauer, German Aerospace Center (DLR), Göttingen, Germany; D. Telitschkin, EADS, Ottobrunn, Germany; Y. Battoneau, National Center for Scientific Research (CNRS), Paris, France; H. Johansson, Nanospace AB, Uppsala, Sweden; M. Ivanov, NPO Mashinostroyenia, Moscow, Russia; P. Palmer, University of Surrey, Guildford, United Kingdom; R. Wiegerink, University of Twente, Enschede, The Netherlands

1730 hrs AIAA-2012-4072 PRECISE - Development of a MEMS-based Monopropellant Micro Chemical Propulsion System

Advanced Propulsion Concepts III

Aerospace and Terrestrial Power Systems Thermal Management II

P. Dunlap, B. Steinetz, NASA Glenn Research Center, Cleveland, OH

D. Kirtley, A. Pancotti, J. Slough, C. Pihl, MSNW, LLC, Redmond, WA

1700 hrs AIAA-2012-4071 Steady Operation of an FRC Thruster on Martian Atmosphere and Liquid Water Propellants

Chaired by: B. STEINETZ, NASA Glenn Research Center and P. DUNLAP, NASA Glenn Research Center 1600 hrs 1630 hrs 1700 hrs AIAA-2012-4073 AIAA-2012-4074 AIAA-2012-4075 Compliant Plate Seals: Static Manufacturing of Compliant A Comparison of Candidate Tests Plate Seals Seal Designs for Future H. Deo, General Electric Company, H. Deo, General Electric Company, Docking Systems

Tuesday, 31 July 2012 142-SCP-2

H. Huang, Self, Webster, TX

Chaired by: J. ROBINSON 1600 hrs AIAA-2012-4069 A Misunderstood/Overlooked/ Traditional/Useful Newly Discovered Force

Tuesday, 31 July 2012 141-APC-3

Lenox

Inman

Hanover A

70

Glenn Research Center, Cleveland, OH

Cathodes

Catherine Ferrie Director Xworx & Test and Evaluation Bell Helicopter

A. Ambekar, A. Chowdhury, Indian Institute of Technology Mumbai, Mumbai, India

D. Cheng, X. Fan, Chinese Academy A. Roy, C. Segal, University of of Sciences, Beijing, China Florida, Gainesville, Gainesville, FL

Chaired by: J. OEFELEIN, Sandia National Laboratories and T. NGUYEN, Aerojet 1630 hrs 1700 hrs 1600 hrs AIAA-2012-4090 AIAA-2012-4091 AIAA-2012-4089 Quasi-1D Compressible Flow of Supercritical Mixing in Single Combustion of Blended Hydrocarbon Fuel and Dual Component Systems Monopropellants


Chaired by: J. LOCKE, United Technologies Research Center and E. JACOB, GTL 1630 hrs 1700 hrs 1600 hrs AIAA-2012-4085 AIAA-2012-4086 AIAA-2012-4084 The Effect of Unsteady Entropy Analysis of the impact of heat On the Sidewall Boundary losses on an unstable model Layer of Transverse Waves on Combustion Instability E. Jacob, G. Flandro, P. Gloyer, GTL rocket-engine combustor using in Simulated Liquid Rocket Company, Tullahoma, TN Large-Eddy Simulation Engines

R. Garby, Fluid Mechanics Institute of C. Haddad, J. Majdalani, University Toulouse (IMFT), Toulouse, France; of Tennessee Space Institute, L. Selle, T. Poinsot, National Center Tullahoma, TN for Scientific Research (CNRS), Toulouse, France

Susan Gorton Project Manager NASA Subsonic Rotary Wing Project


Panelists:

F. Álvarez, C. White, A. Delgado, J. Frias, A. Narayana Swamy, E. Shafirovich, University of Texas, El Paso, El Paso, TX

1730 hrs AIAA-2012-4092 Combustion of JSC-1A Lunar Regolith Simulant Mixed with Magnesium

Fundamental Combustion Processes

1800 hrs AIAA-2012-4088 Comparison Between Simulation and Measurement of Self-Excited Combustion Instability

J. Hardi, M. Oschwald, German Aerospace Center (DLR), T. Feldman, M. Harvazinski, C. Lampoldshausen, Germany; B. Dally, Merkle, W. Anderson, Purdue University of Adelaide, Adelaide, University, West Lafayette, IN Australia

1730 hrs AIAA-2012-4087 Coupling Behaviour of LOx/ H2 Flames to Longitudinal and Transverse Acoustic Instabilities

Combustion Instability I

Richard F. Spivey Director U.S. Army Aeroflightdynamics Directorate


J. Polk, Jet Propulsion Laboratory, M. Coletti, S. Gabriel, University of Kingdom; S. Gabriel, University of Southampton, Southampton, United Southampton, Southampton, United California Institute of Technology, Kingdom Pasadena, CA Kingdom

Moderator: George A Bobula, Chief Engineer, Propulsion Division, Aviation Engineering Directorate, AMRDEC

Tuesday, 31 July 2012 145-JPC-9 1600 - 1830 hrs

D. Goebel, E. Chu, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

Chaired by: I. MIKELLIDES, Jet Propulsion Laboratory, California Institute of Technology and Y. RAITSES, Princeton Plasma Physics Laboratory 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2012-4079 AIAA-2012-4080 AIAA-2012-4081 AIAA-2012-4082 AIAA-2012-4083 High Current Hollow Cathode Insert Temperature A Hollow Cathode Thruster Exploration of RF-Controlled High High Current Lanthanum Performance Model Current Density Cathode Concepts Hexaboride Hollow Cathode Development at NASA Glenn Measurements of a 180A M. Plasek, B. Jorns, E. Choueiri, Hollow Cathode for the HiPER D. Frollani, M. Coletti, Mars for 20-to-100 kW Class Hall Research Center Space, Ltd., Southampton, United Princeton University, Princeton, NJ; H. Kamhawi, J. Van Noord, NASA Thrusters Project


Steve Weiner Director Engineering Sciences Sikorsky Aircraft Corporation

Hanover B

Spring


Harold Rosenstein Chief Engineer Advanced Mobility Boeing Phantom Works

The Learning Center

71

Benha University, Cairo, Egypt

E. Khalil, W. Sweida, Cairo University, Cairo, Egypt

B. Pavlov, L. Qiao, Purdue University, O. Gracia, M. Khan, A. Choudhuri, N. West Lafayette, IN Love, University of Texas, El Paso, El Paso, TX

1700 hrs AIAA-2012-4095 Low-Temperature Oxidation of Methanol with the Assistance of Platinum Nanoparticles

J. Spero, J. Leylegian, Manhattan College, Bronx, NY

S. Srinivasan, S. Menon, Georgia Institute of Technology, Atlanta, GA

M. Ilie, University of Central Florida, Orlando, FL

1700 hrs AIAA-2012-4110 Analysis of Reduced Order Chemical Mechanisms for Oxygen-enriched Combustion of Methane and n-decane

Combustion Modeling II

C. Lee, Y. Na, Konkuk University, Seoul, South Korea; H. Koo, Seoul National University, Seoul, South Korea

1800 hrs AIAA-2012-4108 The effect of a block on flow oscillations near the fuel surface with wall blowing

Fuel Regression Characterization

M. Abdelghanny, A. Shahin, O. Abdellatif, M. Abdraboo, S. Ayad, Benha University, Cairo, Egypt

1730 hrs AIAA-2012-4100 Performance and Flow Field Analysis for a Diffuser Pump at Different Flow and Design Parameters

T. Sakurai, Tokyo Metropolitan P. Chidambaram, A. Kumar, Indian S. Yuasa, N. Shiraishi, K. Hirata, Institute of Technology Madras, Chennai, Tokyo Metropolitan University, Hino, University, Hino, Japan India Japan

Chaired by: J. LEYLEGIAN, Manhattan Colege 1630 hrs 1600 hrs AIAA-2012-4111 AIAA-2012-4109 From Flamelet to Distributed/ Development of a Chemical Kinetic Model to Describe the Broken Reaction Zone Regimes: Investigations Using Endothermic Reforming of the Linear Eddy Model Logistical Fuels


University, Hiratsuka, Japan

Energy-Efficient Systems II

A. Singh, A. Eshaghi, M. Yu, University of Maryland, College Park, College Park, MD; K. Bryden, Iowa State University, Ames, IA; A. Gupta, University of Maryland, College Park, College Park, MD

1730 hrs AIAA-2012-4096 Acoustic Source Localization using Microphone Arrays by TDOA Method

Emerging Fossil Energy Technologies

Chaired by: A. KARABEYOGLU, Space Propulsion Group Inc. and J. MICHLITSCH, The Aerospace Corporation 1630 hrs 1700 hrs 1730 hrs 1600 hrs AIAA-2012-4105 AIAA-2012-4106 AIAA-2012-4107 AIAA-2012-4104 Regression Rate Characteristics A Numerical Study on the Controlling Parameters for Effectiveness of Concaveof Paraffin-based Fuel under Regression Rate of Hybrid Rocket Fuel Regression Rate of convex Surface Grain for Swirled Oxidizer Flow Motors Using a Combination of Swirling-oxidizer-flow-type Hybrid Rocket Combustion I. Nakagawa, K. Shinohara, Tokai S. Hatagaki, Y. Saburo, K. Hirata, Enhancement Techniques Hybrid Rocket Engine


Chaired by: E. KHALIL, Cairo University and T. BRADLEY, Colorado State University 1600 hrs 1630 hrs 1700 hrs AIAA-2012-4097 AIAA-2012-4098 AIAA-2012-4099 Numerical Investigations of Effect of Shorted Blade Numerical Investigations of Flow Patterns and Thermal Circumferential Positions Air Flow Patterns and Thermal Comfort in Air-Conditioned on Centrifugal Pump Comfort in an Ice-Cream Lecture Room Characteristics Factory Conditioned by T. Abou Dief, M. Fouad, E. Khalil, M. Abdelghanny, M. Shehata, A. Conventional Air Conditioning Cairo University, Cairo, Egypt Abd Elhafez, M. Abdraboo, S. Ayad, or Radiant Cooling Systems

Tuesday, 31 July 2012 149-EERE-5

Paso, TX

Chaired by: D. LILLEY, Oklahoma State University and M. KHAN 1600 hrs 1630 hrs AIAA-2012-4093 AIAA-2012-4094 Development of Thermoelectric Experimental Study of Thermoelectric Properties of Temperature Sensors J. Kuchle, K. Hassan, N. Love, Randomly Distributed SWCNTs University of Texas, El Paso, El and SiC Nanoparticles

Tuesday, 31 July 2012 148-TFES-4

Hanover D

University

Greenbriar

Kennesaw

72

A. Pancotti, J. Slough, D. Kirtley, MSNW, LLC, Redmond, WA; M. Pfaff, ; C. Pihl, G. Votroubek, MSNW, LLC, Redmond, WA

J. Cassibry, R. Cortez, M. Stanic, R. Hatcher, M. Beattie, University of Alabama, Huntsville, Huntsville, AL; W. Seidler, The Boeing Company, Huntsville, AL; R. Adams, G. Statham, NASA Marshall Space Flight Center, Huntsville, AL

1700 hrs AIAA-2012-4114 The Case and Development Path for Fusion Propulsion

A. Trejo, S. Flores, A. Choudhuri, University of Texas, El Paso, El Paso, TX

H. Negishi, Y. Daimon, H. Kawashima, N. Yamanishi, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan

G. Williams, Ohio Aerospace Institute, Cleveland, OH; B. Stiegemeier, Artic Slope Research Corporation, Cleveland, OH

1730 hrs AIAA-2012-4124 Vaporization and Zonal Mixing in Performance Modeling of Advanced LOX-Methane Rockets

Exploration Agency (JAXA), Tsukuba, Japan; T. Tomita, M. Sasaki, Japan Aerospace Exploration Agency (JAXA), Kakuda, Japan; H. Negishi, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; T. Kaneko, Mitsubishi Heavy Industries, Ltd., Nogoya, Japan

Heat Tranfer, Cooling and Combustion of Methane Engines

Chaired by: S. FORDE, Aerojet and M. MEYER, NASA Glenn Research Center 1630 hrs 1700 hrs 1600 hrs AIAA-2012-4121 AIAA-2012-4122 AIAA-2012-4120 Verification of Prediction An Experimental Investigation Flowfield and Heat Transfer Methods for Methane Heat on the Heat Transfer Characteristics of Cooling Transfer Characteristics Characteristics of Liquid Channel Flows in a MethaneH. Kawashima, Japan Aerospace Methane Cooled Thrust Chamber

Center for Scientific Research (CNRS), R. Washeleski, E. Meyer, L. King, Orléans, France; M. Merino-Martinez, E. Michigan Technological University, Ahedo, Technical University of Madrid, Houghton, MI Madrid, Spain

M. Patino, L. Chu, R. Wirz, University of California, Los Angeles, Los Angeles, CA

1800 hrs AIAA-2012-4119 Well-Characterized Plasma Experiments for Validation of Computational Models

Hall Thruster Physics III


D. Herman, R. Shastry, W. Huang, M. Nakles, W. Hargus, Air Force G. Soulas, H. Kamhawi, NASA Glenn Research Laboratory, Edwards AFB, Research Center, Cleveland, OH CA; J. Delgado, R. Corey, Space Systems/Loral, Palo Alto, CA

Fusion and Alternative Nuclear Concepts

1730 hrs AIAA-2012-4118 Laser Thomson Scattering Measurements of Electron Temperature and Density in the Near-Field Plume of a HallK. Dannenmayer, S. Mazouffre, National Effect Thruster

Chaired by: J. POLK, Jet Propulsion Laboratory and D. BROWN, Air Force Reseach Laboratory 1600 hrs 1630 hrs 1700 hrs AIAA-2012-4115 AIAA-2012-4116 AIAA-2012-4117 Electrostatic Probe A Performance and Plume Hall Effect Thruster Plasma Measurements in the NearComparison of Xenon and Plume Characterization with field Plume of the NASA 300M Krypton Propellant on the Probe Measurements and Hall Thruster SPT-100 Self-Similar Fluid Models


T. Kammash, Self, Ann Arbor, MI

Chaired by: J. CASSIBRY and R. SEDWICK, University of Maryland 1600 hrs 1630 hrs AIAA-2012-4112 AIAA-2012-4113 Fusion Hybrid Rocket for Moon Mission Design Architecture for the Fusion Driven Rocket Tourism

Tuesday, 31 July 2012 154-NFF-6

Vinnings

Cortland

Hanover E

73

Gulbinska, S. Santee, C. Deroy, Yardney Technical Products, Pawcatuck, CT

Products, Longmont, CO; R. Buckle, EnerSys/ABSL Space Products, Culham, United Kingdom

The Future of Smart Grid in the United States and Abroad

H. Naito, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; T. Hoshino, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; T. Tani, Mitsubishi Heavy Industries, Ltd., Kobe, Japan

1730 hrs AIAA-2012-4128 Study on High Pressure Water Electrolysis for Energy Storage Device of Space Systems

High-Energy Storage for Space Application

Marshall, NASA Glenn Research Center, Cleveland, OH

1730 hrs AIAA-2012-4132 Laser Ignition of a Research 200N RCS LOx/GH2 and LOx/ GCH4 Engine

1800 hrs AIAA-2012-4133 Development and Testing of a Methane/Oxygen Catalytic Microtube Ignition System for Rocket Propulsion

Ignition of Methane and Hydrogen Engines

C. Manfletti, German Aerospace Exploration Agency (JAXA), Tsukuba, C. Manfletti, German Aerospace Center (DLR), Hardthausen, Germany M. Deans, S. Schneider, NASA Glenn Japan; J. Culbertson, J. Torres, E. Center (DLR), Hardthausen, Germany Research Center, Cleveland, OH Besnard, California State University, Long Beach, CA

Chaired by: J. SAUER, Orbital Technologies Corporation and T. POURPOINT, Purdue University 1600 hrs 1630 hrs 1700 hrs AIAA-2012-4129 AIAA-2012-4130 AIAA-2012-4131 Spark Ignition Characteristics Experimental Study of Low Low Ambient Pressure of a LO2/LCH4 Engine at Frequency Plasma for Liquid Injection and Consequences Altitude Conditions Oxygen and Methane Ignition on Ignition of Liquid Rocket J. Kleinhenz, C. Sarmiento, W. T. Nagata, Japan Aerospace Engines


Moderators: William E. Lear, University of Florida, Gainesville, FL and Michael Choi, NASA Goddard Space Flight Center, Greenbelt, MD Speakers: 1625 - 1650 hrs 1650 - 1715 hrs 1715 - 1740 hrs 1600 - 1625 hrs Reji Kumar Pillai Scott Duncan Egon Ortjohann Anh Vu Smart Cities Program Manager President - India Smart Grid Forum School of Aerospace Engineering Head of Power Systems and Power Economics Department ERDF Distribution (a PPP initiative of Govt of India) Georgia Institute of Technology South Westphalia University of Applied Sciences France India USA Germany

1740 - 1805 hrs José Eduardo Azarite Director of Marketing CPqD Brazil

Fairlie

Roswell

Dunwoody

1805 - 830 hrs Takashi Hikihara Professor of Department of Electrical Engineering Kyoto University Japan

Smart Grid has become a critical agenda item around the globe. The speakers will present their views on the future of Smart Grid in the United States and abroad. They will focus on opportunities and challenges.

Chaired by: W. LEAR, University of Florida and M. CHOI, NASA Goddard Space Flight Center


E. Burke, Space Information Laboratories, Santa Maria, CA

Chaired by: R. SHAW, Lockheed Martin Corporation and J. TROUTMAN, EnerSys/ABSL Space Products 1600 hrs 1630 hrs 1700 hrs AIAA-2012-4125 AIAA-2012-4126 AIAA-2012-4127 Lithium Intelli-Pack Battery: A Next Generation Lithium-ion Low Temperature Cycling Performance of the SONY 18650 Modular and Scalable Smart Cell Chemistry for Space Hard Carbon Mandrel Cell Battery for Multiple Aerospace Applications R. Gitzen Danner, F. Puglia, M. J. Troutman, EnerSys/ABSL Space Platforms

Tuesday, 31 July 2012 157-ES-1

74

C. Yoon, S. Heister, P. Santos, O. Campanella, Purdue University, West Lafayette, IN

A. Rettenmaier, S. Heister, Purdue University, West Lafayette, IN

R. Andriani, Technical University of Milan, Milan, Italy; F. Gamma, University of Rome “La Sapienza”, Rome, Italy; U. Ghezzi, Technical University of Milan, Milan, Italy

M. Corbett, Air Force Research Laboratory, Wright-Patterson AFB, OH

1730 hrs Oral Presentation (Invited) Shane Bunnang

1800 hrs Oral Presentation (Invited) Joel Malo-Molina

Young Professionals’ Vision for the Future of Propulsion

Chaired by: J. CONVERY, GE Aviation and J. SORDYL, Williams International 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Nicole Key John McKinnis Matt Billingsley

Engine Performance

Solid Rocket Motor Burn Rate Analysis

Non-Conventional Concepts for Rocket Engines


Technical University of Turin, Turin, Italy

Chaired by: D. JENSEN, Rolls-Royce Corporation and R. BRUCKNER, NASA Glenn Research Center 1600 hrs 1630 hrs 1700 hrs AIAA-2012-4139 AIAA-2012-4140 AIAA-2012-4142 Optimization of Civil Turbofan Off-Design Performances of a Large-Scale Transient Loading with Evolutionary Algorithms Gas Turbine Engine with Heat of a Three Stream Variable L. Casalino, D. Pastrone, F. Simeoni, Recovery and Intercooling Cycle Engine


Rancho Cordova, CA

Chaired by: B. LEARY, ATK Mission Systems 1600 hrs 1630 hrs AIAA-2012-4136 AIAA-2012-4138 Universal Subscale FixedExperimental Study of Nozzle Burning Rate Analysis Erosive and Dynamic Burning Tool in Polybutadiene Based M. Hinkelman, J. Goldin, Aerojet, Composite Propellants


West Lafayette, IN

Chaired by: P. ALLIOT, SNECMA and D. SARGENT, Federal Aviation Administration 1600 hrs 1630 hrs AIAA-2012-4134 AIAA-2012-4135 Valveless Detonation Concepts Plain-Orifice Injector Flow Characteristics with Rheological for Space Exploration B. Kan, S. Heister, Purdue University, Hysteresis


Regency V

Hanover G

Techwood

Piedmont

75

J. Connolly, S. Garg, NASA Glenn Research Center, Cleveland, OH; A. Chicatelli, Analex Corporation, Cleveland, OH

Wednesday, 1 August 2012 166-JPC-10 0800 - 0900 hrs


Wednesday, 1 August 2012 165-IECEC-10 0800 - 0900 hrs

Center, Cleveland, OH

Chaired by: D. CULLEY, NASA Glenn Research Center 1600 hrs 1630 hrs AIAA-2012-4255 AIAA-2012-4257 Overview of Propulsion Model-Based Engine Control of Controls and Diagnostics a Commercial Class Turbofan Research at NASA Glenn Engine Using an Optimal Tuner S. Garg, NASA Glenn Research Approach

Tuesday, 31 July 2012 199-ABPSI-13/GTE-23

L. Foster, J. Saunders, NASA Glenn Cleveland, OH Research Center, Cleveland, OH; B. Sanders, L. Weir, TechLand Research, Inc., North Olmsted, OH

G. Kopasakis, J. Connolly, NASA Glenn Research Center, Cleveland, OH; K. Woolwine, Florida State University, Gainesville, FL

Y. Guo, J. Lu, S. Zhang, Northwestern Polytechnical University, Xi’an, China

Wednesday

1730 hrs 1800 hrs AIAA-2012-4259 Improved hybrid Kalman filter for in-flight aircraft engine performance estimation

1800 hrs AIAA-2012-4147 Quasi One-Dimensional Unsteady Modeling of External Compression Supersonic Inlets

Turbine Engine Control

T. Herges, G. Elliott, J. Dutton, University of Illinois, UrbanaChampaign, Urbana, IL

1730 hrs AIAA-2012-4146 High-Speed Schlieren Analysis of Buzz in a RelaxedCompression Supersonic Inlet

High-Speed Inlets / Isolators I

Flight Testing: Increasing Value and Demand Dr. Wes Harris Charles Stark Draper Professor of Aeronautics and Astronautics Massachusetts Institute of Technology

Wednesday Opening Keynote

David Parekh Vice President of Research, Director United Technologies Research Center

IECEC Plenary Panel Aerospace Capabilities Applied to Solving Terrestrial Energy Problems...An Aerospace Industry View

Y. Guo, Northwestern Polytechnical University, Xi’an, China; L. Wang, Xi’an Aeroengine Controls Corporation, Xi’an, China; J. Lu, J. Wu, Northwestern Polytechnical University, Xi’an, China

1700 hrs AIAA-2012-4258 Fixed Dynamic Method for Transient-State Optimal Control Law Design of Aircraft Engine

Chaired by: T. O’BRIEN, Aerojet and B. MCKAY, Lockheed Martin Aeronautics 1600 hrs 1630 hrs 1700 hrs AIAA-2012-4143 AIAA-2012-4144 AIAA-2012-4145 A simulation scheme for Shock Train Position Control Highlights from a Mach 4 Experimental Demonstration turbine-based combined cycles in an Axisymmetric Scramjet inlet mode-transition control Combustor Flowpath of Inlet Mode Transition for Turbine Based Combined Cycle D. Le, D. Vrnak, J. Slater, E. Hessel, J. Donbar, Air Force Research NASA Glenn Research Center, Laboratory, Wright-Patterson AFB, OH Hypersonic Propulsion

Tuesday, 31 July 2012 164-HSABP/HYP-8/ ABPSI-10


Dunwoody

Hanover C

Regency VII

76

J. Csank, T. Stueber, NASA Glenn Research Center, Cleveland, OH

J. Chang, Harbin Institute of Technology, Harbin, China

C. Wey, ASRC Aerospace Corporation, Cleveland, OH; R. Howard, Arnold Engineering Development Center, Arnold AFB, TN; D. Bulzan, NASA Glenn Research Center, Cleveland, OH

Ziemba, NASA Langley Research Center, Hampton, VA; M. Dewitt, University of Dayton Research Institute, Dayton, OH; B. Knighton, Montana State University, Bozeman, MT; M. Timko, Aerodyne, Billerica, MA

Alternative Aviation Fuel Experiments (AAFEX) I & II

Y. Li, K. Zhang, X. Nan, Nanjing University of Aeronautics and Astronautics, Nanjing, China

1100 hrs AIAA-2012-4151 Design of hypersonic inward turning inlets with controllable Mach number distribution

High-Speed Inlets / Isolators II

J. Garcia, NASA Kennedy Space Center, Cape Canaveral, FL; C. McCleskey, T. Bollo, R. Rhodes, J. Robinson, Seal Beach, CA

1030 hrs AIAA-2012-4154 Exploration and Space Habitation Public Support

W. Knuth, KE, Inc., Huntsville, AL; J. Robinson, Seal Beach, CA; R. Rhodes, NASA Kennedy Space Rhodes, R. Lepsch, E. Henderson, J. Center, Cape Canaveral, FL; E. Henderson, NASA Johnson Space Robinson, Seal Beach, CA Center, Houston, TX

Chaired by: R. CHASE and J. ROBINSON 1000 hrs 0930 hrs AIAA-2012-4153 AIAA-2012-4152 A Systems Approach to Approach to an Affordable Developing an Affordable and Productive Space Space Ground Transportation Transportation System C. McCleskey, NASA Kennedy Space Architecture using a Center, Cape Canaveral, FL; R. Commonality Approach

Wednesday, 1 August 2012 170-APC-4

B. Anderson, A. Beyersdorf, NASA Langley Research Center, Hampton, VA

D. Thorpe, Exploration Partners, LLC, Mount Sterling, KY; J. Robinson,, Seal Beach, CA; R. Rhodes, NASA Kennedy Space Center, Cape Canaveral, FL

1100 hrs AIAA-2012-4155 Affordability Advantages in Integrating the Aircraft and Space Launch Operations

Advanced Propulsion Concepts IV

Chaired by: D. BULZAN, NASA Glenn Research Center and R. DEL ROSARIO, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Introduction, Background, Engine Performance and Solid and Volatile Engine Engine Exhaust Plume Objectives, and Experimental Gaseous Emissions from JP-8, Particulate Emissions from F-T, Measurements and Chemical Details of Alternative Aviation GTL, and CTL Fischer-Tropsch (FT), HEFA, JP-8, and Blends Evolution R. Miakelye, S. Herndon, Aerodyne, Fuel Experiments (AAFEX) I Hydroprocessed Esters and Fatty E. Corporan, Air Force Research Laboratory, Wright-Patterson AFB, OH; L. Billerica, MA and II Acids (HEFA), and Blends

Wednesday, 1 August 2012 168-GEPC-1/GTE-19

T. Kouchi, G. Masuya, Tohoku University, Sendai, Japan

Chaired by: M. BRADLEY, The Boeing Company & Technology and T. BERENS, Cassidian 0930 hrs 1000 hrs 1030 hrs AIAA-2012-4148 AIAA-2012-4149 AIAA-2012-4150 Real-time Unstart Prediction Quantification of Convection A Turbine Based Combined Velocity and Dominant Scale Cycle Engine Inlet Model and and Detection of Hypersonic Inlet Based on Recursive of Large-Scale Structures by Mode Transition Simulation High-Speed Schlieren Imaging Based on HiTECC Tool Fourier Transform

Wednesday, 1 August 2012 167-HSABP/HYP-9/ ABPSI-11

Hanover A

Roswell

Regency VII

77

S. Karl, German Aerospace Center (DLR), Göttingen, Germany; R. Stark, German Aerospace Center (DLR), Lampoldshausen, Germany

S. Gulli, L. Maddalena, University of Texas, Arlington, Arlington, TX; S. Hosder, Missouri University of Science and Technology, Rolla, MO

M. Ferlin, French Space Agency (CNES), Paris, France

1030 hrs AIAA-2012-4163 Assessment and Benchmarking of the Extendible Nozzle Systems in the Liquid Propulsion

Mark Anderson Director Platform Performance Technology The Boeing Company

Chaired by: T. GIEL, Jacobs Technology and D. PERIGO 0930 hrs 1000 hrs AIAA-2012-4164 AIAA-2012-4162 Numerical Investigation of Nozzle Design through Dual Bell Nozzle Flow Field Chemical Kinetics Coupled C. Genin, German Aerospace Center with Axis-Symetric Method of (DLR), Lampoldshausen, Germany; Characteristics

R. Young, R. Hartfield, Auburn University, Auburn, AL

Richard Christiansen Vice President Sierra Lobo

Wednesday, 1 August 2012 174-LP-23

Panelists:

Moderator: Dr. Victor Lebacqz, VICC Associates, Principal


Harbin, China

Compressors III

Douglas Bowers(invited) Chief Propulsion Division USAF AFRL

Nozzle Design

Dale Carlson General Manager, Technology Strategy GE Aviation


Aircraft, Aero-Engine and Hypersonic Vehicle Thermal Management

N. Smith, N. Key, Purdue University, West Lafayette, IN

1030 hrs AIAA-2012-4158 Vane Clocking Effects on Stall Margin in a Multistage Compressor

Chaired by: J. MEHTA, President and C. TARAU, Advanced Cooling Technologies 0930 hrs 1000 hrs 1030 hrs AIAA-2012-4159 AIAA-2012-4160 AIAA-2012-4161 Performance Analysis on Fuel Effects of Pressure on Heat Integrated Analysis for the Turbo-pump and Motor System Sink of n-Decane Design of Reusable TPS Based W. Zhou, Z. Jia, W. Bao, B. Yu, of Scramjet Engine on Variable Transpiration W. Bao, D. Zhang, J. Qin, W. Zhou, Harbin Institute of Technology, Cooling for Hypersonic Cruise Harbin, China Harbin Institute of Technology, Vehicles

Wednesday, 1 August 2012 172-TM-6

Beijing, China; V. Yang, Georgia X. Liu, R. Hou, D. Sun, X. Sun, Beijing University of Aeronautics and Institute of Technology, Atlanta, GA Astronautics, Beijing, China

Chaired by: V. CAPECE, University of Kentucky 0930 hrs 1000 hrs AIAA-2012-4156 AIAA-2012-4157 Application of Unsteady Vortex Flow Instability Inception Model of Compressors based Lift in Turbomachinery L. Du, X. Sun, Beihang University, on Eigenvalue Theory

Wednesday, 1 August 2012 171-GTE-20

John Langford CEO Aurora Flight Sciences

Fairlie

University


Thomas Irvine NASA Deputy Associate Administrator for Aeronautics Research Mission Directorate

Hanover F

78

R. Kiran, S. Wijeyakulasuriya, N. Mueller, Michigan State University, East Lansing, MI; J. Piechna, Warsaw University of Technology, Warsaw, Poland

K. Kawatsu, Y. Mihara, N. Tani, N. Yamanishi, K. Okita, Japan Aerospace Exploration Agency (JAXA), Ibaraki, Japan

University of Padova, Padova, Italy

Chaired by: J. CHENOWETH, CRAFT Tech 1000 hrs 0930 hrs AIAA-2012-4174 AIAA-2012-4173 Feasibility Study of MultiSPONGE: a Sounding Rocket objective Optimization of Experiment for PMDs M. Lazzarin, N. Bellomo, F. Barato, Subsystem Redundancy for Human-rated Launch Vehicle D. Paulon, F. Moretto, D. Rondini,

Wednesday, 1 August 2012 177-SCP-3

University-Purdue University Indianapolis, Indianapolis, IN

Engineering and Analysis for Propulsion Systems I

1100 hrs AIAA-2012-4172 High Energy Spark Discharges for Ignition

Pressure Gain Combustors

J. Leylegian, V. Tulino, Manhattan College, Bronx, NY

1100 hrs AIAA-2012-4168 Further Progress on a Kinetic Model Reduction Method for CFD Applications

Combustion Studies II

J. Kim, B. Sforzo, J. Seitzman, J. Jagoda, Georgia Institute of S. Wijeyakulasuriya, T. Elharis, M. Technology, Atlanta, GA Nalim, Indiana University-Purdue University Indianapolis, Indianapolis, IN

1030 hrs AIAA-2012-4171 Fuel Proximity Effect on HotJet Ignition in a Wave Rotor Constant Volume Combustor

1030 hrs AIAA-2012-4167 Numerical Studies on Combustion in a Film Cooled Semicryogenic Rocket Thrust Chamber

H. Huo, V. Yang, Georgia Institute of J. Prakash, Liquid Propulsion System Technology, Atlanta, GA Centre, Thiruvananthapuram, India; K. Roy, T. Krishnakumar, TKM College of Engineering, Kollam, India; G. Ramesh, J. Pisharady, P. Balachandran, R. Thomas, Liquid Propulsion System Centre, Thiruvananthapuram, India

1000 hrs AIAA-2012-4166 Supercritical LOX/Hydrogen Combustion of a Shear Coaxial Injector

Chaired by: J. SORDYL, Williams International 0930 hrs 1000 hrs AIAA-2012-4169 AIAA-2012-4170 Coupled Analysis of the Thermodynamic cycle Inlet and Fuel Systems of a efficiency enhancement in Wave Rotor Constant-Volume a Wave Disk Engine by reCombustor injection of combusted gas for K. Smith, M. Nalim, Indiana pre-compression


D. Foti, S. Menon, Georgia Institute of Technology, Atlanta, GA

Chaired by: C. CADOU 0930 hrs AIAA-2012-4165 Flame Stabilization Modes in Lean Premixed Swirl Stabilized Combustion

Wednesday, 1 August 2012 175-PC-14

Hanover D

Hanover G

Hanover B

79

D. Lilley, Lilley & Associates, Stillwater, OK

D. Escobar Anton, E. Ahedo, Technical University of Madrid, Madrid, Spain

S. Cho, University of Tokyo, Tokyo, Japan; K. Komurasaki, University of Tokyo, Kashiwa, Japan; Y. Arakawa, University of Tokyo, Tokyo, Japan

D. Lilley, Lilley & Associates, Stillwater, OK

1030 hrs AIAA-2012-4177 Application of the Fire Dynamics Simulator FDS Code to 10 Experimental Fires in the End Room of a Three-Room Structure with 60 Smoke Detectors

P. Stoltz, Tech-X Corporation, Boulder, CO; B. Penkel, J. Menart, Wright State University, Dayton, OH

Cairo, Egypt

A. Fahim, Electro-Mechanical Research Institute, Cairo, Egypt

Ningbo, China

Chaired by: E. KHALIL, Cairo University and J. DARKWA, University of Nottingham-Ningbo 1000 hrs 1030 hrs 0930 hrs AIAA-2012-4188 AIAA-2012-4189 AIAA-2012-4187 Air Flow Distribution Effects on Applicability of Enclosed Fog Effectiveness of a Solar Thermal Comfort Parameters Systems in Rural Development Absorption Cooling System in a Region [Study on Toshki-Egypt Low Carbon Building in an Air-Conditioned Room E. Bially, E. Khalil, Cairo University, Region] J. Darkwa, University of Nottingham,


M. Rayman, C. Garner, Jet Propulsion R. Tsukizaki, H. Koizumi, University Laboratory, California Institute of of Tokyo, Bunkyo, Japan; K. Technology, Pasadena, CA Nishiyama, H. Kuninaka, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan

Chaired by: J. FOSTER, University of Michigan and G. WILLIAMS, Ohio Aerospace Institute 0930 hrs 1000 hrs 1030 hrs AIAA-2012-4182 AIAA-2012-4183 AIAA-2012-4184 In-Flight Operation of the Plasma Diagnostics inside the Speed-up for a PIC-MCC Dawn Ion Propulsion System ECR Ion Thruster μ10 by Laser Disharge Chamber Plasma Through the Preparations For Absorption Spectroscopy with Computer Code S. Mahalingam, Y. Choi, J. Loverich, Escape From Vesta Optical Fiber Probes

Wednesday, 1 August 2012 180-EP-27

Y. Raitses, M. Griswold, L. Ellison, N. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ

Chaired by: O. DUCHEMIN, SNECMA and G. SOULAS, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2012-4179 AIAA-2012-4180 AIAA-2012-4016 Studies of rotating spoke and Low-frequency azimuthal Lifetime Simulation of an SPTbreathing types of oscillations stability analysis of Hall Type Hall Thruster by Using a in Hall thrusters thrusters 2D Fully Kinetic PIC Model


V. Kumar, P. Panda, H. Mongia, S. Naik, Purdue University, West Lafayette, IN

Chaired by: M. KHAN and S. GOLLAHALLI 0930 hrs 1000 hrs AIAA-2012-4175 AIAA-2012-4176 Application of BRANZFIRE to Innovative Approaches for a Variety of Realistic Burning Reducing CO2 Emissions Items in a Room Fire with of Aviation Engines Part 3: Advanced Brayton Cycle Smoke Detectors and Sprinkler Activation Times Optimization

Wednesday, 1 August 2012 178-TFES-5

S. Oghienko, V. Olendarev, S. Veryutin, National Aerospace University, Kharkiv, Ukraine

1130 hrs AIAA-2012-4181 Researches on Anomalous Electron Transportation in Hall Thruster Plasma

R. Shastry, M. Patterson, D. Herman, NASA Glenn Research Center, Cleveland, OH; J. Foster, University of Michigan, Ann Arbor, Ann Arbor, MI

1100 hrs AIAA-2012-4190 Investigation into Compacted Composite Micro-encapsulated Phase Change Energy Storage Material J. Darkwa, O. Su, University of Nottingham, Ningbo, China

1130 hrs AIAA-2012-4186 Current Density Measurements of an Annular-Geometry Ion Engine

Heating and Cooling of Buildings

T. Ise, H. Koizumi, University of Tokyo, Tokyo, Japan; K. Nishiyama, H. Kuninaka, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan

1100 hrs AIAA-2012-4185 Electric Field Measurement of ECR Ion Thruster ?10 with Optical Fiber Sensor

Ion Thrusters IV

A. Shabselowitz, A. Gallimore, University of Michigan, Ann Arbor, MI; P. Peterson, ElectroDynamic Applications, Inc.

1100 hrs AIAA-2012-4336 Performance of a Helicon Hall Thruster Operating with Xenon, Argon, and Nitrogen

Hall Thrusters IV

J. Xu, L. Qiao, J. Gore, Purdue University, West Lafayette, IN

1100 hrs AIAA-2012-4178 Detailed Numerical Modeling of Solar Coal Gasification in a Perfectly-stirred Reactor

Fossil Energy Numerical Modeling

Lenox

The Learning Center

Regency VI

Kennesaw

80

W. Ohmichi, University of Tokyo, Bunkyo, Japan; H. Kuninaka, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan

R. Shastry, W. Huang, D. Herman, A. Gonzales, Air Force Research G. Soulas, H. Kamhawi, NASA Glenn Laboratory, Edwards AFB, CA; M. Research Center, Cleveland, OH Scharfe, ERC, Inc., Edwards AFB, CA; W. Hargus, Air Force Research Laboratory, Edwards AFB, CA

M. Feldman, E. Choueiri, Princeton University, Princeton, NJ

1030 hrs AIAA-2012-4193 Single-Stage Faraday Accelerator with Radiofrequency Assisted Discharge Proof of Concept Experiment

University, Stanford, CA; G. Zilliac, NASA S. Eilers, T. Whitmore, M. Wilson, Z. Peterson, S. Eilers, S. Whitmore, Ames Research Center, Moffett Field, CA Z. Peterson, J. McCulley, Utah State Utah State University, Logan, UT University, Logan, UT

Chaired by: D. PASTRONE, Technical University of Turin and D. MYRE, U.S. Naval Academy 1000 hrs 1030 hrs 0930 hrs AIAA-2012-4199 AIAA-2012-4200 AIAA-2012-4198 Initial Experimental Development and Testing of Closed-Loop Thrust and Investigations of Self-Pressurizing the Regeneratively Cooled Pressure Profile Throttling of Propellant Dynamics Multiple Use Plug Hybrid (for) a Nitrous-Oxide HTPB Hybrid J. Zimmerman, B. Cantwell, Stanford Nanosats (MUPHyN) Motor Rocket Motor

Wednesday, 1 August 2012 184-HR-7

NASA Glenn Research Center, Cleveland, OH

P. Lemieux, California State Polytechnic University, San Luis Obispo, CA

1100 hrs AIAA-2012-4201 Nitrous Oxide Cooled, Reusable Hybrid Aerospike Rocket Motor: Experimental Results

L. Casalino, D. Pastrone, F. Simeoni, Technical University of Turin, Turin, Italy

1130 hrs AIAA-2012-4202 Design Trade-offs for Hybrid Rocket Motors

Novel Motor Operating Configurations I

Hall Thruster Physics IV

B. Jorns, E. Choueiri, Princeton University, Princeton, NJ

Advanced Concepts III 1100 hrs AIAA-2012-4194 Experimental Characterization of Plasma Heating with Beating Electrostatic Waves

Chaired by: L. BRIEDA, Particle In Cell Consulting LLC and D. HERMAN 0930 hrs 1000 hrs 1030 hrs AIAA-2012-4195 AIAA-2012-4196 AIAA-2012-4197 Plume Diagnostics for the Plasma Potential and Comparison of Numerical and Evaluation of the NASA HiVHAc Langmuir Probe Measurements Experimental Time-Resolved EM-R in the Near-field Plume of the Near-Field Hall Thruster W. Huang, H. Kamhawi, R. Shastry, NASA 457Mv2 Hall Thruster Plasma Properties


M. Manente, M. Faenza, F. Ferri, University of Padova, Padova, Italy; A. Selmo, RESIA, Albaredo d’Adige, Italy; K. Katsonis, C. Berenguer, DEDALOS, Thessaloniki, Greece

Chaired by: A. PANCOTTI, MSNW LLC. and T. SWANSON 0930 hrs 1000 hrs AIAA-2012-4191 AIAA-2012-4192 Low Power RF Plasma Thruster Ion Current Distribution of Experimental Characterization ECR Microwave Discharge D. Pavarin, A. Lucca Fabris, F. Trezzolani, Neutralizer


Inman

Cortland

Baker

81

M. Wierman, C. Morgan, W. Anderson, Purdue University, West Lafayette, IN

Combustion Instability II

E. Cavallini, B. Favini, M. Di Giacinto, University of Rome “La Sapienza”, Rome, Italy; F. Serraglia, ESA, Frascati, Italy

Shimizu, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; Y. Yachi, N. Sano, IHI Corporation, Tomioka, Japan

M. Angelone, F. Mascanzoni, C. Milana, Avio S.p.A., Colleferro, Italy

Solid Rocket Motor Development Experiences and History

Three teams will compete for final placing in this 2nd round of design presentations.

AIAA and ASME IGTI Student Design Competition

1100 hrs Oral Presentation (Invited) Perspectives on Affordable Nuclear Thermal Propulsion System Development

S. Bhattacharyya, RENMAR Enterprises, Inc., North Augusta, SC S. Borowski, D. McCurdy, T. Packard, NASA Glenn Research Center, Cleveland, OH

1030 hrs AIAA-2012-4209 Near Earth Asteroid Human Exploration Mission Possibilities Using Nuclear Thermal Rocket (NTR) Propulsion

Nuclear Thermal Propulsion III: Missions, Architectures and Affordability

Exploration Agency (JAXA), Kanagawa, Japan; Y. Daimon, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan

Chaired by: W. FOSTER, Auburn University and M. LANGHENRY, Raytheon Company 0930 hrs 1000 hrs 1030 hrs AIAA-2012-4212 AIAA-2012-4213 AIAA-2012-4211 Analysis of VEGA Solid Stages Solid Propulsion Systems for Technological and Static Firing Tests towards the Epsilon Launch Vehicle Programmatic Development of S. Tokudome, H. Habu, K. Ui, F. Maiden Flight Zefiro 40 Solid Rocket Motor

Wednesday, 1 August 2012 188-SR-9

Chaired by: I. HALLIWELL, Power Systems Manufacturing LLC

Wednesday, 1 August 2012 187-GTE-22 0930 - 1130 hrs

C. Joyner, D. Levack, Pratt & Whitney, Brasuell, Aerojet, Sacramento, CA North Palm Beach, FL; S. Borowski, NASA Glenn Research Center, Cleveland, OH

Chaired by: B. SCHNITZLER and J. WARREN, NASA Headquarters 0930 hrs 1000 hrs AIAA-2012-4207 AIAA-2012-4208 Development of a Small Nuclear Impact and Options for Human Thermal Propulsion Flight Mars Missions Departing from Demonstrator Concept that Is 1000km M. Bulman, V. Collarzo-Perez, D. Scalable to Human Missions

Wednesday, 1 August 2012 186-NFF-7

M. Wierman, C. Fugger, B. Pomeroy, Frederick, University of Alabama, Huntsville, Huntsville, AL W. Anderson, T. Feldman, Purdue University, West Lafayette, IN

Chaired by: W. WANG, The Aerospace Corporation and J. BATTERSON, University of Tennessee Space Institute 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2012-4203 AIAA-2012-4204 AIAA-2012-4205 AIAA-2012-4206 Propellant Throttling Effects on Effect of Step Height on Level Acoustic structure and damping Application of Proper estimation of a cylindrical rocket Orthogonal Decomposition to Self-pulsation of Liquid Rocket of Combustion Instability in a Subscale Transverse Rocket chamber during oscillation Light Intensity Measurements Swirl-coaxial Injection C. Eberhart, D. Lineberry, R. T. Shimizu, D. Hori, Japan Aerospace of Combustion Instability Combustor


Spring

Regency V

Piedmont

Vinnings

82

Organization for Science and Technology, Tehran, Iran

Research Center, Cleveland, OH; J. Dunning, Alphaport Corporation, Cleveland, OH; A. Birchenough, Arctic Slope Research Corporation, Cleveland, OH

The Latest Advances in Radioisotope Power Systems - A Mission Perspective

Spacecraft Power Electronics Design and Performance

Dunwoody

Greenbriar

Techwood

This is an exciting time for radioisotope power systems (RPS). The last General Purpose Heat Source Radioisotope Thermoelectric Generator (GPHS-RTG) produced is on its way to Pluto and beyond on the New Horizons mission. The first Multi-Mission Radioisotope Thermoelectric Generator (MMRTG) is about to land on Mars powering the Mars Science Laboratory (MSL) rover Curiosity. And the Advanced Stirling Radioisotope Generator (ASRG) is being developed for possible use on future missions. Panelists will provide a mission perspective on what radioisotope power systems have meant to space exploration, how the capabilities of GPHS-RTG, MMRTG and ASRG are/will be used by missions, and undoubtedly will cover other aspects of RPS-related technologies, opportunities, and constraints. Panelists: Ralph L. McNutt, Jr. David Woerner Leonard A. Dudzinski Science and Analysis Branch, Chief Scientist for Space Science Nuclear Space Power Office Program Executive Applied Physics Laboratory, Johns Hopkins Laboratory Jet Propulsion Laboratory, California Institute of Technology NASA Headquarters

Chaired by: E. LEWANDOWSKI, NASA Glenn Research Center

Wednesday, 1 August 2012 191-IECEC-11 0930 - 1130 hrs

M. Gollor, B. Fallis, ESA, Noordwijk, The Netherlands

Chaired by: G. CARR, Jet Propulsion Laboratory, California Institute of Technology and A. SALIM 0930 hrs 1000 hrs 1030 hrs AIAA-2012-4219 AIAA-2012-4220 AIAA-2012-4221 Grounding Aspects of Optimum Switching Frequency NEXT Ion Thruster Power Power Processing Units for of a DC-DC Converter in Space Processing Unit (PPU) Capacitor Electric Propulsion Onboard Applications Failure Root Cause Analysis M. Taherbaneh, Iranian Research J. Soeder, L. Pinero, NASA Glenn Spacecrafts

Wednesday, 1 August 2012 190-APS-5

Auburn University, Auburn, AL

1100 hrs AIAA-2012-4318 Coupled CFD Analysis of Thermochemical Erosion and Unsteady Heat Conduction in Solid Rocket Nozzles

Solid Rocket Motor Design and Optimization

D. Bianchi, A. Turchi, F. Nasuti, M. Onofri, University of Rome “La M. Brandyberry, F. Najjar, T. Jackson, Sapienza”, Rome, Italy W. Dick, B. Wasistho, D. Schwenk, M. Campbell, IllinoisRocstar, LLC, Champaign, IL

Chaired by: Y. CHEN, National Space Organization Taiwan and A. GERARDS, US Army AMRDEC 0930 hrs 1000 hrs 1030 hrs AIAA-2012-4214 AIAA-2012-4215 AIAA-2012-4216 Rocstar Simulation Suite: An Evolving Swarm-A Genetically SRM Simulation Using the Level Set Method and Higher Advanced 3-D Multiphysics, Modified Particle Swarm Order Integration Schemes Multiscale Computational Optimizer with Localized Pattern Search Capability for K. Albarado, A. Shelton, R. Hartfield, Framework for Tightly Coupled, Fluid-StructureAerospace Propulsion Systems Auburn University, Auburn, AL R. Hartfield, K. Albarado, R. Jenkins, Thermal Applications


83

IN

Cairo, Egypt; A. Alsayed, Zagazig University, Zagazig, Egypt; M. Fouad, E. Khalil, Cairo University, Cairo, Egypt

M. Aziz, E. Khalil, Cairo University, Cairo, Egypt

A. Fahim, Electro-Mechanical University in Cairo, New Cairo, Egypt; Research Institute, Cairo, Egypt A. Abd El-Rahman, Cairo University, Cairo, Egypt; E. Abdel-Rahman, American University in Cairo, New Cairo, Egypt

1430 hrs AIAA-2012-4234 Simulation of the Influence of Heated Flows on Internal Light Shafts in Residential Buildings

S. Ali, E. Khalil, Cairo University, Cairo, Egypt

1500 hrs AIAA-2012-4235 Numerical Investigation of Impulse Ventilation for Smoke Control in an Underground Car Park

Modeling, Simulation and Analysis of Thermal Systems

Chaired by: E. KHALIL, Cairo University and J. DARKWA, University of Nottingham-Ningbo 1330 hrs 1400 hrs 1300 hrs AIAA-2012-4231 AIAA-2012-4232 AIAA-2012-4233 On the Calculations of Numerical Investigations of Computational Fluid Flow Patterns and Thermal Dynamics Simulation of a Flat Plate Film Cooling Effectiveness Conditions in Large Scale High Thermoacoustic Refrigerator E. Abdelghany, Aviation Institute, Compute Density Data Centers A. Abd El-Rahman, American

P. Panda, V. Kumar, H. Mongia, S. Naik, Purdue University, West Lafayette, IN


V. Kumar, P. Panda, H. Mongia, S. Naik, Agresta, A. Ingenito, University of Rome “La Sapienza”, Rome, Italy Purdue University, West Lafayette, IN

1430 hrs AIAA-2012-4230 Innovative Approaches for Reducing CO2 Emissions of Aviation Engines Part 4: Turbine Exhaust Driven Thermal Secondary Cycle TED-T

Gas Turbine Engines and Related Technologies

Air Mobility History and Flight Testing at Lockheed Martin Wayne Roberts LM Fellow, Chief Test Pilot for Airlift Programs

JPC Awards Luncheon

Nozzles and Thrust Reversers

Chaired by: N. LOVE, University of Texas, El Paso and D. LILLEY, Oklahoma State University 1300 hrs 1330 hrs 1400 hrs AIAA-2012-4227 AIAA-2012-4228 AIAA-2012-4229 Hydrogen Combustors in Gas Innovative Approaches for Numeric Simulation of a Gas Turbines Reducing CO2 Emissions of Turbine Engine with Constant A. Karakurt, B. Khandelwal, V. Aviation Engines Part 2: NPSS Volume Combustion Sethi, R. Singh, Cranfield University, Calibration with Existing Gas R. Andriani, Technical University of Cranfield, United Kingdom Milan, Milan, Italy; F. Gamma, A. Turbine Engines

Wednesday, 1 August 2012 194-TFES-6


A. Sventitskiy, C. Mundt, University of the German Federal Armed Forces, Neubiberg, Germany

Chaired by: C. CHUCK, The Boeing Company and R. DAEBELLIEHN, Aerojet 0930 hrs 1000 hrs 1030 hrs AIAA-2012-4222 AIAA-2012-4223 AIAA-2012-4224 A Multidisciplinary Approach Application of the Narrow-band CFD Validation Study for to Mixer-Ejector Analysis and Correlated k-Distribution Method Internal Performance of to Numerical Simulation of the Advanced SERN Configurations Design E. Hendricks, J. Seidel, NASA Glenn IR Emission from Non-Scattering A. Baucco, K. Shanley, D. Bevis, Rolls-Royce Group plc, Indianapolis, Research Center, Cleveland, OH Exhaust Plumes

Wednesday, 1 August 2012 192-ABPSI-12

A. Fahim, Electro-Mechanical Research Institute, Cairo, Egypt

1530 hrs AIAA-2012-4236 Physical Modeling of ConcreteCore-Radiant Cooling System in Upper Egypt

Lenox

Greenbriar


Pellicone, K. Walker, Advanced V. Kumaresan, Anna University, Cooling Technologies, Inc., Lancaster, Chennai, India; P. Chandrasekaran, SRM PA University, Chennai, India; R. Velraj, Anna University, Chennai, India; M. Nanda, A. Maini, Laser Science and Technology Centre, Delhi, India

1630 hrs AIAA-2012-4237 Role of PCM Based Nanofluids for Energy Efficient Thermal W. Anderson, M. Ellis, J. Hartenstine, Storage in Electronic Cooling R. Hay, K. Lu, J. Montgomery, D. System

1600 hrs Oral Presentation (Invited) Two Phase Thermal Control for Aircraft Applications

Hanover C

84

J. Ausserer, F. Harmon, Air Force Research Laboratory, WrightPatterson AFB, OH

A. Pendharkar, R. McGowan, K. Morillas, M. Pinder, N. Komerath, Georgia Institute of Technology, Atlanta, GA

Astronautics, Nanjing, China

L. Zhang, K. Zhang, Nanjing University of Aeronautics and Astronautics, Nanjing, China

E. Lewandowski, NASA Glenn Research Center, Cleveland, OH

1500 hrs AIAA-2012-4253 Testing of the Advanced Stirling Radioisotope Generator Engineering Unit at NASA Glenn Research Center

High Speed Integrated Inlets

Z. Williams, S. Oriti, E. W. Wong, NASA Glenn Research Center, J. Collins, W. Wong, K. Wilson, M. Lewandowski, NASA Glenn Research Cleveland, OH; K. Wilson, E. Smith, J. Dunlap, E. Smith, Sunpower, Inc., Center, Cleveland, OH Collins, Sunpower, Inc., Athens, OH Athens, OH

1430 hrs AIAA-2012-4252 Sunpower’s Dynamic Conversion to Flight with the Advanced Stirling Convertor (ASC-F)

Chaired by: M. MCMILLAN, Syngenics Corporation and I. HALLIWELL, Power Systems Manufacturing LLC 1430 hrs 1400 hrs AIAA-2012-4065 AIAA-2012-4064 Inverse Design of Supersonic Numerical Investigation of Internal Flow Path Based on Hypersonic Curved Shock TwoGiven Outflow Velocity Profile Dimensional Inlet Designed X. Fang, K. Zhang, Nanjing on the Wall Constant Mach University of Aeronautics and Number Gradient

Wednesday, 1 August 2012 139-ABPSI-9/HSABP/ HYP-7

D. Meer, Sest, Inc., Middleburg Heights, OH; S. Oriti, NASA Glenn Research Center, Cleveland, OH

1500 hrs AIAA-2012-4247 Analysis of Electricity Consumption in the Faculty of Engineering with Integration of Renewable Solar Power System

Stirling System Development

1430 hrs AIAA-2012-4246 CALERA CO2 Sequestration and Enhanced Geothermal Energy

F. Wyczalek, Energy Independence Foundation, Bloomfield Hills, MI; M. A. Abdel Gawad, Zagazig University, Wyczalek, General Motors Corporation, E. Ogedengbe, ENERGHX, Ottawa, Warren, MI; T. Wyczalek, Magna Zagazig, Egypt Canada; E. Ogedengbe, University of Exteriors and Interiors, Novi, MI Lagos, Lagos, Nigeria

1400 hrs AIAA-2012-4245 Novel Electro-Mechanical Mechanism for Blade PitchControl of Horizontal-Axis, Home-scale Wind Turbines

1500 hrs AIAA-2012-4242 Neural Modeling and Predictive Control of a Small Turbojet Engine (SR-30)

Renewable Energy Generation Technologies

1430 hrs AIAA-2012-4241 Design of Hybrid Electric Propulsion System for Long Endurance Small UAV

Power Technologies and Management for Aircraft and UAV

B. Loop, E. Walters, PC Krause Y. Li, L. Liu, X. Ma, H. Tu, Beijing A. Aly, I. Atia, Military Technical and Associates, West Lafayette, Institute of Technology, Beijing, China College (MTC), Cairo, Egypt IN; P. Lamm, Air Force Research Laboratory, Wright-Patterson AFB, OH

1400 hrs AIAA-2012-4240 Optimal System Partitioning for Distributed Heterogeneous Simulations

Chaired by: T. CHAN, Lockheed Martin Corporation and D. HILL, Lockheed Martin Corporation 1330 hrs 1400 hrs 1300 hrs AIAA-2012-4250 AIAA-2012-4251 AIAA-2012-4249 Advanced Stirling Convertor Pathfinding the Flight Advanced Advanced Stirling Convertor Durability Testing: Plans and (ASC-E2) Characterization Stirling Convertor Design with Interim Results Testing the ASC-E3

Wednesday, 1 August 2012 198-EC-6

M. Simpson, A. Glezer, Georgia Institute of Technology, Atlanta, GA

Chaired by: M. SIMPSON and F. WYCZALEK, FW Lilly, Inc. 1300 hrs 1330 hrs AIAA-2012-4243 AIAA-2012-4244 Electric Power Generation Optimization of a Vertical Axis Using Buoyancy-Induced Micro Wind Turbine for Low Tip Vortices Speed Ratio Operation

Wednesday, 1 August 2012 197-EERE-6

Exploration Agency (JAXA), Tokyo, Japan; H. Nomura, Nihon University, Narashino, Japan; T. Tagashira, R. Yanagi, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan

Chaired by: M. LIFFRING, Boeing Commercial Airplanes and J. FU 1300 hrs 1330 hrs AIAA-2012-4238 AIAA-2012-4239 Performance Analysis of a Fuel Integration, Validation, and Cell Hybrid Aviation Propulsion Testing of a Hybrid-Electric Propulsion System for a Small System K. Okai, H. Fujiwara, Japan Aerospace Remotely Piloted Aircraft

Wednesday, 1 August 2012 196-APS-6

S. Oriti, P. Schmitz, E. Lewandowski, NASA Glenn Research Center, Cleveland, OH

1530 hrs AIAA-2012-4254 Test Hardware Design for FlightLike Operation of Advanced Stirling Convertors (ASC-E3)

H. Khalil, Cairo University, Cairo, Egypt

1530 hrs AIAA-2012-4248 Sustainable Urbanism: Theories and Green Rating Systems

Hanover C

Fairlie

Kennesaw

Dunwoody

85

K. Ajmani, ASRC Aerospace Corporation, Cleveland, OH

Institute of Technology, Atlanta, GA F. Florean, A. Petcu, I. Porumbel, C. Carlanescu, C. Sandu, COMOTI National Research & Development Institute for Gas Turbines, Bucharest, Romania; G. Dumitrascu, “Gheorghe Asachi” Technical University, Iasi, Romania

T. Drozda, NASA Langley Research Center, Hampton, VA

1600 hrs AIAA-2012-4264 Progress toward affordable high fidelity combustion simulations using filtered density functions for hypersonic flows in complex geometries (Invited)

D. Schmuland, C. Carpenter, Aerojet, Redmond, WA

1600 hrs AIAA-2012-4269 Mission Applications of the MRS-142 CubeSat High-Impulse Adaptable Monopropellant Propulsion System (CHAMPS)

Combustor Emissions

1530 hrs AIAA-2012-4268 Design and Selection Process for Optimized Heavy Lift Launch Vehicles

Advanced Propulsion Concepts V

B. Khandelwal, A. Karakurt, A. Prakash, V. Sethi, Cranfield P. Ritter, J. Lyne, University of University, Cranfield, United Kingdom Tennessee, Knoxville, Knoxville, TN

1500 hrs AIAA-2012-4267 A Review of Hydrogen as a Fuel for Future Air Transport

J. Edwards, Self, Raleigh, NC

Chaired by: J. CONVERY, GE Aviation and D. BLUNCK, Air Force Reseach Laboratory 1430 hrs 1500 hrs 1400 hrs AIAA-2012-4271 AIAA-2012-4273 AIAA-2012-4270 Experimental Measurements Emissions Prediction for Computational Modeling of Discrete-Jet Lean-Direct in Reactive and Non-Reactive Aircraft Conceptual Design R. Denney, J. Tai, D. Mavris, Georgia Injectors Turbulent Flows


B. Khandelwal, A. Karakurt, V. Sethi, R. Singh, Cranfield University, Cranfield, United Kingdom

Chaired by: T. CHEN and J. ROBINSON 1400 hrs 1430 hrs AIAA-2012-4265 AIAA-2012-4266 Study of Novel Micromix Viscous losses of MNG in Combustors to be used in Gas Hybrid Motor Tests D. Chasman, S. Haight, R. Loehr, Turbines; using Hydrogen, Hydrogen-Methane, Methane Raytheon Company, Tucson, AZ and Kerosene as a fuel

Wednesday, 1 August 2012 201-APC-5

University of Minnesota, Minneapolis, Minneapolis, MN; P. Givi, University of Pittsburgh, Pittsburgh, PA

J. White, NASA Langley Research Center, Hampton, VA

1530 hrs AIAA-2012-4263 Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion Systems

F. Jaberi, Michigan State University, East Lansing, MI

1630 hrs Oral Presentation (Invited) Large Eddy Simulation of High Speed Turbulent Combustion (Invited)

Numerical Modeling of Turbulent Combustion in Hypersonic Flows (Invited)

Chaired by: D. MUSIELAK, University of Texas, Arlington and J. WHITE, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2012-4260 AIAA-2012-4261 AIAA-2012-4262 Large eddy simulation of the Large Eddy/ReynoldsSFMDF in US3D for LES HyShot II scramjet combustor Averaged Navier-Stokes of Compressible Flows on using a supersonic flamelet Simulations of Scramjet Unstructured Meshes C. Otis, University of Pittsburgh, model (Invited) Combustor Flow Fields Pittsburgh, PA; P. Ferrero, G. Candler, J. Larsson, Self, Stanford, CA (Invited)

Wednesday, 1 August 2012 200-HSABP/HYP-10

Hanover F

Hanover A

Regency VII

86

M. Lau, S. Manna, G. Herdrich, University of Stuttgart, Stuttgart, Germany; T. Schönherr, K. Komurasaki, University of Tokyo, Kashiwa, Japan

A. Mingo Perez, University of Southampton, Southampton, United Kingdom; M. Coletti, Mars Space, Ltd., Southampton, United Kingdom; S. Gabriel, University of Southampton, Southampton, United Kingdom

S. Wang, Z. Wu, X. Liu, L. Yang, F. Wang, Y. Cheng, N. Wang, Beijing Institute of Technology,, Beijing, China

D. Codron, D. Erwin, K. Goodfellow, University of Southern California, Los Angeles, CA

1500 hrs AIAA-2012-4277 Results of Experimental Studies on Thorium Migration in Electric Thrusters

R. Webster, K. Sreenivas, D. Hyams, B. Hilbert, W. Briley, D. Whitfield, University of Tennessee, Chattanooga, Chattanooga, TN

A. Ferrar, W. O’Brien, Virginia Polytechnic Institute and State University, Blacksburg, VA

Chaired by: G. WELCH, NASA Glenn Research Center 1430 hrs 1400 hrs AIAA-2012-4283 AIAA-2012-4282 Demonstration of Sub-system Progress in Boundary Layer Level Simulations: A Coupled Ingesting Embedded Engine Inlet and Turbofan Stage Research


H. Koizumi, Y. Arakawa, University of Tokyo, Bunkyo, Japan; K. Komurasaki, University of Tokyo, Kashiwa, Japan

R. Baltz, N. Galyen, Aerospace Testing Alliance, Arnold AFB, TN; T. Moeller, University of Tennessee Space Institute, Tullahoma, TN; M. May, Arnold Engineering Development Center, Arnold AFB, TN

1500 hrs AIAA-2012-4284 AEDC/UTSI J85 Turbojet Test Stands

Chaired by: J. ZIEMER, Jet Propulsion Laboratory, California Institute of Technology 1400 hrs 1430 hrs 1500 hrs AIAA-2012-4278 AIAA-2012-4279 AIAA-2012-4280 Influence of Propellant in the A micro PPT for Nano-satellite Numerical Simulation of Discharge Process of PPT applications: Design and a Water Propellant Pulsed T. Schönherr, Y. Abe, K. Okamura, experimental results Plasma Thruster


University, College Station, TX; J. Shebalin, NASA Johnson Space Center, Houston, TX; D. Staack, Texas A&M University, College Station, TX; B. Longmier, University of Michigan, Ann Arbor, MI; C. Olsen, Ad Astra Rocket Company, Webster, TX

Chaired by: B. LONGMIER, University of Wisconsin, Madison 1400 hrs 1430 hrs AIAA-2012-4274 AIAA-2012-4275 Experimental Investigation Magnetic Nozzle Plasma of the Current Density in the Plume: Review of Crucial Discharge Plasma of ADD Physical Phenomena F. Ebersohn, S. Girimaji, Texas A&M SIMP-LEX


C. Ruscher, J. Dannenhoffer, M. Glauser, Syracuse University, Syracuse, NY; B. Kiel, B. Sekar, Air Force Research Laboratory, WrightPatterson AFB, OH

1530 hrs AIAA-2012-4285 Vortex Shedding of Various Bluff Bodies in Cross Flow

Engine Compatibility, Testing, and CFD

H. Kobayashi, H. Horisawa, Tokai University, Hiratsuka, Japan; I. Funaki, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan

Pulsed Plasma Thrusters

1530 hrs AIAA-2012-4281 A high-peak-power laser assisted pulsed plasma thruster

Electromagnetic Propulsion IV

Hanover G

Regency VI

Regency V

87

Institute of Technology, Atlanta, GA

D. Anderson, E. Pencil, NASA Glenn Research Center, Cleveland, OH; J. Dankanich, Gray Research, Inc., Cleveland, OH; D. Vento, NASA Glenn Research Center, Cleveland, OH; M. Munk, L. Glaab, NASA Langley Research Center, Hampton, VA; T. Peterson, NASA Glenn Research Center, Cleveland, OH

Tokyo, Japan; S. Nonaka, Y. Naruo, Y. Inatani, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; K. Kinefuchi, K. Okita, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan

M. Biolo, Asco Pompe, Milan, Italy; A. Bettella, HIT09, Padova, Italy; R. Da Forno, MDA, Belluno, Italy; D. Pavarin, University of Padova, Padova, Italy

I. Funaki, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; H. Nishida, Tokyo University of Agriculture and Technology, Koganei, Japan; Y. Oshio, Graduate University for Advanced Studies, Sagamihara, Japan; N. Yamamoto, Y. Yamagiwa, Shizuoka University, Hamamatsu, Japan

Y. Yamagiwa, A. Takagi, N. Yoshimura, Shizuoka University, Hamamatsu, Japan; K. Tanaka, T. Abe, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; H. Sahara, Tokyo Metropolitan University, Hino, Japan; H. Fujii, Kanagawa Institute of Technology, Atsugi, Japan

Chaired by: J. CHENOWETH, CRAFT Tech 1430 hrs 1400 hrs AIAA-2012-4303 AIAA-2012-4300 Progress in Current Collection Experiment Magnetohydrodynamic of Bare Electrodynamic Tape and Particle Simulations of Tether by Using Sounding Magnetoplasma Sail Rocket


Huntsville, AL

K. Hagiwara, H. Horisawa, K. Fukuda, Tokai University, Hiratsuka, Japan

Laser ablation thrusters for atmospheric flight applications

AIAA-2012-4302

1500 hrs

M. Gauer, M. Lambert, K. Hannemann, German Aerospace Center (DLR), Göttingen, Germany

Innovative Propulsion Systems

S. Chintalapati, D. Kirk, Florida Institute of Technology, Melbourne, FL

1600 hrs AIAA-2012-4298 Two-phase flow modeling combining the CICSAM with the projection method

Tanks - Sloshing

Engineering and Analysis for Propulsion Systems II

Chaired by: V. AHUJA, Combustion Research & Flow Technology, Inc. and A. LOPEZ, The Boeing Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2012-4294 AIAA-2012-4295 AIAA-2012-4296 AIAA-2012-4297 Prediction of Liquid Slosh Investigation on Pressure Change EUCLID Mission: Theoretical Design of an Experiment Damping Using a High Induced by Cryogenic Sloshing Sloshing Model and CFD Platform for Acquisition of T. Himeno, Y. Umemura, C. Inoue, Comparison Resolution CFD Tool Liquid Slosh Data aboard the H. Yang, CFD Research Corporation, T. Watanabe, University of Tokyo, M. Lazzarin, HIT09, Padova, Italy; International Space Station


G. Boudier, French Space Agency (CNES), Toulouse, France

Chaired by: C. GATTO, Jet Propulsion Laboratory, California Institute of Technology 1400 hrs 1430 hrs 1500 hrs AIAA-2012-4286 AIAA-2012-4287 AIAA-2012-4288 Brayton Cycle Conversion for NASA in-Space Propulsion Propulsion Analysis of Technologies and Their Demeter Microsatellite Fluidic Space Solar Power B. Dessanti, N. Komerath, Georgia Infusion Potential Passivation


H. Hernandez, NASA Johnson Space Center, Houston, TX

1630 hrs AIAA-2012-4299 Design, Test, and Slosh Analysis of Baffled Spherical Tanks for Slosh Control on a Liquid Oxygen-Methane Lander Test Vehicle

Hanover E

Vinnings

Hanover D

88

Novel Motor Operating Configurations II

Piedmont

Center, Huntsville, AL; S. Borowski, NASA Glenn Research Center, Cleveland, OH; J. George, NASA Johnson Space Center, Houston, TX; T. Kim, W. Emrich, R. Hickman, J. Broadway, H. Gerrish, R. Adams, NASA Marshall Space Flight Center, Huntsville, AL

Technology, São José dos Campos, L. Simurda, A. Boiron, K. Hornstein, Brazil; L. Rocco, Flowtest Aerospace K. Stober, Stanford University, Research, São Paulo, Brazil; J. Rocco, K. Stanford, CA Iha, Aeronautical Institute of Technology, São José dos Campos, Brazil

R. Vesterås, G. Raudsandmoen, Nammo Raufoss, Raufoss, Norway

Chaired by: J. MAJDALANI, University of Tennessee Space Institute and D. MYRE, U.S. Naval Academy 1430 hrs 1500 hrs 1400 hrs AIAA-2012-4309 AIAA-2012-4310 AIAA-2012-4311 Evaluation of polyurethane Design and Development of Nammo hybrid rocket propulsion TRL improvement binder additivated with paraffin a Thrust Vector Controlled and tested with a swirl injector Paraffin/Nytrox Hybrid program S. Gomes, Aeronautical Institute of J. Ronningen, J. Husdal, M. Berger, Rocket


W. Emrich, NASA Marshall Space Flight Center, Huntsville, AL

M. Brooks, J. Pitot, B. Genevieve, S. Chowdhury, L. Roberts, University of KwaZulu-Natal, Durban, South Africa

1530 hrs AIAA-2012-4312 The Phoenix Hybrid Sounding Rocket Program: A Progress Report 2012

Paraffin Fuels II

Nuclear Thermal Propulsion IV: Testing and Programmatics

Chaired by: S. BHATTACHARYYA, RENMAR Enterprises, Inc. and T. HARRISON, Oak Ridge National Laboratory 1400 hrs 1430 hrs AIAA-2012-4307 AIAA-2012-4308 Nuclear Thermal Rocket Affordable Development of a Element Environmental Nuclear Cryogenic Propulsion Simulator (NTREES) Upgrade Stage M. Houts, NASA Marshall Space Flight Activities

Wednesday, 1 August 2012 213-NFF-8

Inman

University

Wednesday, 1 August 2012 212-JPC-13 NSTC Aeronautics S&T Subcommittee Public Outreach Centennial Ballroom I 1400 - 1700 hrs The National Science and Technology Council’s (NSTC) Aeronautics Science and Technology Subcommittee will unveil and discuss the results of its recent assessment of progress under the National Aeronautics Research and Development Plan. In addition, the subcommittee will engage public stakeholders on key issues in aeronautics research and development and future subcommittee activities.

N. Bellomo, F. Barato, M. Faenza, Utah State University, Logan, UT A. Bettella, D. Pavarin, University of Padova, Padova, Italy

Chaired by: J. STEVENS, Space Propulsion Group, Inc. and B. EVANS, Space Propulsion Group, Inc. 1400 hrs 1430 hrs AIAA-2012-4304 AIAA-2012-4305 The “Vortex Reloaded” project: Catalytic Decomposition of Nitrous Oxide Monopropellant experimental investigation on fully tangential vortex injection in for Hybrid Motor Re-Ignition M. Wilson, S. Eilers, S. Whitmore, N2O - paraffin hybrid motors


89

University, West Lafayette, IN

P. O’Neil, S. Heister, Purdue University, West Lafayette, IN

A. Yilmaz, Istanbul Kultur University, I. Kronhaus, A. Kapulkin, V. Istanbul, Turkey Balabanov, M. Rubanovich, M. Guelman, B. Natan, Technion--Israel Institute of Technology, Haifa, Israel

1500 hrs AIAA-2012-4315 Characterization of CAMILA Hall Thruster Discharge using Electrical Probe Measurements

M. Fiebig, C. Zakrzwski, NASA Goddard Space Flight Center, Greenbelt, MD

Goddard Space Flight Center, Greenbelt, MD

J. Dennis, T. Pourpoint, S. Son, Purdue University, West Lafayette, IN Command & Technology, Beijing, China

Flight Center, Greenbelt, MD

1600 hrs AIAA-2012-4333 Flight Performance of the MESSENGER Propulsion System from Launch to Orbit Insertion

1630 hrs AIAA-2012-4334 Development and Testing Status of the Vinci Thrust Chamber

S. Bushman, Johns Hopkins M. Wilson, C. Engelbrecht, Johns D. Haeseler, F. Haidinger, L. University Applied Physics Laboratory, Hopkins University Applied Physics Brummer, J. Haeberle, Astrium, Laurel, MD Laboratory, Laurel, MD; M. Trela, Munich, Germany Skybox Imaging, Mountain View, CA

1530 hrs AIAA-2012-4332 Design, Fabrication, and Testing of the Radiation Belt Storm Probes Propulsion Systems

In-Space and Upper Stage Propulsion Systems

C. Brown, U. Mondragon, V. McDonell, Energy Research Consultants, Laguna Hills, CA; B. Kiel, Air Force Research Laboratory, Wright-Patterson AFB, OH

X. Chen, V. Yang, Georgia Institute of Technology, Atlanta, GA

1600 hrs AIAA-2012-4328 A Thickness-based Refinement Method for Multi-scale Twophase Flow Simulation

Spray Combustion II

Z. Ya, Beijing High Technology Research Institute, Beijing, China

1530 hrs AIAA-2012-4323 Research on NEPE Solid Rocket Motor Grain Storage Damage

Solid Rocket Motor Propellant Development

W. Hargus, J. Lubkeman, K. Remy, A. Gonzales, Air Force Research Laboratory, Edwards AFB, CA

1530 hrs AIAA-2012-4316 Investigation of Singly Ionized Iodine Spectroscopy in Support of Electrostatic Propulsion Diagnostics Development

Hall Thruster Physics V

1530 hrs AIAA-2012-4327 Comparison of CFD Predictions and Experimental Measurements of Liquid S. Feng, H. Bo, H. He, L. Su, Z. Jet Injection into a Vitiated Hou, W. Nie, Academy of Equipment Crossflow

1500 hrs AIAA-2012-4326 Experimental Investigation of Atomization and Combustion of Organic Gel Propellant

Chaired by: S. MILLER, Aerojet and A. FRANKEL, AMPAC In-Space Propulsion 1430 hrs 1500 hrs 1400 hrs AIAA-2012-4330 AIAA-2012-4331 AIAA-2012-4329 The SDO Propulsion Subsystem LRO Propulsion System Design LRO Propulsion System Testing W. Willis, NASA Goddard Space M. Fiebig, C. Zakrzwski, NASA & On-Orbit Operations


Pourquie, J. van Buijtenen, Delft University of Technology, Delft, The Netherlands

Chaired by: M. ANAND, Rolls-Royce Corporation 1400 hrs 1430 hrs AIAA-2012-4324 AIAA-2012-4325 Simulation of Reacting Spray Critical Ignition Criteria for in a Multi-Point Lean Direct Monomethylhydrazine and Injection Combustor Red Fuming Nitric Acid in an D. Dewanji, A. Gangoli Rao, M. Impinging Jet Apparatus

Wednesday, 1 August 2012 218-PC-15

P. O’Neil, S. Heister, Purdue University, West Lafayette, IN

Chaired by: J. HANSEN, United Launch Alliance and W. RYAN, United Launch Alliance 1400 hrs 1430 hrs 1500 hrs AIAA-2012-4319 AIAA-2012-4320 AIAA-2012-4321 Investigation of the Evaluation of Ballistic and Experimental Evaluation Effect of Gelling Agents Mechanical Properties of Processing and Aging on Dicyclopentadiene’s of PolymerizedCharacteristics of Polymerized Rheological Characteristics for Dicyclopentadiene-Based Dicyclopentadiene for Use as Improvement of Composite Composite Solid Propellants a Composite Solid Propellant P. O’Neil, S. Heister, Purdue Solid Propellant Quality Binder


K. Hara, I. Boyd, University of Michigan, Ann Arbor, Ann Arbor, MI; V. Kolobov, CFD Research Corporation, Huntsville, AL

Chaired by: C. KOPPEL, KopooS Consulting Ind and R. SHASTRY 1400 hrs 1430 hrs AIAA-2012-4313 AIAA-2012-4314 One Dimensional HybridModeling the Effects of Discharge Voltage on Hall Vlasov Simulation of a Hall Thruster Performance Thruster


Roswell

Hanover B

Techwood

Cortland

90

Abd El-Rahman, A., 195-TM-8 Abd Elhafez, A., 149-EERE-5 Abdel Gawad, A., 197-EERE-6 Abdel-Rahman, E., 195-TM-8 Abdelghanny, M., 149-EERE-5 Abdelghany, E., 108-TM-3, 195-TM-8 Abdellatif, O., 67-EERE-3, 149-EERE-5 Abdraboo, M., 149-EERE-5 Abdul-Rahman, H., 35-TFES-2 Abe, T., 210-SCP-5 Abe, Y., 205-EP-32 Abernathy, S., 74-EDU-1 Abiad, M., 42-EERE-2 Abou Dief, T., 149-EERE-5 Achawangkul, Y., 135-EERE-4 Adams, R., 154-NFF-6, 213-NFF-8 Adelhelm, R., 6-EC-1 Adis, W., 142-SCP-2 Agrawal, A., 8-TFES-1, 35-TFES-2 Agresta, A., 135-EERE-4, 194-TFES-6 Ahedo, E., 58-EP-7, 97-EP-14, 155-EP-24, 179-EP-26 Ahmed, I., 9-EERE-1 Ahuja, V., 107-LP-13, 209-LP-25 Aintablian, H., 106-EC-4 Ajmani, K., 202-GTE-24 Akbari, P., 4-HSABP/HYP-1/PC-1 Al Shoaibi, A., 8-TFES-1 Albarado, K., 189-SR-10 Alexander, J., 117-SCP-1 Ali, A., 34-APC-2 Ali, S., 195-TM-8 Alliot, P., 27-LP-3, 55-LP-6, 70-LP-9, 160-LP-22 Allred, J., 3-ABPSI-1/GTE-1 Alsayed, A., 108-TM-3, 195-TM-8 Althausen, D., 130-GTE-15 Álvarez, F., 147-PC-12 Aly, A., 196-APS-6 Ambekar, A., 147-PC-12 Anand, M., 26-PC-3, 47-PC-5, 218-PC-15 Anderson, B., 168-GEPC-1/GTE-19 Anderson, D., 207-SCP-4 Anderson, J., 124-EP-19 Anderson, P., 24-IECEC-2 Anderson, W., 74-EDU-1, 77-TM-2, 146-LP-19, 185-LP-24, 195-TM-8 Andriani, R., 135-EERE-4, 162-GTE-17, 194-TFES-6 Anflo, K., 48-LP-5 Angelone, M., 188-SR-9 Annovazzi, A., 104-SR-6 Ansart, R., 125-LP-16

Aoyagi, J., 21-LP-2 Arakawa, Y., 26-PC-3, 34-APC-2, 95-EP-13, 179-EP-26, 205-EP-32 Araki, S., 95-EP-13 Arastu, A., 53-APS-1, 105-APS-3 Ardha, V., 8-TFES-1, 35-TFES-2 Arend, D., 110-GTE-12/ABPSI-6, 130-GTE-15 Arias Quintero, S., 101-PC-9 Arnault, A., 34-APC-2 Arnold, R., 90-LP-11 Ashjaee, M., 43-LP-4 Aso, S., 80-HR-3 Ataman, C., 124-EP-19 Atia, I., 196-APS-6 Ausserer, J., 196-APS-6 Austin, B., 133-LP-18 Axdahl, E., 88-HSABP/HYP-4 Ayad, S., 149-EERE-5 Azarnia, G., 69-EP-10 Aziz, M., 195-TM-8 Babou, Y., 92-GTE-11 Baird, B., 33-PC-4 Baisden, A., 53-APS-1, 78-APS-2, 137-APS-4 Bakhle, M., 110-GTE-12/ABPSI-6 Balabanov, V., 215-EP-34 Balachandran, P., 175-PC-14 Baldauff, R., 28-TM-1 Ball, P., 10-GTE-2 Ballard, R., 81-LP-10 Baltz, R., 206-GTE-25 Bambach, P., 120-EP-16 Banterng Silpsakoolsook, B., 79-EC-3 Bao, W., 172-TM-6 Barato, F., 19-HR-1, 80-HR-3, 177-SCP-3, 211-HR-9 Barlow, A., 86-ABPSI-5 Barnes, M., 76-ST-2 Basavanahalli, R., 131-SR-7 Basset, P., 45-GTE-5 Bath, A., 100-HR-4 Batterson, J., 185-LP-24 Battista, F., 90-LP-11 Battoneau, Y., 141-APC-3 Baucco, A., 192-ABPSI-12 Bauer, C., 52-SR-4 Beal, B., 69-EP-10 Beattie, M., 154-NFF-6 Beckel, S., 115-HSABP/HYP-5 Bedard, M., 74-EDU-1 Bedsun, D., 17-NFF-1 Behera, R., 72-TNES-1, 136-TNES-2

Author/Session Chair Index Behruzi, P., 132-LP-17 Beiting, E., 15-EP-2 Bellomo, N., 19-HR-1, 80-HR-3, 177-SCP-3, 211-HR-9 Bemont, C., 28-TM-1 Benchergui, D., 57-ABPSI-3 Bennett, R., 138-EC-5 Berend, N., 76-ST-2 Berenguer, C., 182-EP-28 Berens, T., 113-ABPSI-7, 167-HSABP/HYP-9/ABPSI-11 Berger, M., 122-HR-5, 214-HR-8 Berger, Z., 50-GTE-6 Bering, E., 89-EP-11 Bertacin, R., 104-SR-6 Berton, J., 110-GTE-12/ABPSI-6 Besnard, E., 81-LP-10, 109-LP-14, 159-LP-21 Betancourt-Roque, J., 63-LP-7, 65-LP-8 Bettella, A., 19-HR-1, 80-HR-3, 209-LP-25, 211-HR-9 Betti, B., 81-LP-10, 119-LP-15 Bevis, D., 192-ABPSI-12 Beyersdorf, A., 168-GEPC-1/GTE-19 Bhattacharyya, S., 186-NFF-7, 213-NFF-8 Bhatti, K., 6-EC-1 Bially, E., 181-TM-7 Bianchi, D., 44-HR-2, 75-SR-5, 189-SR-10 Bindon, J., 55-LP-6 Biolo, M., 209-LP-25 Birchenough, A., 190-APS-5 Blachowski, T., 41-ECS-2 Blades, E., 102-LP-12 Blakely, J., 69-EP-10 Blanquet, A., 12-EDGR-1 Blodgett, K., 113-ABPSI-7 Blunck, D., 127-GTE-14, 202-GTE-24 Bo, H., 218-PC-15 Boiron, A., 214-HR-8 Boles, J., 115-HSABP/HYP-5 Bollo, T., 170-APC-4 Bonifacio, S., 101-PC-9 Borner, A., 39-EP-5 Borowski, S., 17-NFF-1, 49-NFF-2, 99-NFF-5, 186-NFF-7, 213-NFF-8 Boss, M., 68-EP-9 Boudier, G., 207-SCP-4 Bowsher, A., 117-SCP-1 Boxberger, A., 120-EP-16 Boyd, I., 15-EP-2, 215-EP-34 Brackbill, J., 97-EP-14 Bradley, M., 167-HSABP/HYP-9/ABPSI-11 Bradley, T., 42-EERE-2, 67-EERE-3, 103-IECEC-6, 108-TM-3, 149-EERE-5 Brandyberry, M., 189-SR-10 Brasuell, D., 17-NFF-1, 186-NFF-7 Breeze-Stringfellow, A., 92-GTE-11 Bridges, J., 20-GTE-3 Brieda, L., 64-EP-8, 183-EP-29 Briggs, M., 6-EC-1 Briley, W., 206-GTE-25 Brinkley, A., 21-LP-2 Briones, A., 33-PC-4 Brito, H., 66-NFF-3 Broadway, J., 49-NFF-2, 213-NFF-8 Brooks, M., 28-TM-1, 42-EERE-2, 55-LP-6, 214-HR-8 Brophy, C., 62-PC-7, 94-PC-8 Brophy, J., 123-EP-18, 140-EP-21 Brossman, J., 10-GTE-2 Brown, C., 218-PC-15 Brown, D., 69-EP-10, 93-EP-12, 121-EP-17, 155-EP-24 Brown, G., 3-ABPSI-1/GTE-1 Brown, M., 32-HSABP/HYP-2 Bruckner, R., 162-GTE-17 Brummer, L., 219-LP-26 Bruno, C., 61-PC-6 Bryden, K., 148-TFES-4 Buckle, R., 157-ES-1 Bulit, A., 124-EP-19 Bulman, M., 17-NFF-1, 99-NFF-5, 186-NFF-7 Bulzan, D., 5-PC-2, 168-GEPC-1/GTE-19 Burchett, J., 41-ECS-2 Burguburu, S., 45-GTE-5 Burke, E., 157-ES-1 Bushman, S., 21-LP-2, 48-LP-5, 219-LP-26 Butler, B., 10-GTE-2 Butler, M., 78-APS-2, 137-APS-4 Butt, A., 70-LP-9 Cadou, C., 175-PC-14 Caldas-Pinto, P., 52-SR-4 Cambier, J., 97-EP-14 Campanella, O., 160-LP-22 Campbell, M., 189-SR-10 Candler, G., 200-HSABP/HYP-10 Cannella, M., 122-HR-5 Cantwell, B., 80-HR-3, 100-HR-4, 122-HR-5, 135-EERE-4, 184-HR-7 Capece, V., 10-GTE-2, 171-GTE-20 Cardell, G., 78-APS-2 Cardiff, E., 95-EP-13 Carlanescu, C., 202-GTE-24 Carpenter, C., 201-APC-5 Carr, G., 137-APS-4, 190-APS-5 Carruthers, B., 74-EDU-1

Carter, C., 33-PC-4 Carter, M., 89-EP-11 Casalino, L., 162-GTE-17, 184-HR-7 Casalis, G., 51-SR-3 Cassady, L., 89-EP-11 Cassenti, B., 17-NFF-1 Cassibry, J., 154-NFF-6 Castaldo, J., 78-APS-2 Catalano, F., 57-ABPSI-3 Cavallini, E., 51-SR-3, 75-SR-5, 188-SR-9 Cavender, D., 74-EDU-1 Celestina, M., 130-GTE-15 Chakraborty, S., 124-EP-19 Chambers, R., 53-APS-1 Chan, T., 198-EC-6 Chandler, A., 100-HR-4 Chandrasekaran, P., 195-TM-8 Chang, J., 167-HSABP/HYP-9/ABPSI-11 Chang, X., 88-HSABP/HYP-4 Chang Diaz, F., 89-EP-11 Chapman, J., 17-NFF-1 Charneski, J., 134-TM-4 Chase, R., 170-APC-4 Chasman, D., 201-APC-5 Chehroudi, B., 101-PC-9 Chen, C., 18-LP-1 Chen, G., 68-EP-9, 96-TFES-3, 97-EP-14 Chen, L., 88-HSABP/HYP-4 Chen, T., 34-APC-2, 88-HSABP/HYP-4, 201-APC-5 Chen, X., 218-PC-15 Chen, Y., 19-HR-1, 189-SR-10 Cheng, D., 147-PC-12 Cheng, Y., 205-EP-32 Chenoweth, J., 177-SCP-3, 210-SCP-5 Chianese, S., 125-LP-16 Chicatelli, A., 199-ABPSI-13/GTE-23 Chidambaram, P., 152-HR-6 Chintalapati, S., 107-LP-13, 209-LP-25 Chiu, Y., 69-EP-10, 129-EP-20 Cho, S., 179-EP-26 Choi, H., 61-PC-6 Choi, M., 28-TM-1, 46-IECEC-3, 77-TM-2, 108-TM-3, 143-TM-5, 158-IECEC-9 Choi, Y., 180-EP-27 Chopinet, J., 70-LP-9 Choudhuri, A., 8-TFES-1, 35-TFES-2, 63-LP-7, 65-LP-8, 74-EDU-1, 148-TFES-4, 156-LP-20 Choueiri, E., 58-EP-7, 144-EP-22, 182-EP-28 Chowdhury, A., 147-PC-12 Chowdhury, S., 214-HR-8

91

Chpoun, A., 70-LP-9 Chu, E., 144-EP-22 Chu, J., 3-ABPSI-1/GTE-1, 31-ABPSI-2/GTE-4 Chu, L., 155-EP-24 Chuck, C., 192-ABPSI-12 Ciezki, H., 101-PC-9 Claflin, S., 80-HR-3 Clarke, J., 25-SR-2 Claus, R., 50-GTE-6 Clingan, P., 74-EDU-1 Cliquet, E., 76-ST-2 Codron, D., 203-EP-30 Coil, M., 5-PC-2 Coles, T., 39-EP-5 Coletti, M., 64-EP-8, 144-EP-22, 205-EP-32 Collarzo-Perez, V., 186-NFF-7 Collins, J., 198-EC-6 Connolly, J., 164-HSABP/HYP-8/ABPSI-10, 199-ABPSI-13/GTE-23 Convery, J., 163-GTE-18, 202-GTE-24 Cooper, C., 17-NFF-1 Coote, D., 63-LP-7, 90-LP-11 Corbett, M., 162-GTE-17 Corey, R., 155-EP-24 Cornell, P., 138-EC-5 Corporan, E., 168-GEPC-1/GTE-19 Corrigan, A., 94-PC-8 Cortez, R., 154-NFF-6 Cote, T., 108-TM-3 Crane, C., 41-ECS-2 Cross, E., 117-SCP-1 Cross, R., 117-SCP-1 Crudgington, P., 117-SCP-1 Csank, J., 167-HSABP/HYP-9/ABPSI-11 Culbertson, J., 159-LP-21 Culley, D., 114-ABPSI-8/GTE-13, 199-ABPSI-13/GTE-23 Cummings, D., 31-ABPSI-2/GTE-4 Curtiss, T., 15-EP-2 Cuvelier, M., 136-TNES-2 Da Forno, R., 209-LP-25 Daebelliehn, R., 192-ABPSI-12 Daimon, Y., 119-LP-15, 156-LP-20, 185-LP-24 Dally, B., 146-LP-19 Dam, B., 8-TFES-1, 35-TFES-2 Dandavino, S., 124-EP-19 Dankanich, J., 15-EP-2, 69-EP-10, 140-EP-21, 207-SCP-4 Dannenhoffer, J., 206-GTE-25 Dannenmayer, K., 155-EP-24 Dao, H., 38-EP-4 Darkwa, J., 42-EERE-2, 181-TM-7, 195-TM-8 Dassonville, R., 109-LP-14 Dausen, D., 4-HSABP/HYP-1/PC-1, 94-PC-8 Davis, E., 66-NFF-3, 83-NFF-4 Dawson, S., 53-APS-1 De Alessandro, R., 66-NFF-3 de Bock, P., 117-SCP-1 de la Torre, M., 8-TFES-1 De Matteis, P., 90-LP-11 De Rosa, M., 81-LP-10 Deans, M., 159-LP-21 Dechristopher, M., 77-TM-2 Deeken, J., 65-LP-8 Del Rosario, R., 168-GEPC-1/GTE-19 Delgado, A., 147-PC-12 Delgado, J., 155-EP-24 Denney, R., 202-GTE-24 Dennis, J., 218-PC-15 Deo, C., 72-TNES-1 Deo, H., 142-SCP-2 Deroy, C., 157-ES-1 Desmira, N., 8-TFES-1 Dessanti, B., 207-SCP-4 Dewanji, D., 218-PC-15 Dewitt, M., 168-GEPC-1/GTE-19 Di Clemente, M., 90-LP-11 Di Giacinto, M., 51-SR-3, 75-SR-5, 188-SR-9 Di Matteo, F., 81-LP-10 Diamant, K., 15-EP-2 Dick, W., 189-SR-10 Dickman, B., 108-TM-3 Didier, B., 76-ST-2 Dinardi, A., 48-LP-5 Dominguez, C., 66-NFF-3 Donbar, J., 164-HSABP/HYP-8/ABPSI-10 Doran, E., 122-HR-5 Doreswamy, R., 63-LP-7 Dotson, B., 93-EP-12 Doulgeris, G., 31-ABPSI-2/GTE-4 Doychak, J., 20-GTE-3 Driscoll, H., 74-EDU-1 Driscoll, R., 4-HSABP/HYP-1/PC-1 Drozda, T., 200-HSABP/HYP-10 Du, L., 171-GTE-20 du Clou, S., 42-EERE-2 Duchemin, O., 179-EP-26 Dumitrascu, G., 202-GTE-24 Duncan, C., 76-ST-2 Duncan, S., 12-EDGR-1, 37-EDGR-2, 45-GTE-5 Dunlap, M., 198-EC-6

Author/Session Chair Index Dunlap, P., 117-SCP-1, 142-SCP-2 Dunning, J., 190-APS-5 Dutton, J., 164-HSABP/HYP-8/ABPSI-10 Dyer, J., 122-HR-5 Eberhart, C., 18-LP-1, 185-LP-24 Ebersohn, F., 58-EP-7, 203-EP-30 Ebrahimi, H., 32-HSABP/HYP-2 Edwards, J., 32-HSABP/HYP-2, 88-HSABP/HYP-4, 200-HSABP/HYP-10 Ehrbar, E., 95-EP-13 Eilers, S., 184-HR-7, 211-HR-9 El-Refaie, A., 117-SCP-1 ElDemerdash, S., 67-EERE-3 Elharis, T., 176-GTE-21 Elliott, G., 164-HSABP/HYP-8/ABPSI-10 Elliott, T., 44-HR-2 Ellis, M., 195-TM-8 Ellison, L., 179-EP-26 Emrich, W., 213-NFF-8 Emsellem, G., 89-EP-11 Engelbrecht, C., 219-LP-26 Enoki, T., 120-EP-16 Epenoy, R., 76-ST-2 Eriguchi, K., 95-EP-13 Erwin, D., 203-EP-30 Escobar Anton, D., 179-EP-26 Eshaghi, A., 148-TFES-4 Estes, R., 132-LP-17 Estivalezes, J., 51-SR-3 Etemad, S., 33-PC-4 Etheridge, S., 33-PC-4 Evans, B., 44-HR-2, 122-HR-5, 135-EERE-4, 211-HR-9 Fabanich, W., 138-EC-5 Fabian, J., 130-GTE-15 Faenza, M., 19-HR-1, 80-HR-3, 182-EP-28, 211-HR-9 Fahim, A., 181-TM-7, 195-TM-8 Falk, G., 107-LP-13 Fallis, B., 190-APS-5 Fan, X., 26-PC-3, 62-PC-7, 88-HSABP/HYP-4, 147-PC-12 Fang, X., 139-ABPSI-9/HSABP/HYP-7 Farnell, C., 95-EP-13 Fasoulas, S., 120-EP-16 Favini, B., 51-SR-3, 75-SR-5, 188-SR-9 Fedkiw, T., 39-EP-5 Felder, J., 3-ABPSI-1/GTE-1 Feldman, M., 182-EP-28 Feldman, T., 74-EDU-1, 146-LP-19, 185-LP-24 Feng, S., 218-PC-15 Ferlin, M., 174-LP-23 Ferraiuolo, M., 90-LP-11 Ferrar, A., 110-GTE-12/ABPSI-6, 206-GTE-25 Ferrero, P., 200-HSABP/HYP-10 Ferretti, V., 51-SR-3 Ferri, F., 182-EP-28 Festa, G., 101-PC-9 Fiebig, M., 219-LP-26 Fisch, N., 179-EP-26 Fisher, T., 134-TM-4 Fittje, J., 99-NFF-5 Flandro, G., 146-LP-19 Fleurial, J., 79-EC-3 Florea, R., 110-GTE-12/ABPSI-6 Florean, F., 202-GTE-24 Florenz, R., 93-EP-12 Flores, S., 156-LP-20 Forde, S., 70-LP-9, 156-LP-20 Foster, J., 40-EP-6, 180-EP-27 Foster, L., 164-HSABP/HYP-8/ABPSI-10 Foster, W., 188-SR-9 Foti, D., 175-PC-14 Fouad, M., 108-TM-3, 149-EERE-5, 195-TM-8 Fox, M., 106-EC-4 Frankel, A., 219-LP-26 Frederick, R., 18-LP-1, 74-EDU-1, 185-LP-24 Frias, J., 147-PC-12 Fries, N., 132-LP-17 Frolik, S., 44-HR-2 Frollani, D., 144-EP-22 Fu, J., 196-APS-6 Fugger, C., 185-LP-24 Fujii, H., 210-SCP-5 Fujino, T., 97-EP-14 Fujiwara, H., 196-APS-6 Fukuda, K., 210-SCP-5 Fukunari, M., 34-APC-2, 57-ABPSI-3 Fulton, J., 88-HSABP/HYP-4 Funaki, I., 34-APC-2, 40-EP-6, 97-EP-14, 123-EP-18, 205-EP-32, 210-SCP-5 Gabriel, S., 144-EP-22, 205-EP-32 Gabrielli, R., 7-APC-1 Gaitonde, D., 32-HSABP/HYP-2 Galian, E., 66-NFF-3 Gallimore, A., 93-EP-12, 129-EP-20, 179-EP-26 Galyen, N., 206-GTE-25 Gamma, F., 135-EERE-4, 162-GTE-17, 194-TFES-6 Gan, Y., 101-PC-9, 118-PC-10 Gangoli Rao, A., 218-PC-15 Ganguly, B., 62-PC-7 Ganji, D., 43-LP-4

Garby, R., 146-LP-19 Garcia, J., 170-APC-4 Gard, L., 138-EC-5 Garg, S., 199-ABPSI-13/GTE-23 Garner, C., 140-EP-21, 180-EP-27 Gatto, C., 207-SCP-4 Gauer, M., 141-APC-3, 209-LP-25 Gauffre, M., 125-LP-16 Genevieve, B., 214-HR-8 Genin, C., 102-LP-12, 174-LP-23 George, J., 213-NFF-8 Gerards, A., 189-SR-10 Germain, B., 51-SR-3 Gernoth, A., 119-LP-15 Gerrish, H., 213-NFF-8 Gerstler, W., 117-SCP-1 Ghaddar, N., 42-EERE-2 Ghali, K., 42-EERE-2 Ghasripoor, F., 117-SCP-1 Ghezzi, U., 162-GTE-17 Ghosh, A., 126-PC-11 Gibson, A., 3-ABPSI-1/GTE-1, 31-ABPSI-2/GTE-4 Gibson, M., 6-EC-1, 134-TM-4 Giel, P., 73-GTE-9 Giel, T., 70-LP-9, 174-LP-23 Gilland, J., 89-EP-11 Gilpin, M., 7-APC-1 Gimelshein, N., 97-EP-14 Gimelshein, S., 97-EP-14 Girimaji, S., 58-EP-7, 203-EP-30 Gitzen Danner, R., 157-ES-1 Giuliano, P., 15-EP-2 Givi, P., 200-HSABP/HYP-10 Glaab, L., 207-SCP-4 Gladin, J., 86-ABPSI-5 Glauser, M., 50-GTE-6, 206-GTE-25 Glezer, A., 197-EERE-6 Glover, T., 89-EP-11 Gloyer, P., 18-LP-1, 43-LP-4, 146-LP-19 Goal, K., 106-EC-4 Goebel, D., 38-EP-4, 40-EP-6, 93-EP-12, 140-EP-21, 144-EP-22 Goetz, A., 90-LP-11 Gogineni, S., 50-GTE-6 Goldin, J., 161-SR-8 Gollahalli, S., 9-EERE-1, 96-TFES-3, 178-TFES-5 Gollor, M., 190-APS-5 Golsen, M., 73-GTE-9 Gomes, S., 118-PC-10, 214-HR-8 Gong, C., 115-HSABP/HYP-5

92

Gonzales, A., 183-EP-29, 215-EP-34 Gonçalves, R., 118-PC-10 Goodfellow, K., 203-EP-30 Gord, J., 62-PC-7 Gore, J., 178-TFES-5 Gracia, O., 148-TFES-4 Gray, P., 86-ABPSI-5 Grayson, G., 107-LP-13, 132-LP-17 Greatrix, D., 11-SR-1, 51-SR-3 Green, M., 31-ABPSI-2/GTE-4 Griswold, M., 179-EP-26 Gross, M., 78-APS-2 Gucker, S., 40-EP-6 Guelman, M., 215-EP-34 Guidos, M., 102-LP-12 Gulbinska, M., 157-ES-1 Gulli, S., 172-TM-6 Guo, Y., 199-ABPSI-13/GTE-23 Gupta, A., 8-TFES-1, 9-EERE-1, 35-TFES-2, 127-GTE-14, 148-TFES-4 Gutmark, E., 4-HSABP/HYP-1/PC-1 Haag, T., 64-EP-8, 93-EP-12 Haas, J., 120-EP-16, 208-EP-33 Habu, H., 188-SR-9 Hack, R., 127-GTE-14 Hada, T., 97-EP-14 Haddad, C., 146-LP-19 Haeberle, J., 219-LP-26 Haeseler, D., 219-LP-26 Hagenmaier, M., 115-HSABP/HYP-5 Hagiwara, K., 210-SCP-5 Haidinger, F., 219-LP-26 Haidn, O., 34-APC-2, 65-LP-8, 81-LP-10 Haight, S., 201-APC-5 Haines, J., 105-APS-3 Hall, D., 31-ABPSI-2/GTE-4 Halliwell, I., 82-GTE-10, 139-ABPSI-9/HSABP/HYP-7, 187-GTE-22 Hallock, A., 89-EP-11 Hammel, T., 138-EC-5 Hange, C., 31-ABPSI-2/GTE-4 Hannemann, K., 209-LP-25 Hansen, J., 217-SR-12 Hara, K., 215-EP-34 Hara, S., 67-EERE-3 Hardi, J., 146-LP-19 Hardin, L., 110-GTE-12/ABPSI-6 Hargus, W., 69-EP-10, 124-EP-19, 155-EP-24, 183-EP-29, 215-EP-34 Harmon, F., 196-APS-6

Harris, J., 132-LP-17 Harrison, T., 99-NFF-5, 213-NFF-8 Hartenstine, J., 195-TM-8 Hartfield, R., 88-HSABP/HYP-4, 174-LP-23, 189-SR-10 Harvazinski, M., 146-LP-19 Hasegawa, S., 87-HSABP/HYP-3 Hashimoto, T., 105-APS-3 Hassan, H., 88-HSABP/HYP-4 Hassan, K., 148-TFES-4 Hatagaki, S., 152-HR-6 Hatcher, R., 154-NFF-6 Hathaway, M., 110-GTE-12/ABPSI-6 Hauser, J., 83-NFF-4 Havrilesko, B., 82-GTE-10 Hay, R., 77-TM-2, 195-TM-8 Hayakawa, Y., 40-EP-6 He, H., 218-PC-15 Heister, S., 26-PC-3, 75-SR-5, 160-LP-22, 161-SR-8, 217-SR-12 Henderson, B., 20-GTE-3 Henderson, E., 170-APC-4 Hendricks, E., 82-GTE-10, 192-ABPSI-12 Herbertz, A., 109-LP-14, 119-LP-15 Herdrich, G., 7-APC-1, 120-EP-16, 203-EP-30 Herges, T., 164-HSABP/HYP-8/ABPSI-10 Herman, D., 40-EP-6, 69-EP-10, 93-EP-12, 123-EP-18, 129-EP-20, 155-EP-24, 180-EP-27, 183-EP-29, 204-EP-31 Hermann Hald, I., 109-LP-14, 119-LP-15 Hernandez, H., 209-LP-25 Herndon, S., 168-GEPC-1/GTE-19 Herrick, G., 110-GTE-12/ABPSI-6 Herring, N., 86-ABPSI-5 Hessel, E., 164-HSABP/HYP-8/ABPSI-10 Hickman, R., 49-NFF-2, 213-NFF-8 Higuchi, T., 40-EP-6 Hikihara, T., 12-EDGR-1, 37-EDGR-2 Hilbert, B., 206-GTE-25 Hill, D., 198-EC-6 Himeno, T., 5-PC-2, 209-LP-25 Hinerman, T., 18-LP-1, 43-LP-4 Hinkelman, M., 161-SR-8 Hirata, K., 80-HR-3, 152-HR-6 Hirata, Y., 80-HR-3 Hirota, M., 67-EERE-3, 143-TM-5 Hitt, M., 125-LP-16 Hoang, T., 28-TM-1 Hodson, S., 134-TM-4 Hofer, R., 38-EP-4, 93-EP-12, 95-EP-13, 129-EP-20, 140-EP-21

Author/Session Chair Index Hohman, K., 95-EP-13 Hojnicki, J., 76-ST-2 Holtmann, C., 6-EC-1 Hopfe, N., 52-SR-4 Hopkins, M., 93-EP-12 Hoppe, M., 37-EDGR-2 Hori, D., 185-LP-24 Horisawa, H., 62-PC-7, 205-EP-32, 210-SCP-5 Hornstein, K., 214-HR-8 Hosangadi, A., 7-APC-1, 41-ECS-2 Hosder, S., 172-TM-6 Hoshino, T., 105-APS-3, 157-ES-1 Hoskins, W., 38-EP-4 Hou, R., 171-GTE-20 Hou, Z., 218-PC-15 Houts, M., 72-TNES-1, 111-IECEC-7, 136-TNES-2, 213-NFF-8 Howard, R., 168-GEPC-1/GTE-19 Howe, S., 17-NFF-1, 49-NFF-2 Hruby, V., 39-EP-5 Hsu, K., 115-HSABP/HYP-5 Huang, H., 141-APC-3 Huang, W., 64-EP-8, 69-EP-10, 93-EP-12, 129-EP-20, 155-EP-24, 183-EP-29 Hubbard, G., 100-HR-4 Hubble, A., 40-EP-6 Huh, K., 117-SCP-1 Huo, H., 175-PC-14 Husdal, J., 214-HR-8 Hutchison, S., APS-4 Hyakutake, T., 120-EP-16 Hyams, D., 206-GTE-25 Ibrahim, A., 42-EERE-2 Ichihara, D., 120-EP-16 Ideta, K., 21-LP-2 Iha, K., 118-PC-10, 214-HR-8 Ihme, M., 18-LP-1 Iizuka, T., 21-LP-2 Ilie, M., 153-PC-13 Ilin, A., 89-EP-11 Inatani, Y., 209-LP-25 Ingenito, A., 135-EERE-4, 194-TFES-6 Inoue, C., 5-PC-2, 209-LP-25 Ise, T., 180-EP-27 Ishibashi, T., 21-LP-2 Ishihara, S., 131-SR-7 Ito, Y., 92-GTE-11, 143-TM-5 Ivanov, M., 141-APC-3 Izumi, T., 123-EP-18 Jaberi, F., 35-TFES-2, 200-HSABP/HYP-10

Jackson, D., 41-ECS-2 Jackson, T., 118-PC-10, 189-SR-10 Jacob, E., 146-LP-19 Jaffe, P., 134-TM-4 Jagoda, J., 176-GTE-21 James, R., 6-EC-1 Jang, D., 48-LP-5 Jaworske, D., 134-TM-4 Jenkins, R., 189-SR-10 Jens, E., 100-HR-4 Jensen, D., 162-GTE-17 Jernigan, F., 70-LP-9 Jia, Z., 172-TM-6 Johansson, H., 141-APC-3 Jones, D., 76-ST-2 Joo, J., 113-ABPSI-7 Jorns, B., 144-EP-22, 182-EP-28 Joyner, C., 186-NFF-7 Joyner, R., 99-NFF-5 Junwei, L., 51-SR-3 Jurgensmeyer, A., 108-TM-3 Justice, K., 82-GTE-10 Kagawa, H., 21-LP-2, 55-LP-6 Kailasanath, K., 20-GTE-3, 94-PC-8, 126-PC-11 Kaiserman, M., 104-SR-6 Kajimura, Y., 40-EP-6 Kakami, A., 21-LP-2, 131-SR-7 Kambly, K., 67-EERE-3 Kamhawi, H., 38-EP-4, 64-EP-8, 69-EP-10, 93-EP-12, 144-EP-22, 155-EP-24, 183-EP-29 Kamisaka, A., 52-SR-4 Kammash, T., 154-NFF-6 Kan, B., 160-LP-22 Kaneko, T., 156-LP-20 Kanno, T., 63-LP-7 Kapat, J., 73-GTE-9, 101-PC-9, 150-GTE-16 Kapulkin, A., 215-EP-34 Karabeyoglu, A., 19-HR-1, 22-HR-5, 135-EERE-4, 152-HR-6 Karakurt, A., 194-TFES-6, 201-APC-5 Karimi, A., 115-HSABP/HYP-5 Karl, S., 174-LP-23 Kartuzova, O., 107-LP-13 Kassemi, M., 107-LP-13 Kasten, L., 134-TM-4 Kato, K., 87-HSABP/HYP-3 Katsonis, K., 182-EP-28 Katsurayama, H., 34-APC-2 Katz, I., 38-EP-4, 93-EP-12, 140-EP-21 Kawashima, H., 156-LP-20

Kawatsu, K., 177-SCP-3 Kaya, N., 105-APS-3 Keidar, M., 64-EP-8, 68-EP-9, 95-EP-13 Kerslake, T., 140-EP-21 Kestner, B., 86-ABPSI-5 Ketsdever, A., 97-EP-14 Keutelian, P., 68-EP-9, 97-EP-14 Key, N., 10-GTE-2, 92-GTE-11, 171-GTE-20 Keyser, S., 138-EC-5 Khalil, A., 35-TFES-2 Khalil, E., 42-EERE-2, 67-EERE-3, 103-IECEC-6, 108-TM-3, 149-EERE-5, 181-TM-7, 195-TM-8 Khalil, H., 197-EERE-6 Khalil Hasan, A., 127-GTE-14 Khan, M., 148-TFES-4, 178-TFES-5 Khandelwal, B., 141-APC-3, 194-TFES-6, 201-APC-5 Khayms, V., 15-EP-2 Kibbey, T., 75-SR-5 Kidaite, Y., 67-EERE-3 Kiel, B., 20-GTE-3, 50-GTE-6, 206-GTE-25, 218-PC-15 Kim, B., 14-ECS-1 Kim, H., 3-ABPSI-1/GTE-1, 59-ABPSI-4/GTE-8, 86-ABPSI-5 Kim, J., 37-EDGR-2, 126-PC-11, 176-GTE-21 Kim, K., 14-ECS-1 Kim, T., 213-NFF-8 Kimura, I., 62-PC-7 Kinefuchi, K., 209-LP-25 King, L., 16-EP-3, 40-EP-6, 93-EP-12, 155-EP-24 Kiran, R., 176-GTE-21 Kirchberger, C., 81-LP-10 Kirk, D., 107-LP-13, 209-LP-25 Kirk, T., 117-SCP-1 Kirtley, D., 120-EP-16, 141-APC-3, 154-NFF-6 Kitagawa, K., 8-TFES-1 Kitamori, Y., 12-EDGR-1 Kitamura, S., 40-EP-6 Klatte, J., 132-LP-17 Kleinhenz, J., 159-LP-21 Knighton, B., 168-GEPC-1/GTE-19 Knuth, W., 170-APC-4 Kobayashi, H., 205-EP-32 Kodera, M., 87-HSABP/HYP-3 Koelfgen, S., 76-ST-2 Koizumi, H., 26-PC-3, 34-APC-2, 95-EP-13, 120-EP-16, 123-EP-18, 180-EP-27, 205-EP-32 Kolobov, V., 215-EP-34 Komatsu, M., 21-LP-2 Komatsu, R., 57-ABPSI-3 Komerath, N., 79-EC-3, 106-EC-4, 197-EERE-6, 207-SCP-4

93

Komurasaki, K., 26-PC-3, 34-APC-2, 57-ABPSI-3, 95-EP-13, 179-EP-26, 203-EP-30, 205-EP-32 Kongtrakool, B., 79-EC-3 Koo, H., 152-HR-6 Kopasakis, G., 164-HSABP/HYP-8/ABPSI-10 Koppel, C., 215-EP-34 Kostka, S., 50-GTE-6, 62-PC-7 Kouchi, T., 167-HSABP/HYP-9/ABPSI-11 Krishnakumar, T., 175-PC-14 Krishnamurthy, A., 68-EP-9, 97-EP-14 Kronhaus, I., 215-EP-34 Kuchle, J., 148-TFES-4 Kulkarni, S., 130-GTE-15 Kumar, A., 88-HSABP/HYP-4, 152-HR-6 Kumar, R., 39-EP-5 Kumar, V., 96-TFES-3, 178-TFES-5, 194-TFES-6 Kumaresan, V., 195-TM-8 Kummer, J., 3-ABPSI-1/GTE-1 Kundu, R., 92-GTE-11 Kuninaka, H., 40-EP-6, 120-EP-16, 123-EP-18, 180-EP-27, 182-EP-28 Kuramoto, Y., 21-LP-2 Kurosu, A., 90-LP-11 Kurth, G., 52-SR-4 Kustas, A., 108-TM-3 Kuwahara, T., 52-SR-4, 104-SR-6 Kwankaomeng, S., 79-EC-3 Kwon, S., 48-LP-5 Lago, V., 70-LP-9 Lakebrink, M., 113-ABPSI-7 Lam, G., 53-APS-1 Lambert, M., 209-LP-25 Lamm, P., 196-APS-6 Langhenry, M., 11-SR-1, 131-SR-7, 188-SR-9 Larsson, J., 200-HSABP/HYP-10 Laskaridis, P., 31-ABPSI-2/GTE-4 Lassoudiere, F., 70-LP-9 Lau, M., 203-EP-30 Laughery, S., 137-APS-4 Lazzarin, M., 19-HR-1, 177-SCP-3, 209-LP-25 Le, D., 164-HSABP/HYP-8/ABPSI-10 Lear, W., 42-EERE-2, 135-EERE-4, 158-IECEC-9 Leary, B., 161-SR-8 Lee, C., 113-ABPSI-7, 152-HR-6 Lee, D., 17-NFF-1 Lee, H., 41-ECS-2 Lee, J., 33-PC-4, 48-LP-5 Lee, S., 126-PC-11 Leichtfuss, S., 10-GTE-2 Leighton, C., 6-EC-1

Leland, D., 53-APS-1 Lelias, G., 31-ABPSI-2/GTE-4 Lemieux, P., 184-HR-7 Lepsch, R., 170-APC-4 Lesage, B., 122-HR-5 Levack, D., 186-NFF-7 Levin, D., 39-EP-5 Lewandowski, E., 191-IECEC-11, 198-EC-6 Leylegian, J., 153-PC-13, 175-PC-14 Leyva, I., 18-LP-1 Li, J., 11-SR-1, 26-PC-3 Li, S., 131-SR-7 Li, Y., 167-HSABP/HYP-9/ABPSI-11, 196-APS-6 Li, Z., 39-EP-5 Liang, J., 87-HSABP/HYP-3, 94-PC-8, 115-HSABP/HYP-5, 126-PC-11 Lieuwen, T., 26-PC-3 Liffring, M., 196-APS-6 Lilley, D., 9-EERE-1, 148-TFES-4, 178-TFES-5, 194-TFES-6 Lin, J., 102-LP-12 Lin, R., 113-ABPSI-7 Lin, Z., 94-PC-8, 126-PC-11 Lineberry, D., 18-LP-1, 63-LP-7, 125-LP-16, 185-LP-24 Liou, M., 86-ABPSI-5 Lipsey, T., 108-TM-3 Little, J., 58-EP-7 Liu, C., 3-ABPSI-1/GTE-1 Liu, J., 32-HSABP/HYP-2, 52-SR-4 Liu, L., 196-APS-6 Liu, T., 93-EP-12 Liu, W., 94-PC-8 Liu, X., 171-GTE-20, 205-EP-32 Ljubanovic, D., 134-TM-4 Locke, J., 65-LP-8, 146-LP-19 Loehr, R., 201-APC-5 Long, D., 20-GTE-3 Longmier, B., 89-EP-11, 203-EP-30 Loop, B., 196-APS-6 Lopez, A., 132-LP-17, 209-LP-25 Love, N., 8-TFES-1, 35-TFES-2, 148-TFES-4, 194-TFES-6 Loverich, J., 180-EP-27 Low, K., 50-GTE-6 Lozano, P., 39-EP-5, 124-EP-19 Lu, J., 199-ABPSI-13/GTE-23 Lu, K., 195-TM-8 Lubkeman, J., 215-EP-34 Lucca Fabris, A., 182-EP-28 Luke, E., 55-LP-6, 102-LP-12 Lynch, E., 26-PC-3

Author/Session Chair Index Lyne, J., 201-APC-5 Ma, X., 196-APS-6 Mace, J., 113-ABPSI-7 MacInnis, D., 52-SR-4 Mack, M., 142-SCP-2 Madavan, N., 59-ABPSI-4/GTE-8 Maddalena, L., 172-TM-6 Madhanabharatam, B., 100-HR-4, 115-HSABP/HYP-5 Mahadevan, S., 73-GTE-9 Mahalingam, S., 180-EP-27 Maini, A., 195-TM-8 Majdalani, J., 19-HR-1, 44-HR-2, 146-LP-19, 214-HR-8 Malo-Molina, F., 32-HSABP/HYP-2 Manente, M., 19-HR-1, 182-EP-28 Manfletti, C., 159-LP-21 Mani, M., 113-ABPSI-7 Mankins, J., 105-APS-3 Manna, S., 203-EP-30 Mao, H., 123-EP-18 Marcu, B., 27-LP-3, 55-LP-6 Marshall, W., 159-LP-21 Martelli, E., 81-LP-10 Martin, M., 89-EP-11 Maruyama, N., 67-EERE-3, 143-TM-5 Mascanzoni, F., 188-SR-9 Masoud, A., 42-EERE-2 Masse, R., 48-LP-5 Masuda, Y., 26-PC-3, 143-TM-5 Masuya, G., 167-HSABP/HYP-9/ABPSI-11 Matalanis, C., 110-GTE-12/ABPSI-6 Matsuoka, T., 97-EP-14 Matsuzawa, Y., 62-PC-7 Mavris, D., 12-EDGR-1, 31-ABPSI-2/GTE-4, 37-EDGR-2, 45-GTE-5, 82-GTE-10, 86-ABPSI-5, 113-ABPSI-7, 199-ABPSI-13/GTE-23, 202-GTE-24 May, M., 206-GTE-25 Mazouffre, S., 155-EP-24 McAlpine, W., 53-APS-1 McCauley, R., 76-ST-2 McCleskey, C., 170-APC-4 McCoy, R., 41-ECS-2 McCulley, J., 100-HR-4, 184-HR-7 McCurdy, D., 186-NFF-7 McDonell, V., 127-GTE-14, 218-PC-15 McDougle, S., 41-ECS-2 McGowan, R., 197-EERE-6 McKay, B., 86-ABPSI-5, 164-HSABP/HYP-8/ABPSI-10 McKeon, B., 18-LP-1 Mckinney, L., 32-HSABP/HYP-2 McManus, K., 33-PC-4 McMillan, M., 139-ABPSI-9/HSABP/HYP-7 McVetta, A., 73-GTE-9 Meeks, W., 89-EP-11 Meer, D., 198-EC-6 Meholic, G., 17-NFF-1, 66-NFF-3 Mehta, J., 8-TFES-1, 96-TFES-3, 134-TM-4, 143-TM-5, 172-TM-6 Menart, J., 180-EP-27 Menon, S., 153-PC-13, 175-PC-14 Merino-Martinez, M., 58-EP-7, 97-EP-14, 120-EP-16, 155-EP-24 Merkle, C., 26-PC-3, 146-LP-19 Methel, J., 10-GTE-2 Meyer, E., 155-EP-24 Meyer, M., 109-LP-14, 156-LP-20 Meyers, N., 125-LP-16 Miakelye, R., 168-GEPC-1/GTE-19 Micheletti, D., 135-EERE-4 Michlitsch, J., 80-HR-3, 152-HR-6 Mihara, Y., 177-SCP-3 Mikellides, I., 38-EP-4, 93-EP-12, 144-EP-22 Milana, C., 188-SR-9 Miley, G., 68-EP-9, 97-EP-14, 105-APS-3 Miller, J., 74-EDU-1 Miller, M., 12-EDGR-1 Miller, S., 39-EP-5, 48-LP-5, 219-LP-26 Milligan, R., 115-HSABP/HYP-5 Millis, M., 66-NFF-3, 83-NFF-4 Mingo Perez, A., 205-EP-32 Minor, B., 108-TM-3 Mireles, O., 49-NFF-2 Miyasaka, T., 40-EP-6 Miyashita, N., 21-LP-2 Miyazaki, K., 40-EP-6 Moehlenkamp, R., 116-HSABP/HYP-6 Moeller, T., 206-GTE-25 Moldenhauer, S., 6-EC-1 Molino, N., 45-GTE-5 Molintas, H., 135-EERE-4 Mondragon, U., 218-PC-15 Mongia, H., 96-TFES-3, 178-TFES-5, 194-TFES-6 Montgomery, J., 195-TM-8 Moore, N., 132-LP-17 Moretto, F., 122-HR-5, 177-SCP-3 Morgan, C., 185-LP-24 Morgan, O., 48-LP-5 Morillas, K., 197-EERE-6 Morris, P., 50-GTE-6 Morton, C., 9-EERE-1 Mueller, N., 4-HSABP/HYP-1/PC-1, 176-GTE-21

Munday, D., 4-HSABP/HYP-1/PC-1 Mundt, C., 87-HSABP/HYP-3, 192-ABPSI-12 Munk, M., 207-SCP-4 Murakami, D., 17-NFF-1 Musielak, D., 88-HSABP/HYP-4, 116-HSABP/HYP-6, 200-HSABP/HYP-10 Muñoz, H., 57-ABPSI-3 Myre, D., 122-HR-5, 184-HR-7, 214-HR-8 Müller, I., 109-LP-14 Müller, M., 10-GTE-2 Na, Y., 152-HR-6 Nagano, H., 40-EP-6 Nagao, N., 63-LP-7 Nagasaki, T., 92-GTE-11 Nagata, K., 143-TM-5 Nagata, T., 21-LP-2, 159-LP-21 Naik, S., 96-TFES-3, 178-TFES-5, 194-TFES-6 Naito, H., 105-APS-3, 157-ES-1 Najjar, F., 189-SR-10 Nakagawa, I., 152-HR-6 Nakamura, T., 97-EP-14 Nakano, M., 26-PC-3, 40-EP-6 Nakano, T., 92-GTE-11 Nakashima, H., 38-EP-4 Nakayama, Y., 40-EP-6 Nakles, M., 64-EP-8, 69-EP-10, 155-EP-24 Nalim, M., 115-HSABP/HYP-5, 176-GTE-21 Nan, X., 167-HSABP/HYP-9/ABPSI-11 Nanda, M., 195-TM-8 Nanri, H., 63-LP-7 Naraghi, M., 109-LP-14 Narayana Swamy, A., 147-PC-12 Naruo, Y., 209-LP-25 Nasuti, F., 44-HR-2, 81-LP-10, 109-LP-14, 119-LP-15, 189-SR-10 Natan, B., 215-EP-34 Natsui, G., 73-GTE-9 Naumann, K., 52-SR-4 Navarro, C., 65-LP-8 Navarro, J., 58-EP-7, 97-EP-14 Neau, H., 125-LP-16 Neely, A., 34-APC-2 Negishi, H., 119-LP-15, 156-LP-20 Negri, M., 101-PC-9 Neri, A., 75-SR-5 Nesmith, B., 79-EC-3 Netter, G., 132-LP-17 Neumaier, W., 21-LP-2 Nguyen, B., 134-TM-4 Nguyen, T., 61-PC-6, 147-PC-12

94

Nie, W., 218-PC-15 Nishida, H., 97-EP-14, 210-SCP-5 Nishikizawa, S., 21-LP-2 Nishiyama, K., 180-EP-27 Nix, A., 56-GTE-7, 73-GTE-9, 150-GTE-16 Noble, D., 26-PC-3 Nomura, H., 196-APS-6 Nonaka, S., 209-LP-25 Nunez, J., 35-TFES-2 Nunome, Y., 119-LP-15 O’Brien, T., 164-HSABP/HYP-8/ABPSI-10 O’Brien, W., 110-GTE-12/ABPSI-6, 130-GTE-15, 206-GTE-25 O’Neil, P., 217-SR-12 Obermaier, G., 90-LP-11 Oda, Y., 57-ABPSI-3 Oefelein, J., 147-PC-12 Ogawa, K., 105-APS-3 Ogedengbe, E., 79-EC-3, 197-EERE-6 Oghienko, S., 179-EP-26 Ohkawa, Y., 40-EP-6 Ohmichi, W., 182-EP-28 Ohyama, S., 80-HR-3 Oide, S., 104-SR-6 Okai, K., 196-APS-6 Okamoto, M., 67-EERE-3 Okamura, K., 205-EP-32 Okayasu, A., 55-LP-6 Okita, K., 177-SCP-3, 209-LP-25 Olendarev, V., 179-EP-26 Oleson, S., 140-EP-21 Oliveira, L., 57-ABPSI-3 Olsen, C., 203-EP-30 Ommi, F., 43-LP-4 Ono, K., 95-EP-13 Onofri, M., 81-LP-10, 109-LP-14, 189-SR-10 Orbekk, E., 11-SR-1 Oriti, S., 106-EC-4, 198-EC-6 Ortelt, M., 109-LP-14, 119-LP-15 Ortjoahnn, E., 37-EDGR-2 Osawa, Y., 75-SR-5 Oschwald, M., 146-LP-19 Oshio, Y., 210-SCP-5 Osvalds, E., 45-GTE-5 Oswald, J., 70-LP-9 Otis, C., 200-HSABP/HYP-10 Otting, W., 138-EC-5 Packard, T., 186-NFF-7 Page, M., 28-TM-1 Paintal, S., 64-EP-8

Paiva, C., 7-APC-1 Palaszewski, B., 17-NFF-1 Palmer, P., 141-APC-3 Pancotti, A., 141-APC-3, 154-NFF-6, 182-EP-28 Panda, P., 96-TFES-3, 178-TFES-5, 194-TFES-6 Paniagua, G., 73-GTE-9, 92-GTE-11 Pantoya, M., 41-ECS-2 Park, K., 75-SR-5 Park, S., 126-PC-11 Parkin, K., 17-NFF-1 Parthasarathy, R., 9-EERE-1 Paseur, L., 70-LP-9 Pastrone, D., 162-GTE-17, 184-HR-7 Patel, M., 78-APS-2 Patino, M., 155-EP-24 Patterson, M., 13-EP-1, 40-EP-6, 180-EP-27 Paulon, D., 177-SCP-3 Pavarin, D., 19-HR-1, 80-HR-3, 182-EP-28, 209-LP-25, 211-HR-9 Pavlov, B., 148-TFES-4 Pederson, D., 76-ST-2 Pei, X., 52-SR-4 Pellicone, D., 195-TM-8 Pencil, E., 13-EP-1, 207-SCP-4 Pendharkar, A., 197-EERE-6 Penkel, B., 180-EP-27 Periagaram, K., 26-PC-3 Perigo, D., 102-LP-12, 174-LP-23 Perna, L., 124-EP-19 Persson, M., 48-LP-5 Perullo, C., 31-ABPSI-2/GTE-4, 82-GTE-10 Pestak, C., 79-EC-3 Petcu, A., 202-GTE-24 Peterson, P., 40-EP-6, 93-EP-12, 179-EP-26 Peterson, T., 64-EP-8, 98-EP-15, 207-SCP-4 Peterson, Z., 184-HR-7 Petitot, S., 125-LP-16 Pfaff, M., 154-NFF-6 Piechna, J., 4-HSABP/HYP-1/PC-1, 176-GTE-21 Pihl, C., 141-APC-3, 154-NFF-6 Pilidis, P., 31-ABPSI-2/GTE-4 Pinder, M., 197-EERE-6 Pineda, F., 63-LP-7 Pinero, L., 190-APS-5 Pinto, F., 7-APC-1 Pisharady, J., 175-PC-14 Piszczor, M., 6-EC-1 Pitot, J., 214-HR-8 Pitts, H., 70-LP-9 Pixberg, C., 10-GTE-2

Author/Session Chair Index Pizzarelli, M., 109-LP-14, 119-LP-15 Plasek, M., 144-EP-22 Poinsot, T., 146-LP-19 Polanka, M., 57-ABPSI-3 Polk, J., 93-EP-12, 144-EP-22, 155-EP-24 Polzin, K., 58-EP-7, 89-EP-11 Pomeroy, B., 185-LP-24 Ponti, F., 104-SR-6 Popp, C., 70-LP-9 Porumbel, I., 202-GTE-24 Pote, B., 64-EP-8 Pouffary, B., 55-LP-6 Poulsen, B., 14-ECS-1 Pourpoint, T., 100-HR-4, 119-LP-15, 159-LP-21, 218-PC-15 Pourquie, M., 218-PC-15 Powell, S., 87-HSABP/HYP-3 Prakash, A., 201-APC-5 Prakash, J., 175-PC-14 Prasad, J., 92-GTE-11 Preclik, D., 65-LP-8, 90-LP-11 Prince, B., 39-EP-5, 69-EP-10, 129-EP-20 Puglia, F., 157-ES-1 Pugmire, K., 133-LP-18 Qiao, L., 101-PC-9, 118-PC-10, 148-TFES-4, 178-TFES-5 Qin, J., 172-TM-6 Qualls, L., 49-NFF-2, 99-NFF-5 Quiller, T., 97-EP-14 Raghav, V., 106-EC-4 Raitses, Y., 144-EP-22, 151-EP-23, 179-EP-26 Raju, M., 5-PC-2 Ramesh, G., 175-PC-14 Ratul, T., 9-EERE-1 Raudsandmoen, G., 214-HR-8 Rayman, M., 180-EP-27 Reba, R., 20-GTE-3 Redaelli, M., 101-PC-9 Reddy, T., 110-GTE-12/ABPSI-6 Reed, B., 76-ST-2 Reid, T., 138-EC-5 Reilly, M., 68-EP-9, 97-EP-14 Remy, K., 215-EP-34 Rettenmaier, A., 74-EDU-1, 161-SR-8 Rhodes, R., 170-APC-4 Riccius, J., 119-LP-15 Ricklick, M., 73-GTE-9, 101-PC-9 Rink, K., 14-ECS-1 Ritter, P., 201-APC-5 Roberts, L., 28-TM-1, 214-HR-8 Robin, M., 64-EP-8, 95-EP-13 Robinson, J., 34-APC-2, 141-APC-3, 170-APC-4, 201-APC-5 Robinson, N., 74-EDU-1 Rocandio, P., 92-GTE-11 Rocco, J., 118-PC-10, 214-HR-8 Rocco, L., 118-PC-10, 214-HR-8 Rodriguez, C., 34-APC-2 Romanchuk, B., 4-HSABP/HYP-1/PC-1 Rondini, D., 19-HR-1, 177-SCP-3 Ronningen, J., 122-HR-5, 214-HR-8 Rosaire, G., 72-TNES-1 Rosenblad, N., 95-EP-13 Roser, H., 120-EP-16 Roth, J., 107-LP-13 Roufberg, L., 53-APS-1, 105-APS-3, 137-APS-4 Rovey, J., 39-EP-5, 89-EP-11 Roy, A., 147-PC-12 Roy, B., 73-GTE-9 Roy, K., 175-PC-14 Roy, S., 62-PC-7 Ruault, J., 76-ST-2 Rubanovich, M., 215-EP-34 Ruf, J., 102-LP-12 Ruggiero, E., 117-SCP-1 Ruscher, C., 206-GTE-25 Russo Sorge, A., 101-PC-9 Ryan, C., 124-EP-19 Ryan, W., 217-SR-12 Saburo, Y., 80-HR-3, 152-HR-6 Sachdev, J., 41-ECS-2 Sahara, H., 21-LP-2, 210-SCP-5 Sait, H., 143-TM-5 Saito, D., 80-HR-3 Saitoh, S., 57-ABPSI-3 Sakamoto, K., 57-ABPSI-3 Sakurai, T., 80-HR-3, 152-HR-6 Salim, A., 137-APS-4, 190-APS-5 Salvador, J., 134-TM-4 Salvatore, V., 90-LP-11 Samborsky, R., 17-NFF-1 Sampson, M., 134-TM-4 Sanal Kumar, V., 131-SR-7 Sanborn, W., 41-ECS-2 Sanchez, L., 65-LP-8 Sanders, B., 164-HSABP/HYP-8/ABPSI-10 Sandrine, P., 70-LP-9 Sands, J., 45-GTE-5, 86-ABPSI-5 Sandu, C., 202-GTE-24 Sano, N., 188-SR-9 Santee, S., 157-ES-1

Santos, P., 160-LP-22 Sanzi, J., 134-TM-4, 143-TM-5 Saracoglu, B., 73-GTE-9 Sardeshmukh, S., 26-PC-3 Sargent, D., 160-LP-22 Sarker, S., 35-TFES-2 Sarmiento, C., 159-LP-21 Sasaki, M., 119-LP-15, 156-LP-20 Sasoh, A., 120-EP-16 Satoh, S., 97-EP-14 Sattelmayer, T., 65-LP-8 Sauer, J., 102-LP-12, 159-LP-21 Saulsberry, R., 41-ECS-2 Saunders, J., 164-HSABP/HYP-8/ABPSI-10 Sauvageau, D., 23-ST-1 Saviers, K., 134-TM-4 Scharfe, D., 7-APC-1 Scharfe, M., 183-EP-29 Scharnhorst, R., 86-ABPSI-5 Schiffer, P., 10-GTE-2 Schiltgen, B., 31-ABPSI-2/GTE-4 Schlechtriem, S., 119-LP-15 Schlieben, G., 81-LP-10 Schlinker, R., 20-GTE-3 Schmid, M., 65-LP-8 Schmidt, J., 62-PC-7 Schmitz, P., 138-EC-5, 198-EC-6 Schmuland, D., 201-APC-5 Schneider, S., 159-LP-21 Schnitzler, B., 99-NFF-5, 186-NFF-7 Schutte, J., 45-GTE-5 Schwenk, D., 189-SR-10 Schwer, D., 94-PC-8 Schönherr, T., 203-EP-30, 205-EP-32 Scroggins, A., 125-LP-16 Sedwick, R., 68-EP-9, 154-NFF-6 Segal, C., 147-PC-12 Seidel, J., 192-ABPSI-12 Seidler, W., 154-NFF-6 Seitzman, J., 26-PC-3, 176-GTE-21 Sekar, B., 33-PC-4, 206-GTE-25 Selim, H., 8-TFES-1 Selle, L., 146-LP-19 Selmo, A., 182-EP-28 Selzer, M., 109-LP-14 Seo, H., 126-PC-11 Serraglia, F., 51-SR-3, 75-SR-5, 188-SR-9 Setayesh, B., 74-EDU-1 Sethi, V., 194-TFES-6, 201-APC-5 Sforzo, B., 176-GTE-21

95

Shabelowitz, A., 179-EP-26 Shabbir, A., 110-GTE-12/ABPSI-6 Shafirovich, E., 147-PC-12 Shah, S., 79-EC-3 Shahin, A., 149-EERE-5 Shamrai, K., 97-EP-14 Shanley, K., 192-ABPSI-12 Sharma, O., 110-GTE-12/ABPSI-6 Shashurin, A., 68-EP-9 Shastry, R., 64-EP-8, 69-EP-10, 93-EP-12, 123-EP-18, 155-EP-24, 180-EP-27, 183-EP-29, 215-EP-34 Shaw, R., 84-IECEC-5, 112-IECEC-8, 157-ES-1, 165-IECEC-10 Shea, H., 124-EP-19 Shebalin, J., 58-EP-7, 203-EP-30 Shehata, M., 149-EERE-5 Shelton, A., 189-SR-10 Shen, X., 117-SCP-1 Sherif, S., 42-EERE-2 Shibasaki, T., 63-LP-7 Shijie, L., 94-PC-8 Shimada, T., 80-HR-3 Shimizu, F., 188-SR-9 Shimizu, S., 55-LP-6 Shimizu, T., 185-LP-24 Shinohara, I., 40-EP-6 Shinohara, K., 152-HR-6 Shinohara, S., 97-EP-14 Shiraishi, N., 80-HR-3, 152-HR-6 Sievers, R., 138-EC-5 Sikarwar, N., 50-GTE-6 Simeoni, F., 162-GTE-17, 184-HR-7 Simonin, O., 125-LP-16 Simpson, M., 197-EERE-6 Simurda, L., 214-HR-8 Singh, A., 148-TFES-4 Singh, R., 31-ABPSI-2/GTE-4, 194-TFES-6, 201-APC-5 Sir, M., 76-ST-2 Sirbi, A., 132-LP-17 Sirignano, W., 33-PC-4 Slater, J., 164-HSABP/HYP-8/ABPSI-10 Slavinskaya, N., 61-PC-6 Slippey, A., 77-TM-2 Slough, J., 141-APC-3, 154-NFF-6 Smith, B., 53-APS-1, 57-ABPSI-3 Smith, E., 198-EC-6 Smith, G., 55-LP-6 Smith, K., 176-GTE-21 Smith, N., 10-GTE-2, 171-GTE-20 Smyth, J., 55-LP-6

Snedden, G., 55-LP-6 Snyder, C., 122-HR-5 Snyder, J., 93-EP-12, 140-EP-21 Snyder, M., 74-EDU-1 Soeder, J., 190-APS-5 Sohn, C., 61-PC-6 Son, S., 100-HR-4, 218-PC-15 Song, G., 87-HSABP/HYP-3 Song, Y., 6-EC-1 Sordyl, J., 163-GTE-18, 176-GTE-21 Soulas, G., 69-EP-10, 93-EP-12, 155-EP-24, 179-EP-26, 183-EP-29 Spektor, R., 15-EP-2 Spencer, S., 28-TM-1, 77-TM-2, 134-TM-4 Spero, J., 153-PC-13 Spores, R., 48-LP-5 Spurling, J., 51-SR-3 Squire, J., 89-EP-11 Sreenivas, K., 206-GTE-25 Srinivasan, S., 153-PC-13 Srivastava, A., 79-EC-3, 106-EC-4 Srivastava, V., 6-EC-1 St Germain, B., 76-ST-2 St. George, A., 4-HSABP/HYP-1/PC-1 Staack, D., 58-EP-7, 203-EP-30 Stanic, M., 154-NFF-6 Stark, J., 124-EP-19 Stark, R., 34-APC-2, 102-LP-12, 174-LP-23 Stark, T., 6-EC-1 Statham, G., 154-NFF-6 Steenken, W., 113-ABPSI-7 Steinetz, B., 117-SCP-1, 142-SCP-2 Stella, P., 53-APS-1 Stevens, J., 211-HR-9 Stewart, M., 99-NFF-5 Stiegemeier, B., 156-LP-20 Stober, K., 214-HR-8 Stoddard, W., 4-HSABP/HYP-1/PC-1 Stoltz, P., 180-EP-27 Stucky, M., 110-GTE-12/ABPSI-6 Stueber, T., 167-HSABP/HYP-9/ABPSI-11 Su, C., 53-APS-1 Su, L., 218-PC-15 Su, O., 181-TM-7 Su, W., 11-SR-1 Suder, K., 130-GTE-15 Sugimori, D., 63-LP-7 Sullivan, R., 26-PC-3 Sullivan-Lewis, E., 127-GTE-14 Sun, D., 171-GTE-20

Author/Session Chair Index Sun, M., 87-HSABP/HYP-3, 115-HSABP/HYP-5 Sun, X., 171-GTE-20 Suresh, A., 92-GTE-11 Suslov, D., 65-LP-8 Sutton, R., 28-TM-1 Suzuki, J., 62-PC-7 Suzuki, N., 21-LP-2 Sventitskiy, A., 192-ABPSI-12 Swanson, T., 182-EP-28 Sweida, W., 149-EERE-5 Swiatek, M., 15-EP-2 Sylvain, G., 70-LP-9 Szabo, J., 64-EP-8, 93-EP-12 Szucs, P., 92-GTE-11 Tachibana, T., 21-LP-2, 131-SR-7 Tagashira, T., 196-APS-6 Taherbaneh, M., 190-APS-5 Tai, J., 45-GTE-5, 82-GTE-10, 127-GTE-14, 202-GTE-24 Tajika, T., 21-LP-2 Takagi, A., 210-SCP-5 Takahashi, K., 52-SR-4, 104-SR-6 Takahashi, N., 39-EP-5 Takahashi, R., 12-EDGR-1 Takao, Y., 95-EP-13 Takegahara, H., 21-LP-2 Taketoshi, H., 131-SR-7 Takubo, M., 120-EP-16 Talty, T., 21-LP-2 Tanaka, K., 210-SCP-5 Tanaka, M., 75-SR-5 Tangirala, V., 4-HSABP/HYP-1/PC-1 Tani, K., 87-HSABP/HYP-3 Tani, N., 90-LP-11, 177-SCP-3 Tani, T., 157-ES-1 Tani, Y., 80-HR-3 Tanikawa, T., 97-EP-14 Tarau, C., 28-TM-1, 77-TM-2, 108-TM-3, 134-TM-4, 172-TM-6 Tashiro, K., 12-EDGR-1 Telitschkin, D., 141-APC-3 Thakur, S., 18-LP-1, 55-LP-6 Thess, A., 6-EC-1 Thomas, R., 58-EP-7, 175-PC-14 Thornburg, H., 33-PC-4 Thorpe, D., 170-APC-4 Tian, L., 87-HSABP/HYP-3 Tian, V., 18-LP-1 Tianyi, S., 94-PC-8 Tillman, G., 110-GTE-12/ABPSI-6, 113-ABPSI-7, 130-GTE-15 Timko, M., 168-GEPC-1/GTE-19 Tiwari, P., 92-GTE-11 Tokudome, S., 188-SR-9 Tomioka, S., 87-HSABP/HYP-3 Tomita, T., 119-LP-15, 156-LP-20 Tong, M., 3-ABPSI-1/GTE-1, 82-GTE-10 Toro, C., 107-LP-13 Torregrosa Mira, M., 67-EERE-3 Torres, J., 159-LP-21 Townsend, M., 17-NFF-1 Trammell, M., 49-NFF-2 Tran, V., 9-EERE-1 Trawick, D., 31-ABPSI-2/GTE-4 Trehan, R., 73-GTE-9 Trejo, A., 156-LP-20 Trela, M., 219-LP-26 Trezzolani, F., 182-EP-28 Troutman, J., 157-ES-1 Tsay, M., 95-EP-13 Tsukizaki, R., 180-EP-27 Tsvetkov, P., 72-TNES-1, 136-TNES-2 Tu, H., 196-APS-6 Tucker, K., 18-LP-1 Tulino, V., 175-PC-14 Turchi, A., 189-SR-10 Ueda, S., 87-HSABP/HYP-3 Ueda, T., 63-LP-7 Ui, K., 188-SR-9 Ulloa-Severino, A., 78-APS-2 Ulmen, B., 68-EP-9, 97-EP-14 Umemura, Y., 209-LP-25 Upadhyay, P., 120-EP-16 Uzawa, S., 5-PC-2 Valdez, C., 35-TFES-2 van Buijtenen, J., 218-PC-15 Van Noord, J., 68-EP-9, 144-EP-22 Van Zante, D., 130-GTE-15 Vasile, M., 105-APS-3 Velraj, R., 195-TM-8 Venanzi, M., 81-LP-10 Venkateswaran, P., 33-PC-4, 47-PC-5 Vento, D., 207-SCP-4 Verma, S., 34-APC-2 Veryutin, S., 179-EP-26 Vesterås, R., 122-HR-5, 214-HR-8 Vigouroux, J., 55-LP-6 Villarreal, J., 104-SR-6, 216-SR-11 Vitucci, J., 68-EP-9 Vogel, P., 32-HSABP/HYP-2 Votroubek, G., 154-NFF-6

Votta, R., 90-LP-11 Vrnak, D., 164-HSABP/HYP-8/ABPSI-10 Vu, A., 37-EDGR-2 Walia, J., 117-SCP-1 Walker, K., 195-TM-8 Walker, M., 38-EP-4, 97-EP-14 Wall, T., 76-ST-2 Walters, E., 196-APS-6 Wang, F., 205-EP-32 Wang, J., 94-PC-8 Wang, L., 199-ABPSI-13/GTE-23 Wang, N., 11-SR-1, 51-SR-3, 52-SR-4, 205-EP-32 Wang, S., 205-EP-32 Wang, T., 102-LP-12 Wang, W., 119-LP-15, 185-LP-24 Wang, X., 138-EC-5 Wang, Y., 131-SR-7 Warren, J., 49-NFF-2, 186-NFF-7 Washeleski, R., 155-EP-24 Wasistho, B., 189-SR-10 Watanabe, H., 40-EP-6 Watanabe, T., 5-PC-2, 209-LP-25 Waxman, B., 80-HR-3, 122-HR-5 Webster, G., 107-LP-13 Webster, R., 206-GTE-25 Weeks, B., 41-ECS-2 Wegeng, R., 79-EC-3 Wei, B., 87-HSABP/HYP-3 Wei, L., 126-PC-11 Weir, L., 164-HSABP/HYP-8/ABPSI-10 Welch, G., 206-GTE-25 Wells, M., 21-LP-2 Wernet, M., 130-GTE-15 West, J., 55-LP-6 Westphal, W., 57-ABPSI-3 Wey, C., 168-GEPC-1/GTE-19 White, C., 147-PC-12 White, J., 200-HSABP/HYP-10 Whitfield, D., 206-GTE-25 Whitmore, S., 100-HR-4, 184-HR-7, 211-HR-9 Whitmore, T., 184-HR-7 Wiegerink, R., 141-APC-3 Wierman, M., 185-LP-24 Wijeyakulasuriya, S., 115-HSABP/HYP-5, 176-GTE-21 Wilde, B., 26-PC-3 Wilhite, A., 88-HSABP/HYP-4 Willams, J., 108-TM-3 Williams, D., 108-TM-3 Williams, G., 93-EP-12, 129-EP-20, 156-LP-20, 180-EP-27, 204-EP-31

96

Williams, L., 83-NFF-4 Williams, Z., 198-EC-6 Willis, W., 219-LP-26 Wilson, K., 198-EC-6 Wilson, M., 184-HR-7, 211-HR-9, 219-LP-26 Wilson, S., 106-EC-4, 138-EC-5 Winters, B., 55-LP-6 Wirasanti, P., 37-EDGR-2 Wirz, R., 95-EP-13, 97-EP-14, 123-EP-18, 151-EP-23, 155-EP-24 Witcher, J., 137-APS-4 Wolff, M., 10-GTE-2 Wolford, D., 6-EC-1 Wong, W., 198-EC-6 Woodward, J., 66-NFF-3 Woolwine, K., 164-HSABP/HYP-8/ABPSI-10 Wright, J., 18-LP-1, 55-LP-6 Wright, R., 94-PC-8 Wu, J., 199-ABPSI-13/GTE-23 Wu, Z., 205-EP-32 Wyczalek, F., 106-EC-4, 197-EERE-6 Wyczalek, M., 106-EC-4, 197-EERE-6 Wyczalek, T., 106-EC-4, 197-EERE-6 Xia, G., 26-PC-3 Xing, S., 51-SR-3 Xu, H., 126-PC-11 Xu, J., 178-TFES-5 Xu, K., 38-EP-4 Xu, X., 87-HSABP/HYP-3 Ya, Z., 217-SR-12 Yachi, Y., 188-SR-9 Yalin, A., 38-EP-4 Yamagiwa, Y., 123-EP-18, 210-SCP-5 Yamaguchi, T., 34-APC-2, 57-ABPSI-3 Yamamoto, N., 38-EP-4, 92-GTE-11, 210-SCP-5 Yamanishi, N., 90-LP-11, 119-LP-15, 156-LP-20, 177-SCP-3 Yamauchi, S., 104-SR-6 Yanagi, R., 196-APS-6 Yandong, Z., 51-SR-3 Yang, H., 209-LP-25 Yang, L., 14-ECS-1, 87-HSABP/HYP-3, 205-EP-32 Yang, M., 62-PC-7 Yang, V., 171-GTE-20, 175-PC-14, 218-PC-15 Yang, X., 105-APS-3 Yentsch, R., 32-HSABP/HYP-2 Yilmaz, A., 215-EP-34 Yim, J., 15-EP-2 Yoh, J., 14-ECS-1 Yokomine, Y., 75-SR-5

Yokota, S., 120-EP-16 Yongsheng, L., 94-PC-8 Yoon, C., 160-LP-22 Yoon, J., 65-LP-8 Yoon, Y., 65-LP-8 Yoshimura, N., 210-SCP-5 Young, J., 15-EP-2, 34-APC-2 Young, M., 7-APC-1 Young, R., 174-LP-23 Yu, B., 172-TM-6 Yu, G., 62-PC-7 Yu, K., 126-PC-11 Yu, M., 148-TFES-4 Yuan, Y., 26-PC-3, 62-PC-7 Yuasa, S., 152-HR-6 Yuhui, W., 94-PC-8 Yusi, L., 94-PC-8 Zakrzwski, C., 219-LP-26 Zaseck, C., 100-HR-4 Zhang, D., 172-TM-6 Zhang, K., 139-ABPSI-9/HSABP/HYP-7, 167-HSABP/HYP-9/ABPSI-11 Zhang, L., 139-ABPSI-9/HSABP/HYP-7 Zhang, Q., 11-SR-1, 51-SR-3 Zhang, S., 199-ABPSI-13/GTE-23 Zhang, T., 26-PC-3, 62-PC-7 Zhang, Y., 11-SR-1, 87-HSABP/HYP-3 Zhao, Y., 87-HSABP/HYP-3 Zhijun, W., 51-SR-3, 52-SR-4 Zhong, F., 88-HSABP/HYP-4 Zhou, J., 94-PC-8, 115-HSABP/HYP-5, 126-PC-11 Zhou, W., 172-TM-6 Zhu, N., 9-EERE-1 Zhuang, F., 94-PC-8, 126-PC-11 Zhuang, T., 68-EP-9 Ziemba, L., 168-GEPC-1/GTE-19 Ziemer, J., 124-EP-19, 205-EP-32 Zilberter, I., 88-HSABP/HYP-4 Zilliac, G., 80-HR-3, 122-HR-5, 184-HR-7 Zimmerman, J., 184-HR-7 Zirakssaz, M., 43-LP-4 Zmijanovic, V., 70-LP-9

Author/Session Chair Index

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