49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit (JPC) Advancing Propulsion Capabilities in a New Fiscal Reality 14–17 July 2013 San Jose Convention Center 11th International Energy Conversion San Jose, California Engineering Conference (IECEC)

FINAL PROGRAM www.aiaa.org/jpc2013 www.iecec.org #aiaaPropEnergy www.aiaa.org/jpc2013 • www.iecec.org 1 #aiaaPropEnergy GET YOUR CONFERENCE INFO ON THE GO! Download the FREE Conference Mobile App

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The 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC) and the 11th International Energy Conversion Engineering Conference (IECEC) combine this week in San Jose, California to provide the world’s premier forum for presentation, discussion, and collaboration of science, research, and technology in these highly related aerospace fields. It brings together experts from industry, government, and academia on an international level to cover a broad spectrum of issues concerning propulsion and energy in the aerospace industry. The co-location of these events provides attendees with a unique opportunity to expand their knowledge of technological advances of these interrelated disciplines and explore areas of common technical expertise. Contents This week you will: WELCOME 3 EVENT OVERVIEW 4 uuPresent recent advances before a SPECIAL SESSIONS 6 knowledgeable international audience NETWORKING AND SPECIAL EVENTS 10 uuEducate customers and providers on the RECOGNITION EVENTS 11 latest research and product developments CONTINUING EDUCATION COURSES 12 STEM 12 u uLearn about the latest technology and EXPOSITION HALL 14 research in the field from industry experts EXHIBIT GUIDE 15 uuDiscover what lies ahead as senior industry PRESENTATION STAGE 18 leaders discuss their program and business GENERAL INFORMATION 20 challenges during keynote and panel GENERAL INFORMATION 21 sessions SPEAKER AND SESSION CHAIR INFORMATION 22 ITAR RESTRICTED SESSIONS 23 uuNetwork to engage new contacts and ORGANIZING COMMITTEE 24 refresh old ones COMMITTEE MEETINGS 25 uuRecognize significant achievements from PROGRAM AT A GLANCE 26 within the community PROGRAM MATRIX 32 PROGRAM AUTHOR SESSION CHAIR INDEX 54 VENUE MAP – SAN JOSE CONVENTION CENTER 91

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Sunday, 14 July 2013 Monday, 15 July 2013

0700 hrs Networking Coffee and Pastries 0730 hrs in the Exposition Hall

0800 hrs Keynote Address 0830 hrs

0900 hrs Networking Break in the Exposition Hall

0930 hrs Speakers’ Briefing in Session Rooms Exposition Hall Open 1000 hrs

1030 hrs IECEC Technical JPC Technical Sessions Sessions and Panel and Panel Discussions 1100 hrs Discussions

1130 hrs

1200 hrs Networking Luncheon 1230 hrs (tickets required)

1300 hrs Speakers’ Briefing in Session Rooms

1330 hrs

1400 hrs IECEC Technical JPC Technical Sessions Sessions and Panel and Panel Discussions 1430 hrs Discussions Exposition Hall Open 1500 hrs

1530 hrs Networking Break in the Exposition Hall Speakers’ Briefing in Session Rooms 1600 hrs

1630 hrs IECEC Technical JPC Technical Sessions Registration Open Sessions and Panel and Panel Discussions 1700 hrs Discussions

1730 hrs

1800 hrs

Welcome Reception 1830 hrs Speakers’ Briefing in Session Rooms (tickets required) 1900 hrs Tech Museum of Innovation Off-Site 1930 hrs Event Additional Ticket JPC Technical Session 2000 hrs Purchase Required

2030 hrs

www.aiaa.org/jpc2013 • www.iecec.org 4 #aiaaPropEnergy EVENT OVERVIEW

Tuesday, 16 July 2013 Wednesday, 17 July 2013

0700 hrs Networking Coffee and Pastries Networking Coffee and Pastries 0730 hrs in the Exposition Hall in the Exposition Hall

0800 hrs Keynote Addresses Keynote Addresses 0830 hrs

0900 hrs Networking Break in the Exposition Hall Networking Break in the Exposition Hall Speakers’ Briefing in Session Rooms 0930 hrs Speakers’ Briefing in Session Rooms Exposition Hall Open Exposition Hall Open

1000 hrs IECEC Technical JPC Technical Sessions 1030 hrs IECEC Technical Sessions and Panel JPC Technical Sessions and Panel Discussions Sessions and Panel Discussions and Panel Discussions 1100 hrs Discussions

1130 hrs

1200 hrs Lunch on Your Own

1230 hrs IECEC Awards Speakers’ Briefing in Session Rooms JPC Awards Luncheon Luncheon Lunch on Your Own 1300 hrs (tickets required) (tickets required)

1330 hrs

JPC Technical Sessions 1400 hrs Speakers’ Briefing in Session Rooms Speakers’ Briefing in Session Rooms and Panel Discussions 1430 hrs Exposition Hall Open 1500 hrs IECEC Technical Sessions 1530 hrs Networking Break in the Exposition Hall Speakers’ Briefing in Session Rooms JPC Technical Sessions and Panel Discussions 1600 hrs IECEC Technical Sessions and Panel 1630 hrs Discussions

1700 hrs JPC Technical Sessions and Panel Discussions 1730 hrs

1800 hrs

1830 hrs Speakers’ Briefing in Session Rooms

1900 hrs

1930 hrs JPC Technical Sessions 2000 hrs

2030 hrs

www.aiaa.org/jpc2013 • www.iecec.org 5 #aiaaPropEnergy SPECIAL SESSIONS

MONDAY, 15 JULY 1000–1200 hrs 210 F 0800–0900 hrs EXHIBIT HALL 1 International Collaboration in Propulsion Panelists will discuss the effect of the current global environment Keynote Address on the international cooperation efforts in propulsion and space Perspectives on Propulsion Policy, Strategy, Budgets, and flight. Activities for Civil, Commercial, and National Security Space Moderator: John Horack, Vice President, Space Systems, Teledyne Brown Engineering Keynote Speaker: John Olson, Former Assistant Director for Space and Aeronautics, White House Office of Science and Panelists: Technology Policy; Vice President, Space Systems Group, Sierra Charles Smith, Human Exploration & Operations Directorate, Nevada Corporation NASA HQ Jens Lassmann, Vice President, Space Systems, Astrium Mark Lewis, Director, Science and Technology Policy Institute 1000–1200 hrs EXHIBIT HALL 3 Charles Precourt, Vice President and General Manager, Space Evolution of Commercial Space and Future Opportunities Launch Division, Aerospace Group, ATK Julie VanKleek, Vice President, Space Advanced Programs, Commercial space is a rapidly growing sector of the space Aerojet Rocketdyne economy. This panel will present a status of current commercial space efforts and challenges with a look forward to new and evolving opportunities. 1330–1530 hrs EXHIBIT HALL 3 Moderator: James Halsell, Technical Director, Aerospace NASA SLS Development Systems, Dynetics NASA’s Space Launch System (SLS) is America’s new Panelists: exploration-class launch vehicle for missions beyond Earth’s Kent Rominger, Vice President and Program Manager, ATK orbit – taking astronauts where no one has been before, as William Claybaugh, Vice President and Program Manager, ATK well as offering unmatched mass and volume capabilities for John Vilja, Vice President Strategy, Aerojet Rocketdyne science missions. The SLS Program is making maximum use of Todd Mosher, Director, Design and Development, Sierra Nevada existing RS-25 core stage engines and advanced developmental Brett Alexander, Director Business Development, Blue Origin hardware in the form of the five-segment solid rocket booster and the J-2X upper stage engine, with a clear plan for beginning flight operations in 2017. SLS chief engineers will 1000–1200 hrs 230 C share plans and progress, as well as innovations being infused The Future of Military Space Launch and How Affordability into the program, such as modifying the Delta IV kick stage to propel the Orion crew craft to translunar injection. These Will Factor In government and industry partners will discuss how the team Evolved Expendable Launch Vehicle (EELV) is the U.S. Air Force’s is solving development challenges and is on track to deliver a expendable launch system that is intended to assure access to safe, affordable, and sustainable infrastructure asset to support space for U.S. government payloads. Started with the goal of America’s space agenda. making government space launch more affordable and reliable, Moderator: Garry Lyles, Space Launch System (SLS) Chief the program resulted in the development of the Delta IV and Engineer, NASA MSFC Atlas V, which remain the primary methods for launching U.S. military payloads. The panelists, each representing companies Panelists: involved in the EELV program, will discuss how the program has Mat Bevill, SLS Booster Element Deputy Chief Engineer, NASA changed over time as well as present and future challenges, MSFC in particular the continued focus on cost reductions, while the Brian Simmons, SLS Boosters Chief Engineer, ATK program strives to sustain and support America’s space interests. Katherine Van Hooser, SLS Engines Element Chief Engineer, Moderator: Andy Crocker, Propulsion Department Manager, NASA MSFC Dynetics Doug Bradley, RS-25 Chief Engineer, Aerojet Rocketdyne Rene Ortega, SLS Spacecraft and Payload Integration Chief Panelists: Engineer, NASA MSFC Steven Bouley, Vice President, Expendable Launch Systems, Michael Wood, SLS Chief Engineer, The Boeing Company Aerojet Rocketdyne Andrew Jackson, Atlas & Delta Structures Manager, ATK Bill Harding, Director, Program Management, United Launch Alliance Bill Parsons, President and CEO, RD AMROSS, LLC

www.aiaa.org/jpc2013 • www.iecec.org 6 #aiaaPropEnergy SPECIAL SESSIONS

1330–1530 hrs 212 D 1600–1800 hrs 214 Emerging Pathways to Jet Fuel Driving Mission Requirements and Technologies for Space Moderator: Mark Bryden, Program Director, Ames National Transportation – the Next Step after Space Shuttle Laboratory The panel will highlight the overall driving mission requirements Panelists: and technologies required to enable future human spaceflight and discuss recent progress and near-term future plans. Prem Lobo, Associate Director, Center of Excellence for Aerospace Particulate Emissions Reductions Research Moderator: Paul Anderson, Director, Avionics, Orion Program, Corinne Valkenburg, Engineer, Pacific Northwest National Lockheed Martin Space Systems Laboratory Panelists: Shane Flemming, Chief Technical Advisor, Lanzatech Jonathan Trent, Project Scientist Bioengineering, NASA Kent Rominger, Vice President, ATK Space Systems Blake Simmons, Senior Manager, Biomass Program Lead, Michael Wood, Chief Engineer, SLS Program, The Boeing Sandia National Laboratories Company Sam Wiley, Program Director of Human Space, Aerojet Rocketdyne 1330–1530 hrs 211 D Larry Price, Deputy Program Manager, Orion Program, Powering the Next Generation Lockheed Martin Space Systems Todd Mosher, Director of Dream Chaser Design and Mark Lewis, Director, Science and Technology Policy Institute Development, Sierra Nevada (interviewed by Steven Howell, AIAA) Sustaining the Pipeline 1600–1800 hrs EXHIBIT HALL 3 Daniel Kirk, Associate Department Head, Mechanical and Legacy RLV Systems DC-X Aerospace Engineering Department, Florida Institute of Technology (interviewed by Steven Howell, AIAA) The DC-X, or Delta Clipper Experimental, was an unmanned prototype of a reusable single stage to orbit launch vehicle built The topics will include a discussion of policy issues for fostering by McDonnell Douglas for the U.S. Strategic Defense Initiative and attracting the next generation of talented engineers into Organization (SDIO) in the early 1990s. Later, the system was the work force, a national strategy on STEM education, the transferred to NASA and upgraded with advanced operations, engineering pipeline, and other issues related to engineering structures and propulsion technology and was renamed the DC- education. XA. The DC-X was never designed to achieve orbital altitudes or velocity, but instead to demonstrate the concept of vertical takeoff and landing using a revolutionary aircraft-like operations 1600–1830 hrs 212 D approach. This session will discuss the lessons learned from the High Power Electric Vehicles and Energy Storage DC-X program and its applicability to future space transportation systems. The panel will address high power electric vehicles and energy storage. Moderator: Jess Sponable, Program Manager, DARPA Moderators: Panelists: Geoffrey Landis, Research Scientist, NASA Glenn Research Peter Worden, Director, NASA Ames Research Center Center Tom Ingersoll, Chief Executive Officer, Skybox Imaging Edward Lewandowski, Research Engineer, NASA Glenn Joaquin Castro, Director, International Advanced Propulsion Research Center Programs, Aerojet Rocketdyne Stephen Cook, Director of Space Technologies, Dynetics Panelists: Subbarao Surampudi, Program Manager, NASA JPL Tim Collins, Chief Executive Officer, Kleenspeed TUESDAY, 16 JULY Joseph Troutman, Chief Engineer, ABSL Space Products EnerSys Advanced Systems 0800–0900 hrs EXHIBIT HALL 1 Robert Baertsch, Executive Vice President of Software Keynote Address Engineering, SkyTran Eric Lentz-Gauthier, Pilot, Solar Flight Propulsion and Power Systems for the Future Keynote Speaker: Henner Wapenhans, Head of Technology Strategy, Rolls-Royce Group

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0800–0900 hrs 212 A & C John Kusnierek, Director – Business Development, Rolls-Royce North American Technologies, Inc. Keynote Address Nateri Madavan, Deputy Project Scientist, Fixed Wing Project, A New Industrial Revolution for a Sustainable Energy Future NASA Ames Research Center Keynote Speaker: Arun Majumdar, Director of Energy Initiatives, Google 1300–1500 hrs 230 C Access to affordable and reliable energy has been a Dealing with the Changing Aerospace Business Environment: cornerstone of the world’s increasing prosperity and economic A Military Aviation Perspective growth since the beginning of the industrial revolution. Our use of energy in the twenty-first century must also be Alton Romig, VP and General Manager, Skunk Works, Lockheed sustainable. This talk will provide a techno-economic snapshot Martin Corporation (interviewed by Guy Norris, Senior Editor, of the current energy landscape and identify several research Aviation Week) and development opportunities and challenges to create the foundation for this new industrial revolution. 1430–1530 hrs 212A&C Energy Conversion Initiatives at Lockheed Martin 1000–1200 hrs EXHIBIT HALL 3 Energy conversion efforts include storage, generation, and Emerging Technologies for the Next Generation of Aircraft various new and unfamiliar and unclassified concepts. Systems Guest Speaker: Ned Allen, Chief Scientist, Lockheed Martin The panelists will discuss government and industry perspectives Corporation on emerging aircraft systems technologies for the next generation. 1600–1800 hrs EXHIBIT HALL 3 Moderator: David Eames, Director, NASA Programs and Advanced System Studies, Rolls-Royce Corporation DoD Energy Panel Panelists: As the largest federal user of energy, the Department of Defense (DoD) has played the leading role in the advancement of energy Fayette Collier, Project Manager, Environmentally Responsible and propulsion systems and innovations for Terrestrial and Aviation Project, NASA Langley Research Center aerospace applications. More recently, energy considerations Ron Kawai, Propulsion Specialist, Boeing Research and have become a prime focus in military operations, with various Technology initiatives under way in operational energy efficiency (in Kenneth Martin, Manager-Conceptual Design, Lockheed Martin addition to installation energy), renewable energy initiatives, Corporation and energy-based acquisition and lifecycle management. Michael Winter, Chief Engineer for Technology, Pratt & Whitney This special session presents perspectives from the DoD and DoE and is focused on DoD Energy challenges and issues, 1000–1200 hrs 230 C strategy/policy, priorities, initiatives, and opportunities. Dealing with the Changing Aerospace Business Environment: Participants: Department of the Navy, U.S. Air Force, U.S. Army, A Commercial Aviation Perspective Office of the Secretary of Defense, U.S. Department of Energy Jim Peterson, Senior Manager, Aviation Policy, Boeing Speakers include: Commercial Airplanes (interviewed by Guy Norris, Senior Vice Admiral Philip H. Cullom, Deputy Chief of Naval Editor, Aviation Week) Operations for Fleet Readiness and Logistics, U.S. Navy Lieutenant General William M. Faulkner, Deputy Commandant, Installations and Logistics, U.S. Marine Corps 1300–1500 hrs EXHIBIT HALL 3 and others Disruptive Aircraft and Propulsion Technologies for the Future 1600–1800 hrs 210 A The panelists will discuss government and industry perspectives on disruptive technologies that will yield alternative propulsion Propulsion Challenges for Commercial Reusable Space Vehicles cycles in a not distant future. Moderator: Bruce Pittman, NASA Space Portal/Emerging Space Moderator: David Eames, Director, NASA Programs and Office Advanced System Studies, Rolls-Royce Corporation Panelists: Panelists: Frank Zegler, Senior Staff Advanced Programs, ULA Marty Bradley, Technical Fellow, Boeing Research and Technology Tom Mueller, Vice President of Propulsion Development, SpaceX Dale Carlson, General Manager Technology Strategy, GE Tim Pickens, Chief Propulsion Engineer, Moon Express Aviation Greg Mungas, CEO and Founder, Firestar Technologies www.aiaa.org/jpc2013 • www.iecec.org 8 #aiaaPropEnergy SPECIAL SESSIONS

1600–1800 hrs 230 C 0930–1200 hrs 230C Engineering Education in a New Fiscal Reality Public-Private Partnerships to Accelerate Technology Transition Moderator: Daniel Kirk, Associate Department Head, Panel will discuss barriers to effective innovation and technology Mechanical and Aerospace Engineering Department, Florida transition to the aerospace industry as well as potential Institute of Technology pathways to improved technology maturation and transition. Panelists: Moderator: Graham Warwick, Senior Editor – Technology, Scott Hubbard, Professor, Stanford University Aviation Week Gary Kawahara, Vice President and General Manager, ATK Panelists: Commerce Alton Romig, Vice President and General Manager of Skunk Don Jaekle, Owner, PMD Technologies Works® Advanced Development Programs, Lockheed Martin Michael Winter, Chief Engineer for Technology, Pratt & Whitney Corporation Dale Carlson, General Manager, Technology Strategy, GE Aviation WEDNESDAY, 17 JULY Alan Epstein, Vice President, Technology & Environment, Pratt & Whitney 0800–0900 hrs EXHIBIT HALL 1 Mark Anderson, Director, Flight Sciences Technology, Phantom Keynote Address Works, The Boeing Company Jaiwon Shin, Associate Administrator for Aeronautics, NASA Hypersonic Propulsion, Leveraging Today to Deliver Unique Capabilities in the Future 1430–1630 hrs 230 C Keynote Speaker: Mark Lewis, Director, Science and Technology Policy Institute Technology, Education and NASA’s New Asteroid Grand Challenge Guest Speaker: Mason Peck, NASA Chief Technologist 0800–0900 hrs 212 A & C NASA technology and education-focused opportunities in the Keynote Address new fiscal reality will be addressed, along with an overview of Power Generation and Processing Challenges for Near-Term NASA’s new “Protect the Planet Grand Challenge,” which invites worldwide participation with NASA on discovering all the High Power Solar Electric Propulsion asteroid threats to the human population and how to respond, Keynote Speaker: Roger M. Myers, Executive Director, Electric including the role of science and technology research. Propulsion and Integrated Systems, Aerojet Rocketdyne

1430–1730 hrs 230 B 0930–1200 hrs EXHIBIT HALL 3 The Aerospace Industry Coping with the Current Fiscal High Speed Propulsion Development and Implementation Environment Moderator: Mark Lewis, Director, Science and Technology Policy The panelists will provide a senior level perspective and Institute discussion on how the propulsion industry is coping with and Panelists: adjusting to maintain success in the current challenging fiscal environment. John Korte, Research Directorate Chief Engineer for Hypersonics, NASA LaRC Moderator: Sandra Magnus, Executive Director, AIAA John Kusnierek, Director, Business Development, Rolls-Royce Panelists: North American Technologies, Inc. Jaiwon Shin, Gerald (Scott) Cruzen, Vice President, Advanced Design and NASA Associate Administrator for Aeronautics Henner Wapenhans, Technology, Williams International Co., LLC Head of Technology Strategy, Rolls-Royce Curtis Berger, Director, Hypersonic Programs, Aerojet Group Rocketdyne Jim Maser, Vice President for Corporate Strategy and Steven Beckel, Director, Advanced Propulsion Business Development, Gen Corp Development, ATK Dale Carlson, General Manager, Technology Strategy, GE Aviation Ray Johnson, Vice President, Space Launch Operations, The Aerospace Corporation

www.aiaa.org/jpc2013 • www.iecec.org 9 #aiaaPropEnergy NETWORKING AND SPECIAL EVENTS

Welcome Reception NEW! Morning Start the conference off right, by Coffee and connecting with old friends and forging Pastries in the new business relationships from 1800– 1930 hrs Sunday evening during the Exposition Hall welcome reception in the exposition hall. A great way to start the day and interact A ticket for the reception is required, and with conference participants! Coffee is included in the conference registration and pastries will be offered Monday– fee where indicated. Additional tickets Wednesday, 0700–0800 hrs, in Exhibit for guests may be purchased on site as Hall 2. This event is open to all registered available. attendees (no tickets required).

Networking Luncheon Off-Site Reception Networking Breaks Join us in the exposition hall on Monday, Tech Museum of Innovation Stand-alone networking breaks are built 15 July for a networking luncheon at Monday, 15 July into the program to allow even more time 1200 hrs. Engage new contacts and 1830–2100 hrs for exploring the exhibits, continuing refresh old ones, while enjoying a discussions from technical sessions, or reception-style luncheon. A ticket for the Meet with your peers and potential checking emails and voicemails to keep luncheon is included in the conference industry partners and join Lockheed in touch with the office while you are at registration where indicated. Additional Martin Corporation at the Tech Museum the conference. Networking breaks will tickets may be purchased on site as of Innovation. There will be hands-on and be located in the exposition hall during space is available. interactive exhibits plus reception-style food the following times: and cocktails to enjoy. Conveniently located across from the San Jose Convention Center, Monday, 15 July 0900–1000 hrs Young Professional won’t want to miss out on this opportunity. 1530–1600 hrs Networking Reception Tickets are only $25, and include the $15 museum admission fee and reception Tuesday, 16 July 0900–1000 hrs The chairs of the AIAA Young Professional catering. Tickets may be purchased on a 1500–1600 hrs Committee and the AIAA Corporate first-come, first-served basis. Wednesday, 17 July 0900–0930 hrs Member Committee invite all early career Sponsored by: professionals to a networking reception Monday Networking Breaks on Tuesday, 16 July, 1600–1730 hrs, Sponsored by: in the AIAA exposition hall. This is a great opportunity for young professional members of the Institute to meet corporate leaders and other members, and to make new contacts. Join the Young Professional and Corporate Member Committees for food, drinks, and relaxed socializing.

www.aiaa.org/jpc2013 • www.iecec.org 10 #aiaaPropEnergy RECOGNITION EVENTS

Recognizing outstanding achievement in our profession is one of the primary goals of AIAA. Please join us in saluting the accomplishments of your peers as we celebrate aerospace ingenuity and collaboration. A ticket for each luncheon is required, and is included with the appropriate conference registration. Additional tickets may be purchased at the registration desk while supplies last.

IECEC AWARDS LUNCHEON JPC AWARDS LUNCHEON AIAA Electric Propulsion Best Paper AIAA Paper 2012-3789, “Design of a Tuesday, 16 July Wednesday, 17 July Laboratory Hall Thruster with Magnetically 1200–1400 hrs 1200–1400 hrs Shielded Channel Walls, Phase III: Exhibit Hall 1 Exhibit Hall 1 Comparison of Theory with Experiment.” Ioannis Mikellides, Ira Katz, Richard Hofer, and Dan Goebel, NASA Jet Propulsion Luncheon Address AIAA Air Breathing Propulsion Award Laboratory. Woodrow Whitlow, Thomas A. Kaemming AIAA High Speed Air Breathing Propulsion Associate Administrator Research Engineer, Best Paper for Mission Support Innovative Scientific Directorate, NASA AIAA Paper 2012-4263, “Low-Dissipation Solutions, Inc. Advection Schemes Designed for Large Technical Fellow Eddy Simulations of Hypersonic Propulsion (Retired), The Boeing Systems.” Jeffery White, Robert Baurle, NASA AIAA Aerospace Power Systems Award Company Langley Research Center; Travis Fischer, Sandia National Laboratories; Jesse Quinlan, “For outstanding technical contributions, Geoffrey A. Landis National Institute of Aerospace; William creativity, and pioneering research that R&D Engineer Black, Purdue University. greatly contributed to the advancement of NASA Glenn Research pulse detonation engines and high speed air Center breathing propulsion technology.” AIAA Hybrid Rockets Best Paper AIAA Paper 2012-4199, “Development and “For 35 years of developing Testing of the Regeneratively Cooled Multiple advanced photovoltaic AIAA Propellants and Combustion Use Plug Hybrid (for) Nanosats (MUPHyN) power systems for extreme Award Motor.” Shannon Eilers, Stephen Whitmore, space environments; providing leadership, and Zachary Peterson, Utah State University. fostering innovation, interfacing with the public; James F. Driscoll and contributing to an improved scientific Professor of Aerospace AIAA Hybrid Rockets Best Student Paper understanding of operating solar power devices Engineering AIAA Paper 2012-4310, “Design and from the solar corona to the Martian surface University of Michigan and beyond.” Development of a Thrust Vector Controlled “For a distinguished record Paraffin/Nytrox Hybrid Rocket.” Laura AIAA Energy Systems Award of technical contributions to Simurda, Keith Stober, Adrien Boiron, Katrina combustion science and a Rachel Hornstein, Elizabeth Jens, and Alex Ryoichi S. Amano sustained record of service and leadership in Fletcher, Stanford University. Professor the propulsion and combustion community.” AIAA Liquid Propulsion Best Paper University of Wisconsin AIAA Sustained Service Award – Milwaukee AIAA Paper 2012-3867, “Investigation of the API-Injection Concept in a LOX/LH2 “For pioneering work in the Kenneth H. Yu Combustion Chamber at GG/PB Operation fields of computational fluid Associate Professor of Conditions.” Dimitry Suslov and Jan Deeken, dynamics and terrestrial Aerospace Engineering German Aerospace Center (DLR); and Oskar energy with interest in propulsion, turbulence, University of Maryland Haidn, Technical University Munich. and energy systems with successful innovations in research, education, and consulting.” “For sustained service AIAA Nuclear and Future Flight Propulsion and leadership to the AIAA Propellants and Best Paper AIAA Aerospace Power Systems Best Paper Combustion Technical Committee, to many AIAA Paper 2012-3860, “Faster-Than-Light AIAA Paper 2012-3892, “Long-Lived Venus AIAA conferences, and to AIAA publications as Space Warps, Status and Next Step.” Lander Thermal Management System Design.” an author and associate editor of the Journal of Eric Davis, Institute for Advanced Studies Rebecca Hay, Andrew Slippey, Calin Tarau, Propulsion and Power.” at Austin. and William Anderson, Advanced Cooling Technologies. AIAA Air Breathing Propulsion Systems AIAA Propulsion and Combustion Best Paper AIAA Paper 2012-1272, “Influence of Steam AIAA Aerospace Power Systems Best Integration Best Paper Dilution on NOx Formation in Premixed Student Paper AIAA Paper 2012-0275, “Addressing Corner Natural Gas and Hydrogen Flames.” AIAA Paper 2012-4048, “Carbon Nanotube Interactions Generated by Oblique Shock- Sebastian Goke and Christian Paschereit Arrays for Enhanced Thermal Interfaces to Waves In Unswept Right-Angle Corners and Hermann-Fottinger Institute. Thermoelectric Modules.” Kimberly Saviers, Implications for High-Speed Inlets.” Dan Stephen Hodson, and Timothy S. Fisher, Purdue Baruzzini, Daniel Miller, and Neal Domel, AIAA Solid Rockets Best Paper Lockheed Martin Aeronautics Company. University; James R. Salvador, General Motors AIAA Paper 2012-3825, “Theoretical Research and Development Center; and Linda Investigation of Parietal Vortex Shedding in Kasten, Air Force Research Laboratory. Solid Rocket Motors.” Germain Boyer, Gregoire Casalis, and Jean-Luc Estivalezes, ONERA. www.aiaa.org/jpc2013 • www.iecec.org 11 #aiaaPropEnergy CONTINUING EDUCATION COURSES

Liquid Propulsion Systems – Evolution and Missile Propulsion Design and System Engineering Advancements Thursday–Friday, 18–19 July Thursday–Friday, 18–19 July 0815–1700 hrs 0815–1700 hrs Willow Glen Ii, Marriott Hotel Willow Glen II, Marriott Hotel Instructor: Eugene L. Fleeman, International Lecturer on Missiles Instructors: Alan Frankel, Business Development, Moog-ISP, Description: Space and Defense Group; Ivett Leyva, Combustion Devices A system-level, integrated method is provided for the missile Group, AFRL/RZSA; and Patrick Alliot, Senior Technical Expert, propulsion system design, development, analysis, and system Space Engine Division, SNECMA engineering activities in addressing requirements such as Description: cost, performance, risk, and launch platform integration. Liquid propulsion systems are critical to launch vehicle and The methods presented are generally simple closed-form spacecraft performance and mission success. This two- analytical expressions that are physics-based, to provide insight day course, taught by a team of government, industry, and into the primary driving parameters. Sizing examples are international experts, will cover propulsion fundamentals and presented for rocket-powered, ramjet-powered, and turbo-jet topics of interest in launch vehicle and spacecraft propulsion; powered baseline missiles. Typical values of missile propulsion non-toxic propulsion; microsat and cubesat propulsion; parameters and the characteristics of current operational propulsion system design and performance; and human rating missiles are discussed as well as the enabling subsystems of liquid engines. and technologies for missile propulsion and the current and projected state of the art. Videos illustrate missile propulsion development activities and performance. Attendees receive To register for one of these courses, visit the registration desk. course notes.

STEM

Engineers as Educators Leading the STEM Charge: Engineers as Educators Workshop Illuminating the Potential in Train the Trainer Monday, 15 July Aerospace Tuesday, 16 July 1830–2130 hrs Tuesday, 16 July 1500–1600 hrs San Jose Convention Center 1300–1530 hrs San Jose Marriott Sharing your passion for aerospace with San Jose Convention Center Is your region looking for a great way to K–12 students is important – and you Join with high school students, parents, engage in STEM outreach? Is your section never get another chance to make a first and teachers to hear from a panel of ready to inspire students by hosting your impression. This workshop will give you aerospace students and professional own Engineers as Educators workshop for insights into how to approach a classroom members about their entry into the your local professional members? In this talk, a mentoring situation, or an informal aerospace industry. Their educational Train the Trainers workshop, participants interaction with after-school or scouting and work pathways may be very different will learn how to be instructors for our groups. You will learn tips and tricks, as – some very intentional, some driven by Engineers as Educators program, allowing well as low-cost activities to make your circumstances – but all joined together those who are interested in coordinating interactions engaging for both students by a common passion for aerospace. their own section/region Engineers as and teachers. These panelists will give you a different Educators events to learn how. Register Register now at www.aiaa.org/JPC13- perspective of the industry and how many now at https://www.aiaa.org/Train-the- Engineers-as-Educators diverse careers can be captured under the Trainer/. broad perspective of the industry.

For further information, please contact Lisa Bacon at [email protected] www.aiaa.org/jpc2013 • www.iecec.org 12 #aiaaPropEnergy TWO PROUD LEGACIES, ONE BRIGHT FUTURE With more than 130 combined years of experience and leadership in With more than 130 combined years of experience and leadership in rocket propulsion, Aerojet and Rocketdyne are raising the bar. Working rocket propulsion, Aerojet and Rocketdyne are raising the bar. Working as one powerful, united team, we are poised to deliver the innovative, as one powerful, united team, we are poised to deliver the innovative, cutting-edge solutions that will be needed to meet customer needs and cutting-edge solutions that will be needed to meet customer needs and create opportunity. We are committed to doing the hard things that create opportunity. We are committed to doing the hard things that keep us free and expand our horizons. We are Aerojet Rocketdyne. keep us free and expand our horizons. We are Aerojet Rocketdyne.

VISIT US AT ROCKET.COM

Aerojet Rockedyne is proud to support AIAA and the 2013 Joint Propulsion Conference Aerojet Rockedyne is proud to support AIAA and the 2013 Joint Propulsion Conference Visit us @ Booths 504 & 612 Visit us @ Booths 504 & 612 EXPOSITION HALL

The Exposition Hall will host the Welcome Reception on Sunday night and remain open during the following hours throughout the week. Companies will be displaying an array of state-of-the-art technology. The Exposition Hall is the place to network and conduct business for all attendees, as well as attend special presentations featured on the Presentation Stage. HALL 2 Exposition Hours Sunday, 14 July 1800–1930 hrs Welcome Reception (ticket required) Monday, 15 July 0700–1100 hrs Networking Luncheon 1200–1330 hrs (ticket required) PRESENTATION 1330–1600 hrs STAGE Tuesday, 16 July 0700–1100 hrs CYBER CAFÉ 422 521 1200–1600 hrs CORPORATE MEMBER & Wednesday, 17 July 0700–1100 hrs EXHIBITOR 415 418 517 518 617 LOUNGE 616 AIAA 416 515 615 EXPOSITION HALL EVENTS PAVILION 314 413 512 613 612 Sunday, 14 July 611 711 310 409 410 Welcome Reception 1800–1930 hrs 216 315 710 (ticket required) CORPORATE MEMBER SMALL 212 311 504 604 704 Monday, 15 July BUSINESS 304 404 SPOTLIGHT 210 309 Coffee and Pastries 0700–0800 hrs Networking Coffee Break 0900–0930 hrs Networking Luncheon 1200–1330 hrs (ticket required) Networking Coffee Break 1530–1600 hrs ENTRANCE Exhibitors by Booth Number Tuesday, 16 July 210 PBC Aerospace and Defense 504 Aerojet Rocketdyne 212 dSPACE 512 The Boeing Company Coffee and Pastries 0700–0800 hrs 216 Sierra Nevada Corporation 515 Desktop Aeronautics 304 Spincraft Division of Standex 517 NTS – National Technical Systems Networking Coffee Break 0900–0930 hrs International 518 Thales Components Corporation 309 Structural Composites Industries LLC 521 Beta CAE Systems Networking Coffee Break 1500–1600 hrs 310 Marotta Controls, Inc 604 GE Aviation 311 JASC 611 General Dynamics Corporate Member / 1600–1730 hrs 314 Metal Technology 612 Aerojet Rocketdyne Young Professional / 315 Eagle Industries Co., Ltd. 613 Pointwise Exhibitor Reception 404 ATK 615 Cambridge University Press 409 Rolls-Royce 616 VACCO Industries 410 Moog 617 ASME International Gas Turbine Institute Wednesday, 17 July 413 Stanford Mu 704 Cobham 415 Lockheed Martin Corporation 710 University of Southern California Coffee and Pastries 0700–0800 hrs 416 Valcor Engineering Corporation Viterbi School of Engineering 418 Mentor Graphics 711 Wyle Networking Coffee Break 0900–0930 hrs 422 L-3 Electron Technologies, Inc www.aiaa.org/jpc2013 • www.iecec.org 14 #aiaaPropEnergy EXHIBIT GUIDE

Aerojet Rocketdyne Booth 504 Boeing has a long tradition of aerospace innovation. Its broad range of capabilities includes creating new, more efficient members of its commercial 9001 Lurline Avenue airplane family, creating advanced technology solutions for military Chatsworth, CA 91311 customers, and integrating aircraft, defense systems, and warfighters through www.rocket.com • [email protected] network-enabled solutions. Aerojet Rocketdyne is a world-recognized aerospace and defense leader Cambridge University Press Booth 615 providing propulsion and energetics to its space, missile defense, strategic, tactical missile and armaments customers throughout the world. For more 32 Avenue of the Americas information, visit www.rocket.com New York, NY 10013-2473 www.cambridge.org/us/ • [email protected] Aerojet Rocketdyne Booth 612 Cambridge’s publishing in books and journals combines state-of-the-art 2001 Aerojet Road content with the highest standards of scholarship, writing and production. Rancho Cordova, CA 95742 Visit our stand to browse new titles, available at a 20% discount, and to pick www.aerojet.com • [email protected] up sample issues of our journals. Visit our website to see everything we do: www.cambridge.org/us/. Aerojet Rocketdyne is a world-recognized aerospace and defense leader providing propulsion and energetics to its space, missile defense, strategic, Cobham Booth 704 tactical missile and armaments customers throughout the world. For more information, visit www.rocket.com 10 Cobham Drive Orchard Park, NY 14127 ASME International Gas Turbine Institute Booth 617 www.cobham.com • [email protected] 6525 The Corners Parkway, Suite 115 Cobham offers an innovative range of technologies and services to solve Norcross, GA 30092 challenging problems across commercial, defense and security markets, on http://igti.asme.org/ • [email protected] space, air, land, and maritime platforms. Cobham Life Support specializes in high pressure pneumatic controls and actuation for space propulsion, life IGTI provides international forums for the exchange of information related to support systems, electro-explosively actuated devices, restraint systems, and gas turbines and turbomachinery. Upcoming events include: ASME Turbine inflation products. Blade Tip Symposium and Course Week, ASME Organic Rankine Cycle Conference, ASME Gas Turbine India, and ASME Turbo Expo 2014. IGTI Desktop Aeronautics Booth 515 also provides professional development opportunities. 1900 Embarcadero Way ATK Booth 404 Palo Alto, CA 94303 www.desktop.aero • [email protected] 9160 North Highway 83 Founded in 1994, Desktop Aeronautics has grown into a well established Corinne, UT 84307 www.atk.com • [email protected] • [email protected] consulting firm dedicated to advancing the state of the art in aerodynamics and aircraft design. ATK is an aerospace, defense, and commercial products company specializing in solid rocket propulsion systems with extensive experience We have significant experience and recognized expertise in aerodynamics, supporting human and space payload missions; small and micro-satellites, aircraft design, computational fluid dynamics, and multidisciplinary components, and subsystems; and lightweight and reliable composite aircraft optimization. We have worked with leading aerospace organizations on structures. ATK has operations in 22 states, Puerto Rico, and internationally. some of the most difficult challenges in aerospace industry. Beta CAE Systems Booth 521 dSPACE Booth 212 29800 Middlebelt Road, Suite 100 50131 Pontiac Trail Farmington Hills, MI 48334 Wixom, MI 48393 www.ansa-usa.com • [email protected] • [email protected] www.dspaceinc.com • [email protected]

BETA CAE Systems is an engineering services company that distributes and dSPACE is the world’s leading provider of hardware and software tools for supports the industry leading ANSA and META software. developing and testing sophisticated electronic control systems. For over 20 years, dSPACE’s high-quality, off-the-shelf software and hardware tools ANSA is a CAE pre-processing tool for FE and CFD analysis, for full-model have empowered engineers to design and innovate, while dramatically build, from CAD to solver input file, in one integrated environment. META is reducing development times and cost. dSPACE’s pioneering products − such a post-processor for analyzing results from ANSYS, NASTRAN, ABAQUS, as the automatic production code generator TargetLink, MicroAutoBox LS-DYNA, PAMCRASH, RADIOSS, MADYMO, and other solvers. rapid prototyping systems, and hardware-in-the-loop (HIL) simulators − have become defacto standards for developing electronics in the automotive sector. They are also heavily relied upon by the aerospace, defense, The Boeing Company Booth 512 commercial vehicle / off-highway, academic, research, and other industries. 6861 Sperryville Lane Learn more by visiting: www.dspaceinc.com. Moorpark, CA 93021 www.boeing.com • [email protected] Eagle Industries Co., Ltd. Booth 315 1731 Technology Drive, Suite 760 Boeing is the world’s largest aerospace company and leading manufacturer of commercial jetliners and defense, space and security systems. A top U.S. San Jose, CA 95110 exporter, the company supports airlines and U.S. and allied government www.ekk.co.jp/eng/ customers in 150 countries. Boeing products and services include commercial and military aircraft, satellites, weapons, C4ISR, electronic and defense EKK is a world-class mechanical seals maker. We research, develop, and systems, launch systems, and performance-based logistics and training. manufacture an extensive range of applications. From Dynamic Seals for Aero engines that meet specific requirements, to Static Metal Seals designed to solve leakage problems. Our Brush Seal products are used in various gas and steam turbines applications. www.aiaa.org/jpc2013 • www.iecec.org 15 #aiaaPropEnergy EXHIBIT GUIDE

General Dynamics Booth 611 Mentor Graphics Booth 418 4300 Industrial Avenue – Mechanical Analysis Division Lincoln, NE 68504 8005 S Boeckman Road www.gdatp.com • [email protected] Wilsonville, OR 97070 www.mentor.com/mechanical • [email protected] General Dynamics Armament and Technical Products, located in Charlotte, NC, provides a broad range of system solutions for military and commercial Mentor Graphics – Mechanical Analysis Division provides 1D and 3D fluid applications. The Lincoln, NE facility develops and produces composite: dynamics software for shortened development. Applications served: Fuel, air, rocket motor cases, overwrapped pressure vessels, launch tubes and fuel gas, and cooling systems internal flow simulation with Flowmaster; 3D fluid tanks. flow and thermal analysis integrated with mechanical design via FloEFD, fully CAD embedded CFD; electronics and avionics cooling with FloTHERM. GE Aviation Booth 604 One Neumann Way, MD G414 Metal Technology Booth 314 Cincinnati, OH 45215 173 Queen Avenue SE www.ge.com/aviation • [email protected] Albandy, OR 97322 www.mtialbany.com • [email protected] GE Aviation, an operating unit of GE (NYSE: GE), is a world-leading provider of jet, turboprop, and turboshaft engines, components, and With more than forty years of experience, Metal Technology leads the way integrated systems for commercial, military, business, and general aviation in the precision machining, forming, and forging of exotic matals. MTI aircraft. GE Aviation has a global service network to support these offerings. works with materials usch as Tatalum, Niobium, Titanium, Molybdenum, For more information, visit us at www.ge.com/aviation. Follow GE Aviation Tungsten, and their alloys. MTI is ISO9001 registered and supplies precission on Twitter at http://twitter.com/GEAviation and YouTube at http://www. components to aerospace, defense, medical, and scientific markets. youtube.com/user/GEAviation. JASC Booth 311 Moog Booth 410 300 Jamison Road, Plant 20 2303 W. Alameda Drive East Aurora, NY 14052 Tempe, AZ 85286 www.moog.com/space • [email protected] www.jasc-controls.com • [email protected] Moog supplies critical components, subsystems and systems for access to and The JASC Corporation specializes in the design and production of high- operation in space, including: thrust vector control, flight control actuators, reliability components for pneumatic, hydraulic, and fuel systems. Since electronic controllers, avionics, payload electronics, fluid control systems, its inception in 1990, JASC has been providing fluid control solutions and propulsion components, subsystems and systems, antenna and solar array advanced products for the aircraft, spacecraft, and power generation positioners, reaction wheels, vibration isolation, and electronic assemblies for industries. satellites. L-3 Electron Technologies, Inc Booth 422 NTS – National Technical Systems Booth 517 3100 W Lominta Boulevard 24007 Ventura Boulevard Torrance, CA 90505 Calabasas, CA 91302 www.L-3com.com/eti • [email protected] www.nts.com • [email protected]

L-3 Electron Technologies, Inc. (ETI) is a leading provider of electric We are a diversified engineering services company, providing a wide range propulsion systems for both commercial and scientific spacecraft. ETI has of product design consulting services, testing and certifications, and supply delivered 13cm and 25cm Xenon Ion Propulsion Systems or XIPS®. ETI also ® chain management solutions. Our clients see us as an extension of their own delviered the 30cm XIPS for NASA’s Deep Space 1 and DAWN spacecraft. engineering teams, filling in their internal gaps and providing the expertise ETI has developed an 8cm xenon thruster for small sat application. required to build better, stronger, safer, more reliable products and bring those products to market quickly and efficiently. With the largest network Lockheed Martin Corporation Booth 415 of test laboratories and engineering service centers in North America and over 50 years of experience to draw from, NTS is prepared to meet any 1011 Lockheed Way challenge. Palmdale, CA 93559 www.lockheedmartin.com • [email protected] Pointwise Booth 613 Lockheed Martin is a global security and aerospace company principally 213 South Jennings Avenue engaged in the design, development, and integration of advanced Fort Worth, TX 76104 technology systems to include cutting-edge propulsion and thermal protection www.pointwise.com • [email protected] solutions to enable extremely high speed, precision performance. Pointwise, Inc. is solving the top problem facing engineering analysts today: Marotta Controls, Inc Booth 310 mesh generation for computational fluid dynamics. Manufacturing firms and research organizations use Pointwise’s mesh generation software to 78 Boonton Avenue seamlessly bridge the gap between CAD and computational fluid dynamics Montville, NJ 07045 analysis. www.marotta.com • [email protected]

Our fluid control components and subsystems play a vital role in pressurization systems, thruster controls, reaction/attitude control systems and propulsion systems for commercial and military applications. Using our deep base of flight-qualified designs, our engineers can specify a previously qualified design or develop a modified design with extensive heritage at the component level. www.aiaa.org/jpc2013 • www.iecec.org 16 #aiaaPropEnergy EXHIBIT GUIDE

PCB Aerospace and Defense Booth 210 Structural Composites Industries LLC Booth 309 3425 Walden Avenue 336 Enterprise Place Depew, NY 14043 Pomona, CA 91768 www.pcb.com • [email protected] www.SCIcomposites.com • [email protected]

PCB Aerospace and Defense specializes in products and programs Manufacturer of composite wound pressure vessels and composite structures. developed exclusively for the aerospace, civil and military aviation, defense, homeland security, and test and measurement markets. Product focus includes MEMS high-G piezoresistive shock accelerometers, acoustic microphones, Thales Components Corporation Booth 518 fatigue rated load cells, and piezoelectric sensors for measuring vibration, 40G Commerce Way pressure, and force. For more information visit www.pcb.com/aerospace. Totowa, NJ 07512 www.thalesgroup.com • [email protected] Rolls-Royce Booth 409 The Thales ion propulsion system, based on HEMPT 3050 (High Efficiency 2001 South Tibbs Avenue Multistage Plasma Thruster), is capable of addressing station-keeping and Indianapolis, IN 46241 orbit-topping. This innovative and modular solution, based on proven in-orbit www.Rolls-Royce.com • [email protected] technologies and processes, meets the needs of all types of missions, from scientific projects to large GEO Comsats. 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 VACCO Industries Booth 616 fuel burn in advanced propulsion and power technologies and systems. 10350 Vacco Street Emphasis areas include highly efficient subsonic, supersonic and high Mach South El Monte, CA 91733 turbine propulsion systems, highly integrated inlet and exhaust systems, and www.vacco.com • [email protected] innovative integrated power and thermal management systems. As your partner in propulsion, VACCO specializes in design and production Sierra Nevada Corporation Booth 216 of engineered fluid controls for human-rated, long duration and expendable space applications. Proven Valves, Regulators, Filters, Couplings, Refueling 1722 Boxelder Street Mechanisms, Welded Manifolds, and highly integrated ChEMS™ Modules Louisville, CO 80027 are available for applications ranging from cryogenic to high pressure and www.sncorp.com • [email protected] Space Systems hazardous propellants.

Sierra Nevada Corporation’s Space Systems business area, headquartered in Louisville, Colorado, designs and manufactures advanced spacecraft, Valcor Engineering Corporation Booth 416 space vehicles, rocket motors and spacecraft subsystems and components 2 Lawrence Road ® for the U.S. government and commercial customers, as well as for the Springfield, NJ 07081 VALCOR international market. SNC Space Systems has more than 25 years of space www.valcor.com • [email protected] heritage in space and has participated in over 400 successful space missions through the delivery of over 4,000 systems and subsystems and components. Valcor Aerospace specializes in the design and manufacture of custom During its history, SNC Space Systems has concluded over 70 programs for valves and control components (solenoid, relief, check, fill and drain valves, NASA and over 50 other clients. pressure regulators, actuators) for liquids (propellants, fuel, hydraulic fluid) and gases in critical aerospace (aircraft, launch vehicle, missile, spacecraft, Spincraft Division of Standex International Booth 304 etc.) applications. 500 Iron Horse Park N. Billerica, MA 01862 University of Southern California www.spincraft.net • [email protected] Viterbi School of Engineering Booth 710

Long recognized as experts in high-performance metal forming technology, 3650 McClintock Avenue OHE 106 Spincraft delivers single-source manufacturing solutions for complex Los Angeles, CA 90089 aerospace challenges. Proven fabrication and assembly capabilities include: http://viterbi.usc.edu/gapp • [email protected] launch vehicle fuel-tank domes, LH2 tank assemblies, titanium propellant tanks, combustion chamber liners, single-piece engine nozzles, and more. The USC Viterbi School of Engineering offers 40+ graduate programs Expertise in virtually all workable alloys. entirely online through the Distance Education Network (DEN@Viterbi). The Viterbi School’s state-of-the-art, proprietary Web-based delivery system enables students from around the world to access classes live, on demand or Stanford Mu Booth 413 by download. 20725 Annalee Avenue Carson, CA 90746-3503 TM Wyle Booth 711 www.stanfordmu.com • [email protected] 128 Maryland Street An internationally recognized leader in the design, development and El Segundo, CA 90245 production of propulsion systems and other fluid control components www.wyle.com • [email protected] for satellites, spacecraft, and space vehicles. Space Components is ISO9001:2008 and AS9100:0029 Rev. C Certified and has delivered Wyle’s San Bernardino, California operations serves as a test facility for over 800 regulators, of which 312 have successfully flown; the balance are rocket engine development and qualifications services. Wyle provides high awaiting launch. 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.

www.aiaa.org/jpc2013 • www.iecec.org The Contents of this Package are Stanford Mu Corporation Confidential.17 #aiaaPropEnergy PRESENTATION STAGE

Monday, 14 July 0945–1000 hrs MOOG (BOOTH #410) 0900–0915 hrs PCB AEROSPACE AND DEFENSE (BOOTH #210) An Update to Moog’s Space Business Rocket Motor Combustion Instability Sensors Chris McCormick, Space Sector Vice President, Moog Space Bob Metz, Manager for Aerospace & Defense and Defense Group Dynamic ICP Pressure Sensors for Detection of Combustion Moog’s Space Sector has changed over the last two years Instability and High Intensity Acoustics in Rocket Motor with additions from Bradford Engineering B.V., AMPAC’s In- Research. Space Propulsion business, and most recently, Broad Reach Engineering. With the addition of these companies, Moog now Bob Metz holds a B.S. in aeronautical and astronautical has greater capabilities and a larger footprint around the world. engineering from The Ohio State University and an MBA from Chris McCormick will introduce himself and give an update on State University of New York. He has been an instrumentation Moog’s Space Sector. engineer for 17 years, focusing on vibration, pressure and force measurement using piezoelectric sensors and is currently a Product Manager for the Aerospace & Defense Division of PCB 1230–1245 hrs MENTOR GRAPHICS (BOOTH #418) Piezotronics, Inc. Enhancing Fluid System Design Time with 1D & 3D Computational Fluid Dynamics 0915–0930 hrs dSPACE (BOOTH #213) Peter Doughty, Marketing Programs Manager – US, Mentor Tools for Embedded Software Development and Validation Graphics Mechanical Analysis Division Marcus Lites Mentor Graphics Corporation provides Computational Fluid The presentation will describe dSPACE tool-chain for model- Dynamics (CFD) aimed at shortening development. This based design, development and testing of embedded software. presentation introduces how aerospace fluid system design dSPACE tools for Rapid Controls Prototyping including solutions teams, e.g fuel, air or oxygen supply systems, can benefit from for simulation of aerospace communication busses, automatic component to system level simulation using 3D CAD-Embedded code generation tool for efficient code, and Hardware-In-the- CFD in close conjunction with 1D system level network flow Loop test systems for closed loop simulation and testing of analysis. aerospace systems will be presented. The presentation will include examples of successful applications currently in flight developed using dSPACE systems. Tuesday, 15 July 1500–1515 hrs VACCO INDUSTRIES (BOOTH #616) 0930–0945 hrs BETA CAE SYSTEMS USA, INC. (BOOTH #521) Non-Pyro Positive Isolation Valve Description ANSA and MetaPost for Advanced Pre- and Post-Processing Joe Cardin Pravin Peddiraju, Senior Software Support Engineer While traditional Pyro Valves actuate via squib charges, VACCO Beta CAE System’s flagship products ANSA and MetaPost are Industries offers a non-pyro alternative – the Positive Isolatoin Valve one of the leading pre- and post-processing software solutions in (PIV). This presentation is an overview of the characteristics and the CAE market, widely used in industries such as automotive, benefits of VACCO’s new normally closed PIV. motor sports, aerospace, marine, and bio-medical. ANSA and MetaPost are multidisciplinary tools with numerous functionalities integrated seamlessly in a single environment, facilitating efficient pre- and post- processing without the need of additional software.

www.aiaa.org/jpc2013 • www.iecec.org 18 #aiaaPropEnergy THANK YOU TO OUR 2013 SPONSORS

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GENERAL INFORMATION

AIAA Registration and Cyber Café (Internet Access) Wireless Access Information Center Hours There will be computers with Hotspots will be available at the San The AIAA Registration and Information complimentary Internet access in the Jose Convention Center concourse level. Center will be located in the Exhibit Hall Exposition Hall for conference attendees Look for the Internet Access Signs and Foyer. Hours are as follows: during the following hours: seating areas. Sunday, 14 July 1500–1900 hrs Sunday, 14 July 1800–1930 hrs Wireless Networks: Joint Propulsion2013-G Monday, 15 July 0700–1800 hrs Monday, 15 July 0700–1800 hrs Joint Propulsion2013-A Tuesday, 16 July 0700–1800 hrs Tuesday, 16 July 0700–1800 hrs Wednesday, 17 July 0700–1700 hrs Wednesday, 17 July 0700–1430 hrs

Conference Proceedings International Traffic in Arms Young Professional Guide for Proceedings for these conferences will be Regulations (ITAR) Gaining Management Support available in online proceedings format. AIAA speakers and attendees are Young professionals have the unique The cost is included in the registration fee reminded that some topics discussed opportunity to meet and learn from where indicated. The online proceedings in the conference could be controlled some of the most important people in will be available on 15 July 2013. by the International Traffic in Arms the business by attending conferences Attendees who registered in advance Regulations (ITAR). U.S. nationals (U.S. and participating in AIAA activities. A for the online proceedings have been citizens and permanent residents) are detailed online guide, published by the provided with instructions on how to responsible for ensuring that technical AIAA Young Professional Committee, is access them. Those registering on site will data they present in open sessions to available to help you gain support and be provided with instructions at that time. non-U.S. nationals in attendance or in financial backing from your company. conference proceedings are not export The guide explains the benefits of Restrictions restricted by the ITAR. U.S. nationals are participation, offers recommendations likewise responsible for ensuring that and provides an example letter for Video or audio recording of sessions they do not discuss ITAR export-restricted seeking management support and or technical exhibits, as well as the information with non-U.S. nationals in funding, and shows you how to get the unauthorized sale of AIAA-copyrighted attendance. most out of your participation. The online material, is prohibited. guide can be found on the AIAA website at www.aiaa.org/YPGuide.

AIAA PAVILION Missile Design and System Engineering Author Signing Monday, 15 July 0900–0930 hrs Meet Missile Design and System Engineering author Eugene L. Fleeman at the AIAA Pavilion in the Exhibit 30% Off All AIAA Books at JPC Hall on Monday, 15 July 0900–0930 hrs. AIAA is offering a special show collection at their special month Speak with the author and have your discount on all titles featured at JPC prices. In addition, the title Propulsion copy of Missile Design and 2013. Attendees receive a 30% Techniques: Action and Reaction, by System Engineering signed. discount off the list price of all books Peter Turchi, has been selected as the Missile Design and System for sale in the AIAA Pavilion. This conference book of JPC and is on sale Engineering will be on sale special offer will only be available for $49.95. Take advantage of these for $80.47 (list $114.95) during JPC. Also featured will be the super savings and visit the bookstore in at the AIAA Pavilion. entire 2013 AIAA Book of Month the AIAA Pavilion. www.aiaa.org/jpc2013 • www.iecec.org 20 #aiaaPropEnergy GENERAL INFORMATION

INFORMATION FOR THOSE REGISTERED FOR TECHNICAL TOURS Messages and Information Messages will be recorded and posted NASA Ames Research Center Lockheed Martin on a bulletin board in the registration area. It is not possible to page attendees. Tuesday, 16 July Wednesday, 17 July 1215–1800 hrs 1415–1830 hrs Bus transportation from and back to Participants Nondiscriminatory Practices the San Jose Convention Center will be must bring valid AIAA accepts registrations without provided. All participants should be in U.S. passport or regard to race, creed, gender, color, the foyer and ready to board the bus at birth certificate sexual orientation, physical handicap, 1215 hrs. (not a copy) to and national or ethnic origin. Tour participants should wear be presented at comfortable shoes since the tours will the Lockheed Control Center. require walking and stair climbing. AIAA Membership Closed toe High-heeled shoes are not allowed. AIAA is your vital lifelong link to the Cameras are allowed in some areas. shoes only, no bare legs, collective creativity and brainpower Participants must be U.S. citizens and no electronics of the aerospace profession, and will need to present a driver’s license allowed. a champion for its achievements – or other form of identification with a and nonmembers who pay the full picture ID. nonmember registration fee will receive Bus leaves from the Convention Center at the start times listed above. their first year’s AIAA membership at no No Tour Sign-Up Available On Site. additional cost!

Certificate of Attendance Certificates of Attendance are available for attendees who request documentation at the conference itself. Please request your copy at the on-site registration desk. AIAA is the largest aerospace AIAA offers this service to better serve professional society in the world, the needs of the professional community. serving a diverse range of more than Claims of hours or applicability toward 35,000 individual and corporate professional education requirements are members from 80 countries, who Airplane Contest the responsibility of the participant. are all part of an innovative, high- value profession that helps make the Come fly with us! AIAA will be hosting a world safer, more connected, more paper airplane contest on Wednesday, Employment Opportunities accessible, and more prosperous. 17 July at 0900 hrs in the exposition AIAA serves as the high-energy AIAA assists members who are searching hall. Build your paper airplane using the voice for this vital profession, and for employment by providing a bulletin template provided or create your own provides its members the kind of board at technical meetings. This bulletin unique design. Fly your plane towards a lifelong community, connections, and board is solely for “open position” and specified target for the chance to win free development opportunities that lead “available for employment” postings. registration to the AIAA Propulsion and to a thriving profession and enduring Employers are encouraged to have Energy 2014 event in Cleveland, Ohio! contributions to society. Contest details and rules will be provided personnel who are attending an AIAA on-site prior to the competition. Sign up at technical conferences bring “open American Institute of the registration desk; space is limited! position” job postings. Individual Aeronautics and Astronautics AIAA members may post “available 1801 Alexander Bell Drive for employment” notices. AIAA cannot Suite 500 Chance to Win a Free P&E assume responsibility for notices Reston, VA 20191-4344 Forum Registration forwarded to AIAA Headquarters. AIAA 703.264.7500 or reserves the right to remove inappropriate 800.639.AIAA (2422) Take a few minutes on Wednesday notices. AIAA members can post and Fax: 703.264.7657 to evaluate the conference, and let us browse resumes, browse job listings, and [email protected] know topics and speakers you’d like to access other online employment resources www.aiaa.org see at future events. Complete the brief by visiting the AIAA Career Center at online survey at the registration desk to http://careercenter.aiaa.org. be entered to win. www.aiaa.org/jpc2013 • www.iecec.org 21 #aiaaPropEnergy SPEAKER AND SESSION CHAIR INFORMATION

NEW! Speakers’ Briefings in Speakers’ Practice Room “No Paper, No Podium” and Session Rooms Speakers who wish to practice their “No Podium, No Paper” Policies Authors who are presenting papers, presentations may do so in Room 233 If a written paper is not submitted by the session chairs, and co-chairs will meet at the San Jose Convention Center. A final manuscript deadline, authors will for a short briefing in their session rooms sign-up sheet will be posted on the door. not be permitted to present the paper on the day of their sessions to exchange In consideration of others, please limit at the conference. Also, if the paper bios and review final details prior to the practice time to 30-minute increments. is not presented at the conference, it session. Morning sessions and afternoon will be withdrawn from the conference sessions will meet separately 30 minutes Audiovisual proceedings. It is the responsibility prior to the session start time. Please of those authors whose papers or attend on the day of your session(s). Each session room will be preset with presentations are accepted to ensure that Laptops pre-loaded with the Speakers’ the following: one LCD projector, one a representative attends the conference Briefing preparation slides will be screen, one microphone and sound to present the paper. These policies are provided in each session room. system (if necessitated by room size), intended to improve the quality of the and one laser pointer. This year, laptop conference for attendees. Session Chair Reports computers will also be provided. You may also use your own computer. Please Journal Publication All session chairs are asked to complete note that AIAA does not provide security a session chair report to evaluate their in the session rooms and recommends Authors of appropriate papers are session for future planning. AIAA has that items of value not be left unattended. encouraged to submit them for possible partnered with Canvas Solutions to Any additional audiovisual requirements, publication in one of the Institute’s provide an electronic Session Chair or equipment not requested by 3 July archival journals: AIAA Journal; Journal Report form. You can download the FREE 2013 will be at cost to the presenter. of Aircraft; Journal of Guidance, Control, mobile app in your App Store, AppWorld, For additional A/V equipment, please and Dynamics; Journal of Propulsion or Marketplace by searching for “Canvas email Joanne Zook at joannez@aiaa. and Power; Journal of Spacecraft and Solutions, Inc.” The mobile app is free, so org. Please note that all requests must Rockets; Journal of Thermophysics and please make sure to download it. Detailed be in writing and must include the paper Heat Transfer; or Journal of Aerospace instructions will be provided in the session number and the session number. Information Systems (formerly Journal rooms. If you do not have a tablet or a of Aerospace Computing, Information, smartphone, you may enter your session and Communication). You may now chair report information on the computers submit your paper online at http:// in the Cyber Café. The Canvas app mc.manuscriptcentral.com/aiaa. will be preloaded on all Cyber Café computers. Report data is collected and used for future planning purposes, including best paper awards, session topics and room allocations. Please submit your session chair report electronically by 25 July 2013.

www.aiaa.org/jpc2013 • www.iecec.org 22 #aiaaPropEnergy ITAR RESTRICTED SESSIONS

New for This Year Important session information for all attendees presenting or attending ITAR-restricted sessions On Tuesday and Wednesday a limited number of papers will be presented AIAA Restricted Papers – ITAR-Restricted Regulations Session Admittance Policy in “U.S.-Only” technical sessions. Several papers scheduled to be presented at this conference will be restricted papers In addition to your JPC/IECEC governed by ITAR (the U.S. International Traffic in Arms Regulations). If you plan to conference registration, a separate attend any presentations restricted by ITAR, you must bring proof of citizenship PLUS the registration process will be required to other verification documents as shown below. Please note that only U.S. Citizens and attend these restricted sessions. Please U.S. Resident Aliens can be considered for attendance at these restricted presentations. see the detailed information on the Admittance to restricted sessions and access to restricted technical papers is implemented and controlled by ITAR. ITAR Registration Grid to determine your individual requirements. All restricted session attendees (including speakers and session chairs for these sessions) MUST abide by the procedures and submittal of verification documents as noted below – NO EXCEPTIONS: Access to ITAR Sessions: Presenting a Paper, Chairing a ATTENDEE IDENTIFICATION and PROOF OF EMPLOYMENT REQUIREMENTS Session, or Attending an ITAR- CLASSIFICATION U.S. Government 1. Proof of U.S. Citizenship (for example, passport, birth certificate, Restricted Presentation Employees voters registration card, naturalization papers), AND Admittance to the restricted Technical 2. Personal photographic identification: U.S. Government/Military Papers is controlled by the U.S. Photo ID badge, such as CAC card International Traffic in Arms Regulations U.S. Citizens 1. Proof of U.S. Citizenship (for example, passport, birth certificate, (ITAR). All attendees, presenters, and voters registration card, naturalization papers), AND session chairs will need to register for the conference, and then visit the ITAR 2. Personal photographic identification (passport, driver’s license, Registration Desk to complete additional etc.), AND registration procedures. Anyone wishing 3. Certification credentials based on DD Form 2345 (see below for to enter the restricted session room MUST details) abide by the procedures and submittal of Resident Aliens 1. Resident Alien Card, AND verification documents mandated by the (U.S.) DOD in order to attend, present, or chair 2. Personal photographic identification (passport, driver’s license, ITAR-restricted sessions. No Exceptions! etc.), AND 3. Certification credentials based on DD Form 2345 (see below for Availability of Manuscripts from details)

ITAR Restricted Sessions DD Form 2345 individual certification credentials (required for U.S. and Resident Aliens) A DVD containing the manuscripts from MUST be from one of the following: the ITAR sessions will be available for 1. Copy of an approved and active DD2345 for the individual, OR purchase on site in San Jose by those 2. Copy of an approved and active DD2345 for the individual’s employer PLUS evidence who are registered to attend the ITAR of current employment status with that employer (corporate ID, business card, etc.), OR Sessions, for $25. There will be no sale or distribution of these papers after the 3. A listing of the individual’s employer in the most recent DoD quarterly Qualified event. U.S. Contractor List PLUS evidence of current employment status with that employer (corporate ID, business card, etc.). ITAR Electronics Policy DD Form 2345 may be downloaded and completed online in order to apply for approval to be listed on the Qualified U.S. Contractor List, www.dlis.dla.mil/jcp. Allow at least 4–6 No phones, computers (other than weeks (or longer) PRIOR to the AIAA technical conference dates for you to receive the for the presenter), iPads, cameras, or approval and be listed on the Qualified U.S. Contractor List. other electronic devices with cameras, recording, or two-way communication How to get your ITAR Badge: capabilities will be permitted into Bring all of the above listed identification, proof of employment and certification credentials the ITAR session room. There will be to the AIAA ITAR Registration Desk in the AIAA Registration area. Your documents will be verified and you will be provided with an ITAR Badge. Photo ID will be checked against your a check-in desk in front of the room ITAR badge before admittance is granted to any ITAR presentation. where you can check these devices during the time you are in the sessions. Please be advised that all policies and procedures MUST be followed or admittance to restricted sessions will not be permitted. www.aiaa.org/jpc2013 • www.iecec.org 23 #aiaaPropEnergy ORGANIZING COMMITTEE

AIAA/ASME/SAE/ASEE JOINT PROPULSION CONFERENCE

Executive Chair General Chair Technical Program Chair Technical Program Jim Maser, Gen-Corp Joaquin Castro, Aerojet Claude Russell Joyner, Aerojet Deputy Chair Rocketdyne Rocketdyne Monica Jacinto, Aerojet Rocketdyne Topic Area Organizers

Academic Gas Turbine Engine ITAR Social Media Daniel Robert Kirk, Florida Janet Covery, General Electric Doug Shafer, General Electric Greg Johnston, Infotech Institute of Technology Jimmy Tai, Georgia Institute of Enterprises America Technology Liquid Rocket Propulsion Advanced Propulsion Concepts Silvio Chianese, Space Solid Rocket Propulsion for Future Flight Green Engineering Exploration Technologies C.W. Rousseau, Denel (Pty) Ltd John Robinson, The Boeing Dyna Benchergui, Bombardier Rob Black, Aerojet Rocketdyne Company (Retired) Richard Wahls, NASA Military Commercial Space Steve Cook, Dynetics Space Transportation Air Breathing Propulsion High Speed Air Breathing Miroslav Sir, The Aerospace Systems Integration Propulsion Nuclear and Future Flight Corporation Bruce McKay, Virgin Galactic Faure Joel Malo-Molina, USAF, Propulsion AFRL/RBAC Greg Meholic, The Aerospace Systems Concepts and Commercial and Military Corporation Supporting Propulsion Aircraft Systems Hybrid Rocket Propulsion Technologies David Eames, Rolls-Royce Madhan Bala, Space Propellants and Combustion James Chenoweth, Craft-tech Propulsion Group, Inc. Thomas Jackson, Center Al Reisz, Reisz Engineering Electric Propulsion for Simulation of Advanced Paulo Lozano, Massachusetts Hypersonic and Combined Rockets Institute of Technology Cycle Propulsion Application Tim O’Brien, Aerojet Propulsion Education Energetic Components and Rocketdyne Robert Frederick Jr., UAH Systems Propulsion Research Center Jim Baglini, Exodynamics Hypersonics Technology, Inc. Rich Mutzman, Air Force Public Policy Research Laboratory Carol Cash, Carol Cash & Associates, LLC

INTERNATIONAL ENERGY CONVERSION ENGINEERING CONFERENCE

General Chair Deputy General Chair Technical Program Chair Ashwani Gupta, University Michael Choi, NASA Goddard Kenneth Mark Bryden, Iowa of Maryland Space Flight Center State University

Topic Area Organizers

Aerospace Power Systems Energy Storage Technology Terrestrial Energy-Efficient and Terrestrial Nuclear Energy Mark Liffring, Boeing Richard Shaw, Lockheed Renewable Energy Systems Systems Commercial Airplanes Martin Corporation Nessreen Ghaddar, American Pavel Tsvetkov, Texas A&M Abbas Salim, Lockheed Martin University of Beirut University Space Systems Company Terrestrial Electricity Delivery Essam Khalil, Cairo University (retired) and Grid Reliability David Muth, Idaho National Thermal Management Scott Duncan, Aerospace Laboratory Technology Energy Conversion Device Systems Design Laboratory Michael Choi, NASA Goddard Technology Georgia Tech Terrestrial Fossil Energy Space Flight Center Edward Lewandowski, NASA Systems Glenn Research Center Bhupendra Khandelwal, Cranfield University Ashan Choudhuri, University of Texas El Paso www.aiaa.org/jpc2013 • www.iecec.org 24 #aiaaPropEnergy COMMITTEE MEETINGS

All meetings are scheduled in the San Jose Marriott unless otherwise indicated.

Sunday, 14 July Tuesday, 16 July 1400–1600 hrs TAC P&E Strategy Meeting CC: 211 C 0800–2200 hrs Moog Meeting Room CC: 232 1600–1700 hrs SRTC Awards and CC: 211 A 0900–1000 hrs ABPTCs Conference Blossom Hill 1 Communications Subcommittees Subcommittees 1600–1700 hrs SRTC Education and History CC: 211 B 1100–1200 hrs Pressure Gain Combustion Salon I & II Subcommittees Working Group 1600–1900 hrs TAC Propulsion and Energy CC: 211 D 1430–1600 hrs 2014 Propulsion and Energy Salon I & II Group Meeting Forum Technical Program Committee Meeting 1630–1730 hrs ABP New Member Orientation CC: 211 C 1500–1600 hrs ABPTCs PAW Committee Blossom Hill 1 Monday, 15 July 1730–1830 hrs ABP WGs (Dinner Meeting Prep) Salon V & VI 1730–2000 hrs Green Engineering PC Salon II 0800–2200 hrs Moog Meeting Room CC: 232 1800–2100 hrs Terrestrial Energy Systems TC San Carlos 0900–1000 hrs ABPTCs Steering Committee Willow Glen I & II 1830–2130 hrs ABPTCs Dinner Meeting Salon V & VI 1000–1100 hrs ABPTCs Communications Willow Glen I & II Subcommittee 1900–2200 hrs Aerospace Power Systems TC CC: 210 E 1100–1200 hrs ABPTCs Education Subcommittee Willow Glen I & II 1900–2200 hrs HRTC Student Meeting Salon III

1200–1400 hrs Nuclear and Future Flight Salon II Propulsion TC Wednesday, 17 July 1200–1330 hrs ASME Propulsion Technical Willow Glen III 0800–2200 hrs Moog Meeting Room CC: 232 Committee 1000–1100 hrs ABP WG Salon I 1300–1400 hrs ABPTCs Honors and Awards Willow Glen I & II Subcommittee Annual Meeting 1430–1530 hrs JPC Steering Committee Salon III 1600–1700 hrs ABP Working Groups (TC Willow Glen III 1530–1630 hrs IECEC Steering Committee Salon III Meeting Prep) 1730–1900 hrs JPC Lessons Learned Salon I 1800–2000 hrs LPTC Steering Committee Willow Glen III 1800–2100 hrs Liquid Propulsion TC Salon III 1800–2100 hrs Energetic Components and Willow Glen I & II 1900–2200 hrs HyTASP PC Salon IV Systems TC 1900–2100 hrs Air Breathing Propulsion Guadalupe SECOND LEVEL Systems Integration TC SECOND LEVEL 1900–2100 hrs High Speed Air Breathing Blossom Hill I SAN JOSE MARRIOTT Propulsion TC and II 1900–2100 hrs Gas Turbine Engines TC CC: 114 SAN JOSE SAN JOSE 1900–2200 hrs Electric Propulsion TC Salon III CONVENTION SALON II BALLROOM SALON V CENTER 1900–2200 hrs Hybrid Rockets TC Salon IV SALON III SALON IV SAN JOSE SAN JOSE CONVENTION SALON IISALON I BALLROOM SALON VSALON VI 1900–2200 hrs Propellants and Combustion TC Salon V & VI CENTER SALON III SALON IV 1900–2200 hrs Solid Rockets TC Salon I & II SALON I SALON VI

SAN WILLOW WILLOW WILLOW GUADALUPE CARLOS GLEN III GLEN II GLEN I

SAN WILLOW WILLOW WILLOW GUADALUPE CARLOS GLEN III GLEN II GLEN I

THIRD LEVEL Key

CC San Jose Convention Center THIRD LEVEL ALMADEN BLOSSOM BLOSSOM BLOSSOM HILL III HILL II HILL I

ALMADEN BLOSSOM BLOSSOM BLOSSOM HILL III HILL II HILL I www.aiaa.org/jpc2013 • www.iecec.org 25 #aiaaPropEnergy PROGRAM AT A GLANCE

Abbreviation Title Start Time Location Sunday, 14 July 1-NW-1 Welcome Reception 1800 hrs Exhibit Hall 2 Monday, 15 July

2-NW-2 Monday Networking Coffee and Pastries 0700 hrs Exhibit Hall 2 3-PLNRY-1 Perspectives on Propulsion Policy, Strategy, Budgets, and Activities for Civil, 0800 hrs Exhibit Hall 1 Commercial, and National Security Space 4-NW-3 Networking Coffee Break 0900 hrs Exhibit Hall 2 5-SB-1 Speakers’ Briefing 0930 hrs Individual Session Rooms 6-ABPSI-1 Inlets I 1000 hrs 210 A 7-ABPSI-2 Engine Systems Integration I 1000 hrs 211 B 8-APC-1 Advanced Aircraft Propulsion Concepts I 1000 hrs 111 9-APS-1 Spacecraft Power Systems and Electronics Design 1000 hrs 213 10-EC-1 Sustainable Energy Conversion Systems 1000 hrs 212 D 11-EC-2 Stirling System Components 1000 hrs 212 B 12-ES-1 Energy Storage 1000 hrs 212 A & C 13-GTE-1 Compressor I 1000 hrs 210 B 14-GTE-2 Turbine I 1000 hrs 210 C 15-GTE-3 Advanced Cycle 1000 hrs 210 D 16-GTE-5 Advanced Engine 1000 hrs 211 C 17-GTE-6 Compressor II 1000 hrs 211 D 18-HR-1 Internal Ballistics Modeling I 1000 hrs 114 19-HSABP-1 Numerical Analysis of Hyper-/Supersonic Inlets 1000 hrs 210 E 20-LP-1 Modeling and Simulation of Nozzles 1000 hrs 112 21-PANEL-1 Evolution of Commercial Space and Future Opportunities 1000 hrs Exhibit Hall 3 22-PANEL-2 The Future of Military Space Launch and How Affordability Will Factor In 1000 hrs 230 C 23-PANEL-3 International Collaboration in Propulsion 1000 hrs 210 F 24-PC-1 Hybrid Rockets and Solid Propellants 1000 hrs 231 25-PC-3 Fundamental Combustion Processes I 1000 hrs 230 B 26-PC-4 Advanced Combustor Concepts I 1000 hrs 113 27-PC-5 Detonations I 1000 hrs 210 G 28-SCP-1 Thermal Sensors and Protection Systems 1000 hrs 210 H 29-TM-1 Two Phase Thermal Control Technologies 1000 hrs 214 30-NW-4 Networking Luncheon (Tickets Required) 1200 hrs Exhibit Hall 2 31-SB-2 Speakers’ Briefing 1300 hrs Individual Session Rooms 32-ABPSI-3 Inlets II 1330 hrs 210 A 33-ABPSI-4 Engine Systems Integration II 1330 hrs 211 B 34-APC-2 Advanced Aircraft Propulsion Concepts II 1330 hrs 111 35-EC-3 Engines 1330 hrs 212 A & C 36-EERE-1 Wind Energy 1330 hrs 213 37-EERE-2 Liquid Fuels 1330 hrs 214 38-GEPC-1 Propulsion Systems and Integration for Next Generation Vehicles 1330 hrs 210 F 39-GTE-7 Compressor III 1330 hrs 210 B www.aiaa.org/jpc2013 • www.iecec.org 26 #aiaaPropEnergy PROGRAM AT A GLANCE

Abbreviation Title Start Time Location 40-GTE-8 Turbine II 1330 hrs 210 C 41-GTE-9 Combustor I 1330 hrs 210 D 42-GTE-10 Gas Turbine Engine Nozzles 1330 hrs 211 A 43-HSABP-2 Numerical Analysis of Supersonic Combustion Systems, Scramjets I 1330 hrs 210 H 44-HSABP-3 Numerical Analysis of Supersonic Combustion Systems, Scramjets II 1330 hrs 210 E 45-LP-2 Modeling and Simulation of Fluids 1330 hrs 113 46-LP-3 Injectors I 1330 hrs 112 47-PANEL-4 NASA SLS Development 1330 hrs Exhibit Hall 3 48-PANEL-5 Emerging Pathways to Jet Fuel 1330 hrs 212 D 49-PC-6 Fundamental Combustion Processes II 1330 hrs 211 C 50-PC-7 Advanced Combustor Concepts II 1330 hrs 231 51-PC-8 Spray Combustion I 1330 hrs 230 A 52-PC-9 Combustion Modeling II 1330 hrs 230 B 53-PC-10 Detonations II 1330 hrs 230 C 54-PC-11 Green Fuels I 1330 hrs 210 G 55-PC-12 High Speed Combustion 1330 hrs 114 56-PP-1 Powering the Next Generation 1330 hrs 211 D 57-TM-2 Spacecraft and Lunar/Mars/Venus Surface Thermal Management I 1330 hrs 212 B 58-NW-5 Networking Coffee Break 1530 hrs Exhibit Hall 2 59-SB-3 Speakers’ Briefing 1530 hrs Individual Session Rooms 60-ABPSI-5 Propulsion Aerodynamics Workshop I 1600 hrs 211 B 61-APS-2 Spacecraft Power Systems In-Orbit Performance 1600 hrs 212 A & C 62-EERE-3 Gas 1600 hrs 213 63-EERE-4 Solar Power 1600 hrs 212 B 64-GTE-14 Cooling and Leakages 1600 hrs 210 D 65-HSABP-4 Analytical/Experimental Analysis of Hyper-/Supersonic Flow Path 1600 hrs 210 E 66-HSABP-5 Numerical Analysis of Dual Mode Supersonic Combustion 1600 hrs 210 H 67-LP-4 Liquid Rocket Engines I 1600 hrs 111 68-LP-5 Spacecraft Propulsion Systems 1600 hrs 230 C 69-LP-6 Turbomachinery I 1600 hrs 114 70-NFF-1 Future Flight Propulsion Systems I 1600 hrs 113 71-PANEL-6 High Power Electric Vehicles and Energy Storage 1600 hrs 212 D 72-PANEL-7 Driving Mission Requirements and Technologies for Space Transportation – the Next 1600 hrs 214 Step after Space Shuttle 73-PANEL-8 Legacy RLV Systems DC-X 1600 hrs Exhibit Hall 3 74-PC-13 Advanced Combustor Concepts III 1600 hrs 211 A 75-PC-14 Fundamental Combustion Processes III 1600 hrs 211 C 76-PC-15 Spray Combustion II 1600 hrs 231 77-PC-16 Rocket Combustion Instability 1600 hrs 230 A 78-PC-17 Combustion Diagnostics 1600 hrs 230 B 79-PC-18 Green Fuels II and Microscale Combustion 1600 hrs 210 G 80-PC-19 Combustion Modeling III 1600 hrs 112 81-SR-1 Motor Design and Plume Effects 1600 hrs 211 D 82-NW-6 Tech Museum of Innovation Off-Site Reception 1830 hrs Off-Site www.aiaa.org/jpc2013 • www.iecec.org 27 #aiaaPropEnergy PROGRAM AT A GLANCE

Abbreviation Title Start Time Location 83-SB-4 Speakers’ Briefing 1830 hrs Individual Session Rooms 84-ABPSI-6 Propulsion Aerodynamics Workshop II 1900 hrs 211 B Tuesday, 16 July

85-NW-7 Tuesday Networking Coffee and Pastries 0700 hrs Exhibit Hall 2 86-PLNRY-2 Propulsion and Power Systems of the Future 0800 hrs Exhibit Hall 1 87-PLNRY-3 A New Industrial Revolution for a Sustainable Energy Future 0800 hrs 212 A & C 88-NW-8 Networking Coffee Break 0900 hrs Exhibit Hall 2 89-SB-5 Speakers’ Briefing 0930 hrs Individual Session Rooms 90-ABPSI-7 Propeller Systems 1000 hrs 210 E 91-APC-3 Advanced Concepts and Planning 1000 hrs 210 F 92-APS-4 Hybrid Power Systems 1000 hrs 212 B 93-EC-4 Cooling 1000 hrs 212 A & C 94-EC-5 Stirling System Testing 1000 hrs 212 D 95-ECS-1 Ignition Characterization and Analysis 1000 hrs 210 A 96-EERE-5 Sustainable Energy Solutions 1000 hrs 214 97-EP-1 Electrospray Propulsion I 1000 hrs 210 B 98-EP-2 Plasma Thruster Modeling I 1000 hrs 210 C 99-EP-3 Helicon Thrusters 1000 hrs 112 100-HR-2 Swirling Oxidizer Flows 1000 hrs 210 D 101-HSABP-6 Hypersonic Air-Breathing Propulsion Concepts 1000 hrs 231 102-ITAR-1 Liquid Rocket Propulsion/Solid Rocket Propulsion/System Concepts and 1000 hrs 210 H Supporting Propulsion Technologies (ITAR Restricted Session) 103-LP-7 Rocket Nozzles 1000 hrs 211 C 104-LP-8 Propellant Storage and Management I 1000 hrs 211 A 105-LP-9 Modeling and Simulation of Engine Heat Transfer I 1000 hrs 230 A 106-LP-10 Green Propellant Infusion Mission (GPIM) 1000 hrs 230 B 107-LP-11 Injectors II 1000 hrs 211 D 108-PANEL-9 Emerging Technologies for the Next Generation of Aircraft Systems 1000 hrs Exhibit Hall 3 109-PP-2 Dealing with the Changing Aerospace Business Environment: A Commercial Aviation 1000 hrs 230 C Perspective 110-SCP-2 Spacecraft Thrusters 1000 hrs 211 B 111-SCP-3 Advanced Seals Session I 1000 hrs 210 G 112-SR-2 Nozzle Materials and Slag Accumulation 1000 hrs 111 113-SR-3 Combustion Instability 1000 hrs 114 114-TM-3 Aerospace and Terrestrial Power Systems Thermal Management I 1000 hrs 213 115-NW-9 IECEC Awards Luncheon 1200 hrs Exhibit Hall 1 116-SB-6 Speakers’ Briefing 1230 hrs Individual Session Rooms 117-ABPSI-8 Integrated Propulsion and Configuration 1300 hrs 210 E 118-APC-4 Advanced Space Propulsion Concepts I 1300 hrs 210 F 119-EP-4 Electrospray Propulsion II 1300 hrs 210 B 120-EP-5 Plasmas in Propulsion 1300 hrs 211 B 121-EP-6 Plasma Thruster Modeling II 1300 hrs 211 C 122-EP-7 Ion Engines I 1300 hrs 211 D www.aiaa.org/jpc2013 • www.iecec.org 28 #aiaaPropEnergy PROGRAM AT A GLANCE

Abbreviation Title Start Time Location 123-HR-3 Internal Ballistics Modeling II 1300 hrs 210 D 124-HR-4 Novel Motor Operating Conditions I 1300 hrs 211 A 125-HSABP-7 Innovative Scramjet Concepts 1300 hrs 231 126-LP-12 Propellant Storage and Management II 1300 hrs 210 C 127-LP-13 Modeling and Simulation of Engines and Propulsion Systems 1300 hrs 230 A 128-LP-15 Liquid Propulsion History I: LOX/HC Propulsion I: Goddard – Peenemuende – Sputnik 1300 hrs 230 B (8K71PS/8A91 R-7), Vanguard, Juno 1 to Titan, Atlas, Falcon and Beyond 129-NFF-4 Fusion and Alternative Nuclear Concepts I 1300 hrs 113 130-PANEL-10 Disruptive Aircraft and Propulsion Technologies for the Future 1300 hrs Exhibit Hall 3 131-PP-3 Dealing with the Changing Aerospace Business Environment: A Military Aviation 1300 hrs 230 C Perspective 132-SCP-4 Advanced Seals Session II 1300 hrs 210 G 133-SR-4 Flow Effects in Solid Rocket Motors 1300 hrs 111 134-ST-1 Space Transportation I 1300 hrs 112 135-SB-7 Speakers’ Briefing 1400 hrs Individual Session Rooms 136-APS-3 Advanced Space Power Generation Designs & Status 1430 hrs 212 A & C 137-EC-6 Thermoelectric Devices and Systems 1430 hrs 212 D 138-TFES-2 Combustion 1430 hrs 213 139-TM-4 Heating and Cooling of Buildings I 1430 hrs 212 B 140-TM-5 Heating and Cooling of Buildings II 1430 hrs 214 141-NW-10 Networking Coffee Break 1500 hrs Exhibit Hall 2 142-SB-8 Speaker Briefing 1530 hrs Individual Session Rooms 143-ABPSI-9 Engine Systems Integration II 1600 hrs 210 E 144-APC-5 Advanced Rocket Propulsion Concepts II 1600 hrs 210 F 145-CS-1 Propulsion Challenges for Commercial Reusable Space Vehicles 1600 hrs 210 A 146-ECS-2 Energetic Devices – Modeling and Analysis 1600 hrs 112 147-EDU-1 Engineering Education in a New Fiscal Reality 1600 hrs 230 C 148-EP-8 Micropropulsion I 1600 hrs 210 B 149-HR-5 Paraffin Fuels I 1600 hrs 210 D 150-HR-6 Paraffin Fuels II 1600 hrs 211 A 151-HSABP-8 Pulse/Rotating Detonation Systems 1600 hrs 231 152-HSABP-9 Numerical Analysis of Supersonic Combustion Systems, Scramjets III 1600 hrs 230 A 153-ITAR-3 Propellants and Combustion/High Speed Air-Breathing 1600 hrs 210 H (ITAR Restricted Session) 154-LP-16 Propellant Storage and Management III 1600 hrs 211 D 155-LP-17 Liquid Rocket Engines III 1600 hrs 210 C 156-LP-18 Modeling and Simulation of Instabilities I 1600 hrs 211 C 157-LP-19 Modeling and Simulation of Engine Heat Transfer II 1600 hrs 211 B 158-LP-20 Liquid Propulsion History II: LOX/Hydrocarbon Propulsion: Liquid Propulsion 1600 hrs 230 B Capability At Crossroads; Where Do We Go From Here? 159-NFF-5 Nuclear Thermal Propulsion II: Engine Modeling 1600 hrs 113 160-PANEL-11 DoD Energy Panel 1600 hrs Exhibit Hall 3 161-SCP-5 Integrated Modeling and Simulation 1600 hrs 210 G 162-SCP-6 Systems Design, Engineering and Analysis I 1600 hrs 114 163-SR-5 Propellant Effects on Internal Ballistics and Performance 1600 hrs 111 www.aiaa.org/jpc2013 • www.iecec.org 29 #aiaaPropEnergy PROGRAM AT A GLANCE

Abbreviation Title Start Time Location 164-SB-9 Speakers’ Briefing 1830 hrs Individual Session Rooms 165-APC-6 Advanced Space Propulsion Concepts II 1900 hrs 210 F 166-EDU-2 Propulsion Education I 1900 hrs 230 C 167-LP-22 Combustion Devices I 1900 hrs 211 B 168-SR-6 SRTC Special Session: M. Prevost and F. Blomshield (Testing and Experimental 1900 hrs 111 Combustion Instability) Wednesday, 17 July

169-NW-11 Wednesday Networking Coffee and Pastries 0700 hrs Exhibit Hall 2 170-PLNRY-4 Hypersonic Propulsion, Leveraging Today to Deliver Unique Capabilities in the Future 0800 hrs Exhibit Hall 1 171-PLNRY-5 Power Generation and Processing Challenges for Near-Term High Power Solar 0800 hrs 212 A & C Electric Propulsion 172-NW-12 Networking Coffee Break 0900 hrs Exhibit Hall 2 173-SB-10 Speakers’ Briefing 0900 hrs Individual Session Rooms 174-APC-7 SOA Propulsion Concepts 0930 hrs 111 175-APS-5 Spacecraft Solar Power and Solar Array Designs 0930 hrs 212 D 176-EC-7 Energy Harvesting 0930 hrs 212 A & C 177-EP-9 Electrospray Propulsion III 0930 hrs 210 D 178-EP-10 Hollow Cathodes 0930 hrs 211 A 179-HR-7 Fuel Regression Characterization 0930 hrs 211 C 180-HR-8 Novel Motor Operating Conditions II 0930 hrs 211 D 181-HR-9 New Approaches to Hybrid Motor Development 0930 hrs 211 B 182-ITAR-4 Pressure Gain Combustion: VULCAN Program Overview 0930 hrs 210 H (ITAR Restricted Session) 183-LP-23 Monopropellant Catalyst Development and Decomposition Phenomena 0930 hrs 210 A 184-LP-24 Liquid Rocket Engines IV 0930 hrs 210 B 185-LP-26 Modeling and Simulation of Instabilities II 0930 hrs 231 186-LP-27 Combustion Devices II 0930 hrs 210 F 187-LP-28 Turbomachinery II 0930 hrs 210 E 188-LP-29 Modeling and Simulation of Injector and Chamber Flows 0930 hrs 230 A 189-NFF-6 Fusion and Alternative Nuclear Concepts II 0930 hrs 112 190-NFF-7 Nuclear Thermal Propulsion III: Missions, Vehicles and Architectures 0930 hrs 113 191-PANEL-12 High Speed Propulsion Development and Implementation 0930 hrs Exhibit Hall 3 192-PP-4 Public-Private Partnerships to Accelerate Technology Transition 0930 hrs 230 C 193-SR-7 SRM Throttleability Using Pintle Nozzles and Novel Techniques 0930 hrs 230 B 194-SR-8 Particle Effects on Combustion Instability and Agglomeration 0930 hrs 210 G 195-SR-9 Nozzle and Internal Ballistic Prediction 0930 hrs 114 196-TFES-1 Gaseous Fuels 0930 hrs 214 197-TM-6 Aerospace and Terrestrial Power Systems Thermal Management II 0930 hrs 213 198-TM-7 Spacecraft and Lunar/Mars/Venus Surface Thermal Management II 0930 hrs 212 B 199-NW-13 JPC Awards Luncheon 1200 hrs Exhibit Hall 1 200-SB-11 Speakers’ Briefing 1400 hrs Individual Session Rooms 201-ECS-3 Energetic Devices and Materials – Design and Application 1430 hrs 214 202-EDU-3 Technology, Education and NASA’s New Asteroid Grand Challenge 1430 hrs 230 C 203-EDU-4 Propulsion Education II 1430 hrs 211 B www.aiaa.org/jpc2013 • www.iecec.org 30 #aiaaPropEnergy PROGRAM AT A GLANCE

Abbreviation Title Start Time Location 204-EP-11 Ion Engines II 1430 hrs 210 E 205-EP-12 Qualification and Operation of EP Systems 1430 hrs 212 D 206-EP-14 Hall Thrusters 1430 hrs 210 D 207-EP-15 Micropropulsion II 1430 hrs 211 A 208-EP-16 Applications of Electric Propulsion 1430 hrs 212 A & C 209-EP-17 Facilities Effects and Interactions with Materials 1430 hrs 212 B 210-HR-10 Analytic Modeling of Hybrid Motors 1430 hrs 211 C 211-HR-11 Testing of Hybrid Motors 1430 hrs 211 D 212-ITAR-5 Thermal Management and Enegy Conversion Device Technologies 1430 hrs 210 H (ITAR Restricted Session) 213-LP-30 Combustion Chamber Heat Transfer 1430 hrs 210 F 214-LP-31 Liquid Rocket Engines V 1430 hrs 210 B 215-LP-33 Ignition Systems 1430 hrs 114 216-LP-34 Liquid Rocket Combustion Modeling 1430 hrs 111 217-LP-35 German Liquid Rocket Propulsion 1430 hrs 210 A 218-NFF-8 Nuclear Thermal Propulsion IV: Testing and Programmatics 1430 hrs 113 219-PANEL-13 The Aerospace Industry Coping with the Current Fiscal Environment 1430 hrs 230 B 221-SCP-7 Systems Design, Engineering and Analysis II 1430 hrs 231 222-SR-10 Solid Fueled Ramjet/Scramjet and Novel Propellants 1430 hrs 230 A 223-SR-11 SRM Systems 1430 hrs 210 G 224-ST-2 Space Transportation II 1430 hrs 213

www.aiaa.org/jpc2013 • www.iecec.org 31 #aiaaPropEnergy Sunday Sunday, 14 July 2013 1-NW-1 Welcome Reception Exhibit Hall 2 1800 - 1930 hrs Monday Monday, 15 July 2013 2-NW-2 Monday Networking Coffee & Pastries Exhibit Hall 2 0700 - 0800 hrs Monday, 15 July 2013 3-PLNRY-1 Perspectives on Propulsion Policy, Strategy, Budgets, and Activities for Civil, Commercial, and National Security Space Exhibit Hall 1 0800 - 0900 hrs Keynote Speaker John Olson Former Assistant Director for Space and Aeronautics, White House Office of Science and Technology Policy VP, Space Systems Group, Sierra Nevada Corporation Monday, 15 July 2013 4-NW-3 Networking Coffee Break Exhibit Hall 2 0900 - 1000 hrs Monday, 15 July 2013 32 5-SB-1 Speakers’ Briefing Individual Session Rooms 0930 - 1000 hrs Monday, 15 July 2013 6-ABPSI-1 Inlets I 210 A Chaired by: K. BLODGETT, GE Aviation 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3600 AIAA-2013-3601 AIAA-2013-3602 Twin Impinging Jets Aligned With Computational Investigation of The Influence of Duct Development a Crossflow Compressible Flow in a Diffusing Distance on Screen-Generated Total J. Barata, University of Beira Interior, S-duct Pressure Distortion Profiles Covilha, Portugal B. Reza Ahrabi, K. Sreenivas, R. Webster, W. O’Brien, J. Bailey, Virginia Polytechnic University of Tennessee, Chattanooga, Institute and State University, Blacksburg, Chattanooga, TN VA Monday, 15 July 2013 7-ABPSI-2 Engine Systems Integration I 211 B Chaired by: C. BEARD, Boeing Commercial Airplanes 1000 hrs 1030 hrs AIAA-2013-3603 AIAA-2013-3604 Experimental Study of the An Assessment of Relative Unsteady Aerodynamics the Technology Benefits of a Variable Compressor-Combustor Interface of Pitch Fan and Variable Area Nozzle a Lean Burn Combustion System G. Krishnan, C. Perullo, D. Mavris, Georgia A. Walker, P. Graham, J. Carrotte, A. Institute of Technology, Atlanta, GA Spencer, J. McGuirk, Loughborough University, Loughborough, United Kingdom Monday, 15 July 2013 8-APC-1 Advanced Aircraft Propulsion Concepts I 111 Chaired by: T. CHEN, NASA 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3605 AIAA-2013-3606 AIAA-2013-3607 AIAA-2013-3608 NASA Fixed Wing Project Propulsion Robust Optimization of Thermal Design and Performance Pre-Concept Performance Research and Technology and Power Systems For a Battery- Considerations for a Investigation of Electrically Development Activities to Reduce Powered Competition Aircraft Superconducting Electric Power Powered Aero-Propulsion Systems Specific Energy Consumption K. Reynolds, NASA Ames Research Center, System to power future Aircraft A. Seitz, A. Isikveren, M. Hornung, M. Hathaway, R. Del Rosario, NASA Glenn Moffett Field, CA P. Malkin, CERFACS, Cranfield, United Bauhaus Luftfahrt e.V., Munich, Germany Research Center, Cleveland, OH; N. Madavan, Kingdom NASA Ames Research Center, Moffett Field, CA Monday, 15 July 2013 9-APS-1 Spacecraft Power Systems and Electronics Design 213 Chaired by: R. CHAMBERS, Lockheed Martin Corporation and G. LAM, Research Division 1000 hrs 1030 hrs AIAA-2013-3609 AIAA-2013-3610 Electric Propulsion Electronics Soil Moisture Active Passive Activities in Europe - 2013 (SMAP) Observatory Power System M. Gollor, ESA, Noordwijk, The Architecture Netherlands; M. Boss, Astrium, H. Aintablian, Jet Propulsion Laboratory, Friedrichshafen, Germany; E. Bourguignon, California Institute of Technology, Thales Alenia Space, Charleroi, Belgium; P. Pasadena, CA Galantini, Selex ES, Nerviana, Italy; F. De la Cruz, Crisa, Tres Cantos, Spain 33 Monday, 15 July 2013 10-EC-1 Sustainable Energy Conversion Systems 212 D Chaired by: P. CORNELL, NASA Glenn Research Center and D. WOLFORD, NASA Glenn Research Center 1000 hrs 1030 hrs AIAA-2013-3611 AIAA-2013-3612 A Simulator for Experimental An Ammonia/Hydrogen-Fueled Evaluation of Heat Collection Micro-Thermophotovoltaic Device Elements in Parabolic Concentrating Integrated with a Micro-reformer Solar Power Troughs D. Um, O. Kwon, Sungkyunkwan R. Gardner, J. Goljenboom, J. LaFavor, A. University, Suwon, South Korea Messina, P. Benjamin, M. Traum, Milwaukee School of Engineering, Milwaukee, WI Monday, 15 July 2013 11-EC-2 Stirling System Components 212 B Chaired by: T. CHAN, Lockheed Martin Space Systems 1000 hrs 1030 hrs AIAA-2013-3613 AIAA-2013-3614 A Review of Models for Appendix Performance Analysis of a Fault Gap Losses in Stirling Cycle Tolerant Controller for a Single Machines Stirling Convertor J. Pfeiffer, H. Kuehl, Technical University of D. Duven, H. Ambrose, M. Fraeman, Dortmund, Dortmund, Germany D. Frankford, Johns Hopkins University Applied Physics Laboratory, Laurel, MD Monday, 15 July 2013 12-ES-1 Energy Storage 212 A & C Chaired by: R. SHAW, Lockheed Martin Space Systems 1000 hrs 1030 hrs AIAA-2013-3615 AIAA-2013-3616 Peripheral Electronics Prototype of High Energy Density Storage Using Super-Capacitor Energy Storage for In-Situ Hydrogen Production Small Satellites S. Elitzur, V. Rosenband, A. Gany, T. Shimizu, Kyushu Institute of Technology, Technion--Israel Institute of Technology, Kitakyushu, Japan; C. Underwood, Haifa, Israel University of Surrey, Guildford, United Kingdom; M. Cho, Kyushu Institute of Technology, Kitakyushu, Japan Monday, 15 July 2013 13-GTE-1 Compressor I 210 B Chaired by: M. LIOU, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3617 AIAA-2013-3618 AIAA-2013-3619 AIAA-2013-3620 An evaluation of the potential An Efficient Coupled Method of Computationally Efficient Axial Analysis and Compression of of additive manufacturing Cascade Flutter Investigation Based Compressor Characteristic Map Time-Accurate Turbomachinery technologies in future aero engine on Reduced Order Model Generation Based on 1-D Meanline Simulations Using Proper design D. Su, W. Zhang, Northwestern Polytechnical Approximation Orthogonal Decomposition D. Rockel, A. Hupfer, H. Kau, Technical University, Xi’an, China; M. Ma, China H. Desmidt, K. Ekici, K. Young, University T. Blanc, S. Gorrell, M. Jones, Brigham University of Munich, Munich, Germany Aerodynamics Research and Development of Tennessee, Knoxville, Knoxville, TN Young University, Provo, UT; E. Duque, Center, Mianyang, China; Z. Ye, Northwestern

34 Intelligent Light, Rutherford, NJ Polytechnical University, Xi’an, China Monday, 15 July 2013 14-GTE-2 Turbine I 210 C Chaired by: S. SUBRAMANIAN, QuEST Global, Inc. 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3621 AIAA-2013-3622 AIAA-2013-4178 Computation of Heat Transfer Experimental Heat Transfer Study Fabrication and Analysis of Porous In Turbine Rotor Blade Cooling in an Intermediate Turbine Duct Superalloys for Turbine Components Channels with Angled Rib B. Rojo, V. Chernoray, M. Johansson, Using Laser Additive Manufacturing Turbulators M. Golubev, Chalmers University of J. Bernstein, A. Bravato, B. Ealy, M. Ricklick, J. G. Flynt, R. Webster, K. Sreenivas, Technology, Göteborg, Sweden Kapat, University of Central Florida, Orlando, University of Tennessee, Chattanooga, FL; I. Mingareev, M. Richardson, Townes Laser Chattanooga, TN Institute, Orlando, FL; W. Meiners, I. Kelbassa, Fraunhofer Institute for Laser Technology, Orlando, FL Monday, 15 July 2013 15-GTE-3 Advanced Cycle 210 D Chaired by: J. SORDYL, Williams International 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3623 AIAA-2013-3624 AIAA-2013-3625 AIAA-2013-3626 Potential Benefits to Commercial Experimental Comparison of Axial Design and Demonstration of Investigation of Operating Propulsion Systems from Pressure Turbine Performance Under Pulsed- Emergency Control Modes for Conditions on Distortion Transfer Gain Combustion Air and Pulsed-Detonation Flows Enhanced Engine Performance and Generation in a Three Stage S. Jones, D. Paxson, NASA Glenn Research A. St. George, R. Driscoll, D. Munday, Y. Liu, N&R Engineering, Parma Heights, Fans Center, Cleveland, OH E. Gutmark, University of Cincinnati, OH; J. Litt, T. Guo, NASA Glenn Research M. Marshall, D. Weston, S. Gorrell, Cincinnati, OH Center, Cleveland, OH Brigham Young University, Provo, UT Monday, 15 July 2013 16-GTE-5 Advanced Engine 211 C Chaired by: J. TAI, Georgia Institute of Technology 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3627 AIAA-2013-3628 AIAA-2013-3629 AIAA-2013-3630 Optimization of Open Rotor Updated Assessment of an Open Effect of a Winglet on Open Rotor Off-Design Characteristics of Low- Engines for Civil Aircraft Using a Rotor Airplane using an Advanced Aerodynamics and Tip Vortex Fuel Consumption Gas Turbine Cooperative Evolutionary Method Blade Design Interaction Engine for Long-Range UAV L. Casalino, D. Pastrone, F. Simeoni, E. Hendricks, J. Berton, W. Haller, M. S. Read, T. Hynes, University of R. Andriani, U. Ghezzi, Technical University Technical University of Turin, Turin, Italy Tong, NASA Glenn Research Center, Cambridge, Cambridge, United Kingdom of Milan, Milan, Italy; A. Ingenito, F. Cleveland, OH; M. Guynn, NASA Langley Gamma, A. Agresta, University of Rome Research Center, Hampton, VA “La Sapienza”, Rome, Italy Monday, 15 July 2013 17-GTE-6 Compressor II 211 D Chaired by: G. WELCH, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3631 AIAA-2013-3632 AIAA-2013-3633 Computational Study of the CC3 Effect of Casing Groove Locations Characterization of the Discharge Impeller and Vaneless Diffuser on the Performance of an Axial Flow of a Dual Volute Axi- Experiment Flow Stage Centrifugal Gas Turbine Compressor S. Kulkarni, NASA Glenn Research Center, W. Lin, K. Sreenivas, R. Webster, J. Ilott, StandardAero, Winnipeg, Canada; Cleveland, OH; T. Beach, Coyote Hollow D. Hyams, University of Tennessee, W. Allan, A. Asghar, Royal Military College of Consulting, Cleveland, OH; G. Skoch, NASA Chattanooga, Chattanooga, TN Canada, Kingston, Canada; R. Woodason, Glenn Research Center, Cleveland, OH StandardAero, Winnipeg, Canada

35 Monday, 15 July 2013 18-HR-1 Internal Ballistics Modeling I 114 Chaired by: B. EVANS, Space Propulsion Group Inc. and J. DAVITIAN, The Aerospace Corporation 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3634 AIAA-2013-3635 AIAA-2013-3636 AIAA-2013-3637 A Study on Performance High Performance Hybrid Mass Flow Rate and Isolation CFD Analysis of Hybrid Rocket Improvement of Paraffin Fueled Propulsion System for Small Characteristics of Injectors for Use with Flowfields Including Fuel Pyrolysis Hybrid Rocket Engines with Multi- Satellites Self-Pressurizing Oxidizers in Hybrid and Nozzle Ablation Section Swirl Injection Method L. Simurda, G. Zilliac, NASA Ames Rockets D. Bianchi, F. Nasuti, University of Rome K. Araki, Y. Hirata, S. Oyama, K. Ohe, S. Aso, Research Center, Moffett Field, CA B. Waxman, B. Cantwell, Stanford University, “La Sapienza”, Rome, Italy Y. Tani, Kyushu University, Fukuoka, Japan; T. Stanford, CA; G. Zilliac, NASA Ames Research Shimada, Japan Aerospace Exploration Agency Center, Moffett Field, CA; J. Zimmerman, (JAXA), Kanagawa, Japan Stanford University, Stanford, CA Monday, 15 July 2013 19-HSABP-1 Numerical Analysis of Hyper-/Supersonic Inlets 210 E Chaired by: H. HASSAN, North Carolina State University 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3638 AIAA-2013-3639 AIAA-2013-3640 Assessment of Wall-modeled Large Numerical Investigation of Effects Inlet Geometry Effects on the Eddy Simulation For Supersonic of Boundary Layer Bleed on a Internal Performance of a Variable Compression Ramp Flows RBCC inlet in Ejector Mode Flow Ducted Rocket Combustor D. Dawson, S. Lele, J. Bodart, Stanford L. Shi, G. He, F. Qin, X. Wei, X. Lv, X. S. Kim, B. Natan, Technion--Israel Institute University, Stanford, CA Tang, B. Lin, Northwestern Polytechnical of Technology, Haifa, Israel University, Xi’an, China Monday, 15 July 2013 20-LP-1 Modeling and Simulation of Nozzles 112 Chaired by: T. GIEL, Jacobs Technology and H. KAGAWA, JAXA 1000 hrs 1030 hrs AIAA-2013-3641 AIAA-2013-3642 Development of an Aeroelastic Linear Stability Analysis Using Modeling Capability for Transient the Arnoldi Eigenmode Extraction Nozzle Side Load Analysis Technique Applied to Separated T. Wang, NASA Marshall Space Flight Nozzle Flow Center, Huntsville, AL; X. Zhao, Alabama R. Larusson, N. Andersson, Chalmers University A&M University, Huntsville, AL; S. Zhang, of Technology, Göteborg, Sweden; J. Ostlund, ESI Group, Huntsville, AL; Y. Chen, GKN Aerospace Engine Systems, Trollhättan, National Applied Research Laboratories, Sweden; L. Eriksson, Chalmers University of Hsinchu, Taiwan Technology, Göteborg, Sweden Monday, 15 July 2013 21-PANEL-1 Evolution of Commercial Space and Future Opportunities Exhibit Hall 3 1000 - 1200 hrs Commercial space is a rapidly growing sector of the space economy. This panel will present a status of current commercial space efforts and challenges with a look forward to new and evolving opportunities. Moderator: James Halsell, Technical Director, Aerospace Systems, Dynetics Panelists: Kent Rominger Bob Richards John Vilja Todd Mosher Brett Alexander Vice President and Program Manager Vice President, Human Spaceflight Systems’ Advanced Vice President Strategy Director, Design and Development Director Business Development ATK Programs Group Aerojet Rocketdyne Sierra Nevada Blue Origen

36 Orbital Sciences Corporation

Monday, 15 July 2013 22-PANEL-2 The Future of Military Space Launch and How Affordability Will Factor In 230 C 1000 - 1200 hrs The Future of Military Space Launch and How Affordability Will Factor In: Evolved Expendable Launch Vehicle (EELV) is the U.S. Air Force’s expendable launch system that is intended to assure access to space for U.S. government payloads. Started with the goal of making government space launch more affordable and reliable, the program resulted in the development of the Delta IV and Atlas V, which remain the primary methods for launching U.S. military payloads. The panelists, each representing companies with involvement in the EELV program, will discuss how the program has changed over time as well as present and future challenges, in particular the continued focus on cost reductions, while the program strives to sustain and support America’s space interests. Moderator: Andy Crocker, Propulsion Department Manager, Dynetics Panelists: Steven Bouley Andrew Jackson Bill Harding Bill Parsons Vice President, Expendable Launch Systems Atlas & Delta Structures Manager Director, Program Management President & CEO Aerojet Rocketdyne ATK United Launch Alliance RD AMROSS, LLC

Monday, 15 July 2013 23-PANEL-3 International Collaboration in Propulsion 210 F 1000 - 1200 hrs Panelists will discuss the effect of the current global environment on the international cooperation efforts in propulsion and space flight. Moderator: John Horack, Vice President, Space Systems, Teledyne Brown Engineering Panelists: Charles Smith Jens Lassmann Mark Lewis Charles Precourt Julie VanKleek Human Exploration & Operations Directorate Vice President, Space Systems Director Vice President & General Manager Vice President Space Advanced Programs NASA HQ Astrium Science and Technology Policy Institute Space Launch Division, Aerospace Group Aerojet Rocketdyne ATK Monday, 15 July 2013 24-PC-1 Hybrid Rockets and Solid Propellants 231 Chaired by: T. SHIMADA, Japan Aerospace Exploration Agency-Institute of Space Technology and Aeronautics 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3643 AIAA-2013-3644 AIAA-2013-3645 AIAA-2013-3646 Interaction of vortices due to Large Eddy Simulation of Swirling N2O-HTPB Hybrid Rocket A Comparison between the diaphragm on the wall blowing Combustion Flow with Wall Fuel Combustion Modeling with Mixing OpenFOAM® Toolbox and Custom- surface Blowing modeled for Hybrid Rocket Enhancement Designs built Numerical Solvers for Composite C. Lee, K. Mon, Konkuk University, Seoul, Engines Y. Chen, National Space Organization, Solid Propellant Combustion Modeling South Korea; H. Koo, Seoul National M. Motoe, University of Tokyo, Tokyo, Hsinchu, Taiwan; T. Chou, A. Lai, J. Wu, F. Retief, J. Knoetze, Stellenbosch University, University, Seoul, South Korea Japan; T. Shimada, Japan Aerospace National Chiao Tung University, Hsinchu, Stellenbosch, South Africa; C. Rousseau, Exploration Agency (JAXA), Sagamihara, Taiwan Rheinmetall Denel Munition, Somerset West, Japan South Africa; A. Steenkamp, Flamengro, Pretoria, South Africa; G. Smit, Stellenbosch University, Stellenbosch, South Africa Monday, 15 July 2013 25-PC-3 Fundamental Combustion Processes I 230 B Chaired by: M. ANAND, Rolls-Royce Corporation 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3647 AIAA-2013-3648 AIAA-2013-3649 AIAA-2013-3650 Characterization of Swirl-Venturi Computational Investigation Small Internal Combustion Engine Thermo-acoustic Coupling in Swirl- Lean Direct Injection Designs for of Combustion Instabilities in a Dependence on Inlet Pressure and Stabilized Flames with Helical Aviation Gas-Turbine Combustion Laboratory-Scale LDI Gas Turbine Temperature at Altitude Vortices C. Heath, NASA Glenn Research Center, Engine T. Husaboe, J. Rittenhouse, M. Polanka, V. Caux-Brisebois, A. Steinberg, University

37 Cleveland, OH C. Yoon, R. Gejji, C. Huang, W. Anderson, Air Force Institute of Technology, Wright- of Toronto, Toronto, Canada; C. Arndt, W. Purdue University, West Lafayette, IN; V. Patterson AFB, OH; P. Litke, Air Force Meier, German Aerospace Center (DLR), Sankaran, Air Force Research Laboratory, Research Laboratory, Wright-Patterson Stuttgart, Germany Edwards AFB, CA AFB, OH; J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH Monday, 15 July 2013 26-PC-4 Advanced Combustor Concepts I 113 Chaired by: H. MONGIA, Purdue University 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3651 AIAA-2013-3652 AIAA-2013-3653 AIAA-2013-3654 Biofuel Emissions of a Multipoint N+3 and N+4 Generation N+3 and N+4 Generation N+3 and N+4 Generation Staged Low NOx Combustion Aeropropulsion Engine Combustors: Aeropropulsion Engine Combustors Aeropropulsion Engine Combustors: System at Intermediate Pressures Part 4: Specific Fuel Burn and Co2 Part 5: NOx, CO, HC and Smoke Part 6: Operating Conditions, B. Dolan, R. Villalva Gomez, D. Munday, Emissions Emissions Target Goals and Lifted Jets E. Gutmark, University of Cincinnati, H. Mongia, Purdue University, West H. Mongia, Purdue University, West H. Mongia, Purdue University, West Cincinnati, OH; G. Zink, J. Ryon, S. Pack, Lafayette, IN Lafayette, IN Lafayette, IN J. Goeke, United Technologies Corporation, Des Moines, IA Monday, 15 July 2013 27-PC-5 Detonations I 210 G Chaired by: E. BARBOUR, The Aerospace Corpation 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3655 AIAA-2013-3656 AIAA-2013-3657 Simulations of Unsteady Shocks Flame Propagation from the Closed Deflagration to Detonation and Detonation Interactions with End of an Open-ended Tube: an Transition by Hybrid Obstacles in Structures analysis of the effects of fuel type, Pulse Detonation Engines B. Muralidharan, S. Menon, Georgia tube length, and equivalence ratio J. Li, C. Teo, K. Lim, C. Wen, B. Khoo, Institute of Technology, Atlanta, GA and an insight into flame dynamics National University of Singapore, J. Gray, J. Moeck, C. Paschereit, Technical Singapore, Singapore University of Berlin, Berlin, Germany Monday, 15 July 2013 28-SCP-1 Thermal Sensors and Protection Systems 210 H Chaired by: C. GATTO, Jet Propulsion Laboratory 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3658 AIAA-2013-3659 AIAA-2013-3660 Development of a Test Bed with Development of an In-Situ Ablation In-situ Ablation Recession an Increased Area for Ablative Sensor for Thermal Protection Sensor Based on Ultra-Miniature Research Systems Thermocouples - Part A: 0.25mm C. Miers, R. Naylor, E. Woods, E. Gibson, C. Yee, M. Ray, F. Tang, J. Wan, J. Koo, Diameter Thermocouples J. Koo, University of Texas, Austin, University of Texas, Austin, Austin, TX; M. M. Natali, J. Koo, KAI, LLC, Austin, TX; E. Austin, TX Natali, University of Perugia, Perugia, Italy Allcorn, O. Ezekoye, University of Texas, Austin, Austin, TX 38 Monday, 15 July 2013 29-TM-1 Two Phase Thermal Control Technologies 214 Chaired by: C. TARAU, Advanced Cooling Technologies and S. SPENCER, Naval Research Laboratory-Code 8221 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3661 AIAA-2013-3662 AIAA-2013-3663 AIAA-2013-3664 High Temperature Heat Pipes for Variable Conductance Heat Pipe Variable Conductance Heat Pipe Thermal Control of Surveillance Space Fission Power Radiator for Lunar Fission Power Cooling of Stirling Convertor and Systems Using Pulsating Heat Pipes K. Walker, C. Tarau, W. Anderson, Systems General Purpose Heat Source R. Riehl, L. de O. Cachuté, National Advanced Cooling Technologies, Inc., B. Muzyka, C. Peters, Advanced Cooling C. Tarau, C. Schwendeman, W. Anderson, Institute for Space Research (INPE), São Lancaster, PA Technologies, Inc., Lancaster, PA; T. Stern, Advanced Cooling Technologies, Inc., José dos Campos, Brazil G. Williams, Vanguard Space Technologies, Lancaster, PA; P. Cornell, NASA Glenn Inc., San Diego, CA; J. Hartenstine, W. Research Center, Cleveland, OH Anderson, Advanced Cooling Technologies, Inc., Lancaster, PA Monday, 15 July 2013 30-NW-4 Networking Reception Exhibit Hall 2 1200 - 1330 hrs (Tickets Required) Monday, 15 July 2013 31-SB-2 Speakers’ Briefing Individual Session Rooms 1300 - 1330 hrs Monday, 15 July 2013 32-ABPSI-3 Inlets II 210 A Chaired by: J. FLAMM, NASA Langley Research Center 1330 hrs 1400 hrs AIAA-2013-3665 AIAA-2013-3666 The StreamVane Method: A New Way Inertial Particle Separator Efficiency to Generate Swirl Distortion for Jet Using Spherical Particles Engine Research D. Barone, J. Hawkins, E. Loth, University of K. Hoopes, W. O’Brien, Virginia Polytechnic Virginia, Charlottesville, Charlottesville, VA; P. Institute and State University, Blacksburg, VA Snyder, Rolls-Royce Group plc, Indianapolis, IN Monday, 15 July 2013 33-ABPSI-4 Engine Systems Integration II 211 B Chaired by: B. MCKAY, Lockheed Martin Aeronautics 1330 hrs 1400 hrs AIAA-2013-3667 AIAA-2013-3668 Frequency Resolved Density Mach 8 Flight condition Tests of Fluctuation Measurements of Rocket-Ramjet Combined-Cycle Combustion Oscillations in a Model Engine Model Combustor M. Takegoshi, S. Tomioka, M. Kodera, S. J. Peterleithner, A. Marn, T. Leitgeb, Hasegawa, K. Kato, T. Saito, K. Tani, A. J. Woisetschläger, Graz University of Murakami, Japan Aerospace Exploration Technology, Graz, Austria Agency (JAXA), Kakuda, Japan Monday, 15 July 2013

39 34-APC-2 Advanced Aircraft Propulsion Concepts II 111 Chaired by: J. ROBINSON, Retired f/Boeing 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3669 AIAA-2013-3670 AIAA-2013-3671 A comprehensive workflow combining Potential of high power density Geared Turbofan With Water numerical and experimental tools to Diesel engines for green rotorcrafts Alcohol Technology study the combustion of aviation fuels propulsion A. Purohit, Hindusthan Educational in Diesel aircraft engines S. Richard, IFP Energies nouvelles, Rueil- Institutions, Coimbatore, India S. Richard, IFP Energies nouvelles, Rueil- Malmaison, France Malmaison, France Monday, 15 July 2013 35-EC-3 Engines 212 A & C Chaired by: S. WILSON, NASA Glenn Research Center and J. SCHREIBER, NASA Glenn Research Center 1330 hrs 1400 hrs AIAA-2013-3672 AIAA-2013-3673 A Direct Simulation Monte Carlo Study Understanding the Thermodynamic on the Effect of Temperature Gradient Possibilities and Limitations of the on the Gas Mixing in Microgeometries Solid-oxide Fuel Cell, Gas Turbine M. Darbandi, M. Sabouri, E. Lekzian, Sharif Double Cycle University of Technology, Tehran, Iran; G. R. Pass, C. Edwards, Stanford University, Schneider, University of Waterloo, Waterloo, Stanford, CA Canada Monday, 15 July 2013 36-EERE-1 Wind Energy 213 Chaired by: E. KHALIL, Cairo University; N. GHADDAR, American University of Beirut and D. MUTH, Idaho National Lab 1330 hrs 1400 hrs AIAA-2013-3674 AIAA-2013-3675 Hybrid Solar/Natural Gas Power Design and CFD Analysis of Wind System Turbine Blades R. Wegeng, Battelle Memorial Institute, R. Amano, A. Gupta, A. Alsultan, University Richland, WA; C. Pestak, Battelle Memorial of Wisconsin, Milwaukee, Milwaukee, WI Institute, Cleveland, OH; J. Mankins, SolarThermoChemical, LLC, Santa Maria, CA Monday, 15 July 2013 37-EERE-2 Liquid Fuels 214 Chaired by: E. KHALIL, Cairo University; N. GHADDAR, American University of Beirut and D. MUTH, Idaho National Lab 1330 hrs 1400 hrs AIAA-2013-3676 AIAA-2013-3677 Combustion Characteristics of Combustion Properties of Jet A/ Diesel/Canola Methyl Ester Spray Ethanol Blends in a Porous Media Flames in a Furnace Burner C. Morton, V. Tran, R. Parthasarathy, R. Parthasarathy, S. Gollahalli, C. S. Gollahalli, University of Oklahoma, Attaphong, University of Oklahoma, Norman, Norman, OK Norman, Norman, OK Monday, 15 July 2013

40 38-GEPC-1 Propulsion Systems & Integration for Next Generation Vehicles (Invited) 210 F Chaired by: D. BENCHERGUI, Bombardier Inc and M. BRADLEY, Boeing Engineering Operations & Technology 1330 hrs 1400 hrs 1430 hrs 1500 hrs AIAA-2013-3678 AIAA-2013-3679 AIAA-2013-3680 AIAA-2013-3681 A Method for Reducing Sonic Boom Proton Exchange Membrane Fuel Cell Flight Test Results of an Efficient Propulsion, Power, and Strength by Tailoring the Shape of Systems for Airplane Auxiliary Power Axisymmetric Channeled Center- Thermal Management Integration the Propulsive Streamtube J. Pratt, L. Klebanoff, Sandia National body Supersonic Inlet at off Design R. Newman, M. Dooley, C. Lui, Northrop T. Conners, P. Henne, D. Howe, Gulfstream Laboratories, Livermore, CA; K. Munoz-Ramos, Conditions Grumman Corporation, Redondo Beach, CA Aerospace Corporation, Savannah, GA A. Akhil, Sandia National Laboratories, C. St. John, M. Frederick, NASA Dryden Albuquerque, NM; D. Curgus, Sandia National Flight Research Center, Edwards, CA Laboratories, Livermore, CA; B. Schenkman, Sandia National Laboratories, Albuquerque, NM Monday, 15 July 2013 39-GTE-7 Compressor III 210 B Chaired by: M. ATTIA, Embry-Riddle Aeronautical University 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3682 AIAA-2013-3683 AIAA-2013-3684 2D Investigation of the Flow Through 2D Investigation of the Flow Through Experimental Testing of a Dual a Symmetric Variable Inlet Guide a Symmetric Variable Inlet Guide Compression Rotor Vane, Part 1: Experimental Analysis Vane, Part 2: Numerical Analysis N. Grannan, University of Dayton Research D. Händel, S. Barthmes, R. Niehuis, University S. Barthmes, D. Händel, R. Niehuis, University Institute, Dayton, OH; J. Hoke, Innovative of the German Federal Armed Forces, Munich, of the German Federal Armed Forces, Munich, Scientific Solutions, Inc., Dayton, OH; Germany; U. Rockstroh, L. Leopold, MAN Germany; C. Wacker, J. Klausmann, MAN P. Litke, M. Dale, Air Force Research Diesel & Turbo SE, Berlin, Germany Diesel & Turbo SE, Berlin, Germany Laboratory, Wright-Patterson AFB, OH Monday, 15 July 2013 40-GTE-8 Turbine II 210 C Chaired by: I. HALLIWELL, Power Systems Manufacturing LLC 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3685 AIAA-2013-3686 AIAA-2013-3687 Power Turbine Blade Aerodynamic Numerical Study on Inter Turbine Effect of Periodic Pressure Pulses Optimization Using Non-Restrictive Ducts with Variable Curvature on Axial Turbine Performance Evolution Strategies Distribution M. Fernelius, S. Gorrell, Brigham Young D. Curriston, R. Hartfield, J. Burkhalter, V. Kuchana, Honeywell International, Inc., University, Provo, UT; J. Hoke, Innovative Auburn University, Auburn, AL Hyderabad, India; S. Guntu, B. Srinivasan, Scientific Solutions, Inc., Dayton, OH; F. Honeywell International, Inc., Bangalore, Schauer, Air Force Research Laboratory, India; P. Couey, C. Mckeever, M. Malak, Wright-Patterson AFB, OH Honeywell International, Inc., Phoenix, AZ Monday, 15 July 2013 41-GTE-9 Combustor I 210 D Chaired by: J. CONVERY, GE Aviation 1330 hrs 1400 hrs 1430 hrs 1500 hrs AIAA-2013-3688 AIAA-2013-3689 AIAA-2013-3690 AIAA-2013-3691 CFD Best Practices for Combustor Experimental Study of Gas Turbine Advanced Novel Jet Engines Stirred Reactor Approach for Design Using a Very Large Eddy Combustion with Elevated Fuel Emission Modelling to Predict NOX Cryoplane Engines’ NOX Prediction Simulation (VLES) Approach Temperatures & CO2 by Physics Based Model A. Prakash, Cranfield University, Cranfield, K. Ajmani, CFD Nexus, LLC, Cleveland, OH; H. H. Wiest, L. Larson, S. Heister, S. Meyer, A. Prakash, Cranfield University, Cranfield, United Kingdom Mongia, Purdue University, West Lafayette, IN; Purdue University, West Lafayette, IN United Kingdom P. Lee, Woodward FST, Inc., Zeeland, MI

41 Monday, 15 July 2013 42-GTE-10 Gas Turbine Engine Nozzles 211 A Chaired by: C. PERULLO 1330 hrs 1400 hrs AIAA-2013-3692 AIAA-2013-3693 A General Purpose Discrete Adjoint Experimental Study of Annular Formulation for Inviscid Flow Coaxial Jet with Hot Wire Nozzle Design Anemometry A. Dadone, G. Caramia, L. Catalano, J. Hodges, G. Natsui, M. Ricklick, J. Kapat, Technical University of Bari, Bari, Italy CATER, Orlando, FL Monday, 15 July 2013 43-HSABP-2 Numerical Analysis of Supersonic Combustion Systems, Scramjets I 210 H Chaired by: D. MUSIELAK, University of Texas at Arlington and B. SEKAR, USAF AFRL/RZTC 1330 hrs 1400 hrs 1430 hrs 1500 hrs AIAA-2013-3694 AIAA-2013-3695 AIAA-2013-3696 AIAA-2013-3697 Numerical Study on the Stability of Numerical Analysis of Solid Fuel Blowout Limits of Supercritical A Study of Numerical Simulation of the Supersonic Turbulent Lifted Flame Scramjet Operating at Mach 4 to 6 Kerosene in Supersonic Combustors Supersonic Conical Nozzle Exhaust using High Resolution Schemes L. Biao, Z. Wei, H. Chi, Beijing Institute of T. Zhang, J. Wang, L. Qi, Y. Yuan, J. Li, G. J. Mern, R. Agarwal, Washington J. Choi, Pusan National University, Busan, Technology, Beijing, China Yu, X. Fan, Chinese Academy of Sciences, University in St. Louis, St. Louis, MO South Korea; V. Yang, Georgia Institute of Beijing, China Technology, Atlanta, GA Monday, 15 July 2013 44-HSABP-3 Numerical Analysis of Supersonic Combustion Systems, Scramjets II 210 E Chaired by: R. MOEHLENKAMP, Aerojet Rocketdyne 1330 hrs 1400 hrs 1430 hrs 1500 hrs AIAA-2013-3698 AIAA-2013-3699 AIAA-2013-3700 AIAA-2013-3701 Hybrid RANS/LES Simulation of the Response of a Ramped Cavity to Ethylene Augmentation of JP- Air vitiation effects in scramjet Fuel Injection and Mixing Process in Shock-Induced Distortions in a 8+100 in a Supersonic Combustor engines a Supersonic Combustor with Cavity Mach 3 Freestream M. Bateup, University of Queensland, A. Agresta, University of Rome “La Flame-holder S. Peltier, Texas A&M University, College Brisbane, Australia Sapienza”, Rome, Italy; R. Andriani, J. Liang, C. Gong, S. Ming-bo, Z. Jin, Station, TX; J. Kirik, C. Goyne, University Technical University of Milan, Milan, Italy; National University of Defense Technology, of Virginia, Charlottesville, Charlottesville, F. Gamma, A. Ingenito, University of Rome Changsha, China VA; C. Carter, Air Force Research “La Sapienza”, Rome, Italy Laboratory, Wright-Patterson AFB, OH Monday, 15 July 2013 45-LP-2 Modeling and Simulation of Fluids 113 Chaired by: K. KREINER, The Boeing Company and M. NARAGHI, Manhattan Colege 1330 hrs 1400 hrs AIAA-2013-3702 AIAA-2013-3703 Numerical Simulation of a Construction of thermodynamic Cavitating flow using Unstructured properties look-up table with Hybrid Meshes adaptive finite element methods K. Yada, IHI Corporation, Yokohama, Z. Liu, J. Liang, Y. Pan, National University Japan; M. Sun, Tohoku University, of Defense Technology, Changsha, China Sendai, Japan; I. Inuzuka, M. Shito, IHI Corporation, Yokohama, Japan 42 Monday, 15 July 2013 46-LP-3 Injectors I 112 Chaired by: P. GLOYER, Gloyer-Taylor Laboratory and G. SAUNDERS, Jacobs Technology 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3704 AIAA-2013-3705 AIAA-2013-3706 Effects of orifice geometry on Impinging Atomization Enhanced Gas-on-Liquid Impinging Injectors : spray characteristics of impinging by Microjet Injection - effect, Some New Results jet injectors for gelled propellants mechanism and optimization - R. Prabhakaran, R. Basavanahalli, Indian Q. Fu, L. Yang, Beihang University, Beijing, C. Inoue, T. Watanabe, T. Himeno, S. Institute of Science, Bangalore, India China; F. Zhuang, Academy of Equipment Uzawa, University of Tokyo, Tokyo, Japan Command & Technology, Beijing, China Monday, 15 July 2013 47-PANEL-4 NASA SLS Development Exhibit Hall 3 1330 - 1530 hrs NASA’s Space Launch System (SLS) is America’s new exploration-class launch vehicle for missions beyond Earth’s orbit - taking astronauts where no one has been before, as well as offering unmatched mass and volume capabilities for science missions. The SLS Program is making maximum use of existing RS-25 core stage engines and advanced developmental hardware in the form of the 5-segment solid rocket booster and the J-2X upper stage engine, with a clear plan for beginning flight operations in 2017. SLS chief engineers will share plans and progress, as well as innovations being infused into the program, such as modifying the Delta IV kick stage to propel the Orion crew craft to trans-lunar injection. These government and industry partners will discuss how the team is solving development challenges and is on track to deliver a safe, affordable, and sustainable infrastructure asset to support America’s space agenda. Moderator: Garry Lyles, Space Launch System (SLS) Chief Engineer, NASA MSFC Panelists: Mat Bevill Brian Simmons Katherine Van Hooser Doug Bradley Rene Ortega Michael Wood SLS Booster Element Deputy Chief Engineer SLS Boosters Chief Engineer SLS Engines Element Chief Engineer RS-25 Chief Engineer SLS Spacecraft and Payload Integration SLS Chief Engineer NASA MSFC ATK NASA MSFC Aerojet Rocketdyne Chief Engineer The Boeing Company NASA MSFC Monday, 15 July 2013 48-PANEL-5 Emerging Pathways to Jet Fuel 212 D 1330 - 1530 hrs Moderator: Mark Bryden, Program Director, Ames National Laboratory Panelists: Prem Lobo Corinne Valkenburg Shane Flemming Jonathan Trent Blake Simmons Associate Director Engineer Chief Technical Advisor Project Scientist Bioengineering Senior Manager, Biomass Program Lead Center of Excellence for Aerospace Particulate Pacific Northwest National Laboratory Lanzatech NASA Sandia National Laboratories Emissions Reductions Research

Monday, 15 July 2013 49-PC-6 Fundamental Combustion Processes II 211 C Chaired by: C. CADOU, University of Maryland 1330 hrs 1400 hrs AIAA-2013-3707 AIAA-2013-3708 Burn Rate Characterization of Iso- Large Eddy Simulation Based Flame propyl Nitrate Blends: Part II Transition Modeling in a Lean A. Ambekar, L. Mallick, R. Gandhi, A. Premixed Swirl Combustor Chowdhury, Indian Institute of Technology B. Sen, Pratt & Whitney, East Hartford, Bombay, Mumbai, India; D. Radhakrishna, CT; G. Goldin, ANSYS, Inc., Lebanon, NH; S. Challa, Vehicle Research & Development K. Song, Y. Guo, R. McKinney, Pratt & Establishment, Ahmednagar, India Whitney, East Hartford, CT Monday, 15 July 2013

43 50-PC-7 Advanced Combustor Concepts II 231 Chaired by: M. POLANKA, US Air Force 1330 hrs 1400 hrs 1430 hrs 1500 hrs AIAA-2013-3709 AIAA-2013-3710 AIAA-2013-3711 AIAA-2013-3712 Computational Study of Pulsejet- Hot Jet Re-ignition of Hydrocarbons Integration Issues of an Ultra- Flame Structure Effects at High Driven Pressure Gain Combustors and Hydrogen in Air: Effect of Jet Compact Combustor to a Jet G-Loading at High-Pressure Chemical Activity Turbine Engine J. Wilson, M. Polanka, J. Miranda, Air S. Yungster, Ohio Aerospace Institute, A. Karimi, P. Chinnathambi, M. Rajagopal, M. Conrad, J. Wilson, M. Polanka, Air Force Institute of Technology, Wright- Cleveland, OH; D. Paxson, H. Perkins, NASA M. Nalim, Indiana University-Purdue Force Institute of Technology, Wright- Patterson AFB, OH Glenn Research Center, Cleveland, OH University Indianapolis, Indianapolis, IN Patterson AFB, OH Monday, 15 July 2013 51-PC-8 Spray Combustion I 230 A Chaired by: M. ANAND, Rolls-Royce Corporation 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3713 AIAA-2013-3714 AIAA-2013-3715 Combustion of Gelled Propellants Effects of NTO Oxidizer Convection Experimental Investigation of Containing Aluminum Particles Velocity and Pressure on the Atomization and Combustion of M. Negri, H. Ciezki, German Aerospace Combustion Characteristics of Gelled Propellant in High-pressure Center (DLR), Lampoldshausen, Germany UDMH Nonmetalized Organic Gel Oxidant Environment Droplet: Experimental Studies S. Feng, B. He, H. Haobo, L. Su, Z. Hou, W. Nie, B. He, F. Zhuang, Academy of W. Nie, Academy of Equipment Command Equipment Command & Technology, & Technology, Beijing, China Beijing, China Monday, 15 July 2013 52-PC-9 Combustion Modeling II 230 B Chaired by: J. OEFELEIN, Sandia National Laboratories 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3716 AIAA-2013-3717 AIAA-2013-3718 Theory and Analysis of Liquid- Modeling High-Density-Gradient A Numerical Study on Combustion Oxygen--Hydrogen Interface Flows at Supercritical Pressures Characteristics of Coaxial-Jet Dynamics in Liquid Rockets at G. Lacaze, J. Oefelein, Sandia National Injectors Using Scaling Techniques Supercritical Pressures Laboratories, Livermore, CA in a Subscale Chamber R. Dahms, J. Oefelein, Sandia National Y. Kim, C. Sohn, Sejong University, Seoul, Laboratories, Livermore, CA South Korea; S. Lee, Korea Aerospace Research Institute, Daejeon, South Korea Monday, 15 July 2013 53-PC-10 Detonations II 230 C Chaired by: C. BROPHY, Naval Postgraduate School 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3719 AIAA-2013-3720 AIAA-2013-3721 The Effects of Repetitively Pulsed Thermodynamic and Visualization Detonation engine development Nanosecond Discharges on Ignition Study of Shock Transfer in a Dual for reaction control systems of a Time in a Pulsed Detonation Engine Pulse Detonation-Crossover System spacecraft J. Lefkowitz, Y. Ju, Princeton University, R. Driscoll, A. St. George, D. Munday, K. Gawahara, H. Nakayama, J. Kasahara, Princeton, NJ; C. Stevens, Air Force E. Gutmark, University of Cincinnati, University of Tsukuba, Tsukuba, Japan; Institute of Technology, Wright-Patterson Cincinnati, OH S. Tomioka, T. Hiraiwa, Japan Aerospace AFB, OH; T. Ombrello, F. Schauer, Air Force Exploration Agency (JAXA), Kakuda, Japan

44 Research Laboratory, Wright-Patterson AFB, OH; J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH Monday, 15 July 2013 54-PC-11 Green Fuels I 210 G Chaired by: J. MURPHY, The Aerospace Corporation 1330 hrs 1400 hrs AIAA-2013-3722 AIAA-2013-3723 Recommended Figures of Merit for Solid ADN Propellant Development Green Monopropellants N. Wingborg, Swedish Defense Research W. Marshall, M. Deans, NASA Glenn Agency (FOI), Stockholm, Sweden Research Center, Cleveland, OH Monday, 15 July 2013 55-PC-12 High Speed Combustion 114 Chaired by: Y. DAIMON, Japan Aerospace Exploration Agency 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3724 AIAA-2013-3725 AIAA-2013-3726 Review of Numerical Modeling Characteristic Scales in Supersonic Mechanism of Combustion and Simulation Results Pertaining Combustion Instability Due to Flame-Vortex to High-speed Combustion in X. Li, X. Fan, Chinese Academy of Interactions in a Lean Premixed Scramjets Sciences, Beijing, China Gas Turbine Combustor R. Clark, S. Bade Shrestha, Western H. Lee, J. Lee, B. Quay, D. Santavicca, Michigan University, Kalamazoo, MI Pennsylvania State University, University Park, PA Monday, 15 July 2013 56-PP-1 Powering the Next Generation/Sustaining the Pipeline 211 D 1330 - 1530 hrs

Powering the Next Generation Sustaining the Pipeline Mark Lewis Dan Kirk Director, Science and Technology Policy Institute Associate Deprtment Head, Mechanical and Aerospace Engineering Department, Florida Institute of Technology

Interviews by Steven Howell, AIAA

The topics will include a discussion of policy issues for fostering and atrtracting the next generation of talented engineers into the work force, a national strategy on STEM education, the engineering pipeline and other issues related to engineering education. Monday, 15 July 2013 57-TM-2 Spacecraft and Lunar/Mars/Venus Surface Thermal Management I 212 B Chaired by: M. CHOI, NASA-Goddard Space Flight Center and S. SPENCER, Naval Research Laboratory 1330 hrs 1400 hrs 1430 hrs 1500 hrs AIAA-2013-3727 AIAA-2013-3728 AIAA-2013-3729 AIAA-2013-3730 Investigation of Insulation Numerical Analysis for Multi- Optical Test of a Cooled Focal Plane Thermal Control on the Sensitive Materials for Future Radioisotope layer Insulation (MLI) effect on Assembly in Hyper-Spectral Imager: Star Tracker of FORMOSAT-5 Power Systems (RPS) Spacecraft Thermal Control System Design, Integration, and Test of the Satellite: Design, Modeling and P. Cornell, F. Hurwitz, D. Ellis, K. Shaw, NASA A. Farag, E. Khalil, Cairo University, Cairo, HSI Prototype Developed in Taiwan Validation Glenn Research Center, Cleveland, OH; P. Egypt B. Wang, C. Chen, J. Tsai, G. Chang, National M. Chen, C. Wang, J. Huang, C. Chen, Schmitz, Alphaport, Inc., Cleveland, OH Space Organization, Hsinchu, Taiwan National Space Organization, Hsinchu, Taiwan Monday, 15 July 2013 45 58-NW-5 Networking Coffee Break Exhibit Hall 2 1530 - 1600 hrs Monday, 15 July 2013 59-SB-3 Speakers’ Briefing Individual Session Rooms 1530 - 1600 hrs Monday, 15 July 2013 60-ABPSI-5 Propulsion Aerodynamics Workshop I 211 B Chaired by: B. MCKAY, Lockheed Martin Aeronautics and C. CHUCK, The Boeing Company 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2013-3731 AIAA-2013-3732 AIAA-2013-3733 AIAA-2013-3734 AIAA-2013-3735 BCFD Analysis for the 1st AIAA 2D and 3D Performance Prediction Performance Prediction of Conical A CFD analysis of compressible flow Comparison of Participant Analyses Propulsion Workshop: Nozzle of a Convergent Nozzle at Nozzle using Navier-Stokes through convergent-conical nozzles with Experimental Results for Results Pressure Ratios from 1.4 to 7 and Computation N. Spotts, Colorado State University, Fort Conical Nozzle Flowfields and C. Winkler, A. Dorgan, The Boeing Comparison with Wind Tunnel Data H. Chen, Tsinghua University, Beijing, Collins, CO Performance Company, St. Louis, MO M. Attia, Embry-Riddle Aeronautical China R. Thornock, Self, Seattle, WA University, Daytona Beach, FL Monday, 15 July 2013 61-APS-2 Spacecraft Power Systems In-Orbit Performance 212 A & C Chaired by: G. CARR, Jet Propulsion Laboratory and J. WITCHER, Sandia National Laboratories 1600 hrs 1630 hrs AIAA-2013-3736 AIAA-2013-3737 Tabulation of Power-Related The Van Allen Probes Power System Satellite Failure Causes Launch and Early Mission Performance G. Landis, NASA Glenn Research Center, M. Butler, Johns Hopkins University Cleveland, OH Applied Physics Laboratory, Laurel, MD Monday, 15 July 2013 62-EERE-3 Gas 213 Chaired by: E. KHALIL, Cairo University; N. GHADDAR, American University of Beirut and D. MUTH, Idaho National Lab 1600 hrs 1630 hrs AIAA-2013-3738 AIAA-2013-3739 Effect of Oxygen enrichment on Laminar flame speed of Fossil/Air Acid Gas Combustion under Claus and Biofuels/Air Combustion Conditions A. Ingenito, University of Rome “La S. Ibrahim, H. Selim, University of Maryland, Sapienza”, Rome, Italy; R. Andriani, College Park, College Park, MD; A. AlShoaibi, Technical University of Milan, Milan, Italy; Petroleum Institute, Abu Dhabi, United Arab A. Agresta, F. Gamma, University of Rome Emirates; A. Gupta, University of Maryland, “La Sapienza”, Rome, Italy College Park, College Park, MD Monday, 15 July 2013

46 63-EERE-4 Solar Power 212 B Chaired by: E. KHALIL, Cairo University; N. GHADDAR, American University of Beirut and D. MUTH, Idaho National Lab 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3740 AIAA-2013-3741 AIAA-2013-3742 AIAA-2013-3743 Heat Transfer and Charge Transport A Correlation for Airflow Rate Modeling and Simulation of Solar A combined photovoltaic -thermal Characterization of Organic Wafering of Inclined and Vertical Solar Thermal Electric Energy and Water (PV-T) panel to minimize the with Photo-sensitive Mimosa pudica Chimneys Production Systems electrical and air conditioning Extract C. Chen, Columbia University, New York, S. Karaki, H. Ashkar, American University energy consumption of a typical M. Shitta, National Centre for Energy NY; M. Naraghi, Manhattan College, of Beirut, Beirut, Lebanon office in Beirut Efficiency and Conservation, Akoka, Nigeria; Riverdale, NY; P. Akbari, Columbia K. Ghali, S. Makarem, N. Ghaddar, S. E. Ogedengbe, University of Lagos, Akoka, University, New York, NY Karaki, American University of Beirut, Nigeria; E. Khalil, Cairo University, Cairo, Egypt Beirut, Lebanon Monday, 15 July 2013 64-GTE-14 Cooling and Leakages 210 D Chaired by: E. HENDRICKS, NASA 1600 hrs 1630 hrs AIAA-2013-3744 AIAA-2013-3745 Effect of Endwall Contouring in The Impact of Manufacturing presence of Upstream Leakage Flow Techniques on Film Cooling in a Transonic Turbine Blade Passage: Effectiveness Heat Transfer Measurements P. Johnson, M. Ricklick, J. Kapat, H. A. Roy, D. Blot, S. Ekkad, W. Ng, Virginia Zuniga, University of Central Florida, Polytechnic Institute and State University, Orlando, FL; G. Brown, Siemens Energy, Blacksburg, VA; A. Lohaus, M. Crawford, Inc., Jupiter, FL Siemens Energy, Inc., Orlando, FL Monday, 15 July 2013 65-HSABP-4 Analytical/Experimental Analysis of Hyper-/Supersonic Flow Path 210 E Chaired by: S. BECKEL, ATK Mission Systems 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3746 AIAA-2013-3747 AIAA-2013-3748 AIAA-2013-3749 Evaluation of Dual-Mode Methane Pyrolysis: literature Experimental Investigation of Velocimetry Measurements of a Combustor Characteristics with survey and comparisons of a Ramjet Combustor Using an Scramjet Cavity Flameholder with Inlet Vitiated and non-Vitiated Inflow available data for use in numerical Aluminized Gel Fuel Distortion J. Noda, Tohoku University, Sendai, Japan; simulations G. Gafni, A. Kuznetsov, D. Har-Lev, J. Kirik, C. Goyne, University of Virginia, S. Tomioka, N. Sakuranaka, T. Hiraiwa, N. Gascoin, University of Orléans, Bourges, B. Natan, Technion--Israel Institute of Charlottesville, Charlottesville, VA; S. Peltier, Japan Aerospace Exploration Agency France Technology, Haifa, Israel Texas A&M University, College Station, TX; (JAXA), Kakuda, Japan C. Carter, M. Hagenmaier, Air Force Research Laboratory, Wright-Patterson AFB, OH Monday, 15 July 2013 66-HSABP-5 Numerical Analysis of Dual Mode Supersonic Combustion 210 H Chaired by: E. AXDAHL, NASA Langley Research Center 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3750 AIAA-2013-3751 AIAA-2013-3752 AIAA-2013-3753 Fluid Transport brought by a Strut- Research on Mixing Characteristics Application of Evidence Theory on Unsteady Three-Dimensional Cowl System in a Scramjet Engine and Total Pressure Loss of the Jet in Dual Combustor Ramjet Model Phenomena in Mode-Transition S. Sato, Japan Aerospace Exploration Supersonic Crossflow J. Ahn, R. Starkey, Colorado University, Simulations of the HIFiRE-2 Agency (JAXA), Kakuda, Japan; M. Y. Zhao, J. Liang, Y. Zhao, J. Liu, National Boulder, CO Scramjet Flowpath Fukui, Space Service, Kakuda, Japan; University of Defense Technology, R. Yentsch, D. Gaitonde, Ohio State T. Watanabe, T. Munakata, Hitachi East Changsha, China University, Columbus, OH Japan Solutions, Sendai, Japan 47 Monday, 15 July 2013 67-LP-4 Liquid Rocket Engines I 111 Chaired by: C. GATTO, Jet Propulsion Laboratory 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3754 AIAA-2013-3755 AIAA-2013-3756 Design Verification Results of Tri-Gas RCS Thruster Performance Pulsed Chemical Rocket with Green Japanese 120N Bi-propellant Characterization High Performance Propellants thrusters (HBT-1) based on its first K. Pedersen, NASA Marshall Space A. Pasini, L. Torre, Alta S.p.A., Pisa, Italy; flight in HTV3 Flight Center, Huntsville, AL; V. Dorado, G. Pace, D. Valentini, L. d’Agostino, S. Takata, K. Sugimori, Y. Daimon, Japan University of Texas, El Paso, El Paso, TX; University of Pisa, Pisa, Italy Aerospace Exploration Agency (JAXA), Z. Grunder, B. Schaefer, University of Tsukuba, Japan; N. Matsuda, Y. Tashiro, Colorado, Boulder, Boulder, CO; M. Sung, IHI Corporation, Tomioka, Japan University of California, Irvine, Irvine, CA Monday, 15 July 2013 68-LP-5 Spacecraft Propulsion Systems 230 C Chaired by: S. BUSHMAN, JHU/Applied Physics Laboratory and A. FRANKEL, Moog Inc, ISP Division 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3757 AIAA-2013-3758 AIAA-2013-3759 AIAA-2013-3760 MESSENGER Propulsion System: Design and Testing of the Global Cold Gas Propulsion System for CubeSat High-impulse Adaptable Strategies for Orbit-Phase Propellant Precipitation Measurement Mission CNES Microscope spacecraft : Modular Propulsion System Extraction at Low Fill-Fractions Core Propulsion System presentation of the project and (CHAMPS) Product Line M. Wilson, C. Engelbrecht, Johns Hopkins M. Fiebig, C. Bacha, NASA Goddard Space development and verification plan Development Status and Mission University Applied Physics Laboratory, Laurel, Flight Center, Greenbelt, MD T. Lienart, K. Pfaab, French Space Agency Applications MD; D. Jaekle, PMD Technology, North (CNES), Toulouse, France R. Masse, C. Carpenter, D. Schmuland, J. Andover, MA Overly, M. Allen, Aerojet, Redmond, WA Monday, 15 July 2013 69-LP-6 Turbomachinery I 114 Chaired by: B. MARCU, SpaceX and D. RANSOM, Southwest Research Institute 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3761 AIAA-2013-3762 AIAA-2013-3763 A Comparison of 3-Bladed and Study on the Cavitating Flows in a Experimental Characterization of 4-Bladed Inducers at On and Off Turbopump Inducer the Dynamic Transfer Matrix of Design Flow Rates C. Choi, J. Kim, Korea Aerospace Research Cavitating Inducers R. Cluff, R. Lundgreen, S. Gorrell, D. Institute, Daejeon, South Korea G. Pace, University of Pisa, Pisa, Italy; L. Maynes, Brigham Young University, Provo, Torre, A. Pasini, Alta S.p.A., Pisa, Italy; UT; K. Oliphant, Concepts NREC, White D. Valentini, L. d’Agostino, University of River Junction, VT Pisa, Pisa, Italy Monday, 15 July 2013 70-NFF-1 Future Flight Propulsion Systems I 113 Chaired by: B. PALASZEWSKI, NASA Glenn Research Center and B. CASSENTI, University of Connecticut 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3764 AIAA-2013-3765 AIAA-2013-3766 An Analysis of Combined Thermal Atmospheric Mining in the Outer Extended Weight Measurements Protection and Thermal Propulsion Solar System: Resource Capturing, of Uncharged and Charged Systems for Aerogravity Assist Exploration, and Exploitation Spinning Gyroscopes in the Earth’s Vehicles B. Palaszewski, NASA Glenn Research Gravitational Field D. Murakami, NASA Ames Research Center, Cleveland, OH I. Lorincz, E. Edlinger, D. Hochwarter, C. Center, Moffett Field, CA Boy, M. Tajmar, Dresden University of Technology, Dresden, Germany 48 Monday, 15 July 2013 71-PANEL-6 High Power Electric Vehicles and Energy Storage 212 D 1600 - 1830 hrs Panel will address high power electric vehicles and energy storage. Moderators: Geoffrey Landis, Research Scientist, NASA Glenn Research Center and Edward Lewandowski, Research Engineer, NASA Glenn Research Center Panelists: Subbarao Surampudi Tim Collins Joseph Troutman Robert Baertsch Eric Lentz-Gauthier Program Manager Chief Executive Officer Chief Engineer Executive Vice President of Software Engineering Pilot NASA JPL Kleenspeed ABSL Space Products EnerSys Advanced Systems SkyTran Solar Flight

Monday, 15 July 2013 72-PANEL-7 Driving Mission Requirements and Technologies for Space Transportation - the Next Step after Space Shuttle 214 1600 - 1800 hrs The panel will highlight the overall driving mission requirements and technologies required to enable future human spaceflight and to status the tremendous recent progress and near-term future plans. Moderator: Paul Anderson, Director, Avionics, Orion Program, Lockheed Martin Space Systems Panelists: Kent Rominger Michael Wood Sam Wiley Larry Price Todd Mosher Vice President Chief Engineer, SLS Program Program Director of Human Space Deputy Program Manager, Orion Program Director of Dream Chaser Design and Development ATK Space Systems The Boeing Company Aerojet Rocketdyne Lockheed Martin Space Systems Sierra Nevada Monday, 15 July 2013 73-PANEL-8 Legacy RLV Systems DC-X Exhibit Hall 3 1600 - 1800 hrs The DC-X, or Delta Clipper Experimental, was an unmanned prototype of a reusable single stage to orbit launch vehicle built by McDonnell Douglas for the U.S. Strategic Defense Initiative Organization (SDIO) in the early 1990’s. Later, the system was transferred to NASA and upgraded with advanced operations, structures and propulsion technology and was renamed the DC-XA. The DC-X was never designed to achieve orbital altitudes or velocity, but instead to demonstrate the concept of vertical takeoff and landing using a revolutionary aircraft like operations approach. This session will discuss the lessons learned from the DC-X program and applicability to future space transportation systems. Moderator: Jess Sponable, Program Manager, DARPA Panelists: Peter Worden Tom Ingersoll Joaquin Castro Stephen Cook Director Chief Executive Officer Director, International Advanced Propulsion Programs Director of Space Technologies, NASA Ames Research Center Skybox Imaging Aerojet Rocketdyne Dynetics

Monday, 15 July 2013 74-PC-13 Advanced Combustor Concepts III 211 A Chaired by: Y. DAIMON, Japan Aerospace Exploration Agency 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3767 AIAA-2013-3768 AIAA-2013-3769 AIAA-2013-3770 Experimental and Numerical An Investigation on the Numerical Investigations of Small- Formulation And Testing Of A Investigations on Liner Cooling Performance of the Ramjet Size High Throughflow Speed Rocket Type Thruster Discharging Characteristics of a Trapped Vortex Trapped-vortex Combustor Combustors with Trapped-Vortex A Weight Combustor H. Xiaomin, Z. Jingyu, Nanjing University Concept D. Michaels, A. Gany, Technion--Israel Z. Jingyu, H. Xiaomin, J. Yi, W. Lu, of Aeronautics and Astronautics, Nanjing, S. Chen, R. Chue, T. Nguyen, S. Yu, Institute of Technology, Haifa, Israel Nanjing University of Aeronautics and China Nanyang Technological University, Astronautics, Nanjing, China Singapore, Singapore 49 Monday, 15 July 2013 75-PC-14 Fundamental Combustion Processes III 211 C Chaired by: L. MASSA, UT Arlington 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3771 AIAA-2013-3772 AIAA-2013-3773 Burning Characteristics of Liquid Experimental Study of Radiation-Induced Droplet Breakup Fuels with Suspensions of Energetic Impingement and Reaction of of Nano-Dispersed Coal-in-Water Nanoparticles: The Effect of Droplet Hypergolic Droplets Colloidal Fuels Size J. Forness, T. Pourpoint, S. Heister, Purdue J. Xu, L. Qiao, Purdue University, West S. Tanvir, L. Qiao, Purdue University, West University, West Lafayette, IN Lafayette, IN Lafayette, IN Monday, 15 July 2013 76-PC-15 Spray Combustion II 231 Chaired by: B. CHEHROUDI, European Research Council (ERC) 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3774 AIAA-2013-3775 AIAA-2013-3776 Effects of NTO Oxidizer Convection Studies on Spray in Crossflow for a Ignition and Combustion of Velocity and Pressure on the Cavity Combustor Isopropyl Nitrate Sprays Combustion Characteristics of A. Sinha, R. Ravikrishna, Indian Institute A. Ambekar, R. Bhangale, A. Dukale, R. UDMH Nonmetalized Organic Gel of Science, Bangalore, India Gandhi, A. Chowdhury, Indian Institute Droplet: Numerical Studies of Technology Bombay, Mumbai, India; B. He, W. Nie, F. Zhuang, Academy of D. Radhakrishna, S. Challa, Vehicle Equipment Command & Technology, Research & Development Establishment, Beijing, China Ahmednagar, India Monday, 15 July 2013 77-PC-16 Rocket Combustion Instability 230 A Chaired by: R. ERICKSON, The Aerospace Corporation 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3777 AIAA-2013-3778 AIAA-2013-3779 Stochastic Modeling of Transverse Development of Combustion A Conceptional Approach for the Wave Instability in a Liquid Response Functions in a Subscale Prediction of Thermoacoustic Propellant Rocket Engine High Pressure Longitudinal Stability in Rocket Engines P. Popov, A. Sideris, W. Sirignano, Combustor M. Schulze, M. Schmid, D. Morgenweck, University of California, Irvine, Irvine, CA M. Wierman, W. Anderson, Purdue S. Köglmeier, T. Sattelmayer, Technical University, West Lafayette, IN University of Munich, Munich, Germany Monday, 15 July 2013 78-PC-17 Combustion Diagnostics 230 B Chaired by: K. MCMANUS, GE 1600 hrs 1630 hrs AIAA-2013-3780 AIAA-2013-3781 On the Use of OH* Radiation as a Study of LOx/H2 Spray Flame Marker for the Heat Release Rate Response to Acoustic Excitation in a in High-Pressure Hydrogen Liquid Rectangular Rocket Combustor Rocket Combustion J. Hardi, M. Oschwald, German Aerospace T. Fiala, T. Sattelmayer, Technical Center (DLR), Lampoldshausen, Germany; University of Munich, Munich, Germany B. Dally, University of Adelaide, Adelaide, Australia

50 Monday, 15 July 2013 79-PC-18 Green Fuels II and Microscale Combustion 210 G Chaired by: M. COIL, Orbital Technologies Corporation 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3782 AIAA-2013-3783 AIAA-2013-3784 Burn Rate Characterization of Iso- Experimental Evaluation of New PRECISE - preliminary results of the propyl Nitrate Blends: Part I Ionic Liquid Fuels MEMS-based µCPS A. Ambekar, L. Mallick, R. Gandhi, M. Coil, Orbital Technologies Corporation, M. Gauer, German Aerospace Center (DLR), A. Chowdhury, Indian Institute of Madison, WI Göttingen, Germany; D. Telitschkin, U. Gotzig, Technology Bombay, Mumbai, India; EADS, Ottobrunn, Germany; Y. Batonneau, D. Radhakrishna, S. Challa, Vehicle National Center for Scientific Research Research & Development Establishment, (CNRS), Poitiers, France; P. Rangsten, Ahmednagar, India 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 Monday, 15 July 2013 80-PC-19 Combustion Modeling III 112 Chaired by: J. MURPHY, The Aerospace Corporation 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3785 AIAA-2013-3786 AIAA-2013-3787 Bluff Body Flame Holder with Flow Study on Combustion Dynamic Modeling the Effect of Condensed- Entrainment Using Perforated Plate Characteristics of Oxygen-Rich phase Contributions in Ammonium S. Tanaka, K. Takahashi, J. Hosoi, IHI Preburners Perchlorate Based Composite Solid Corporation, Mizuho, Japan; M. Uchida, I. Moon, S. Kang, S. Lee, Korea Aerospace Propellants IHI Corporation, Yokohama, Japan Research Institute, Daejeon, South Korea; F. Retief, J. Knoetze, G. Smit, Stellenbosch S. Seo, Hanbat National University, University, Stellenbosch, South Africa; C. Daejeon, South Korea Rousseau, Rheinmetall Denel Munition, Somerset West, South Africa Monday, 15 July 2013 81-SR-1 Motor Design and Plume Effects 211 D Chaired by: R. BLACK, Aerojet Rocketdyne and M. LANGHENRY, Raytheon Missile Systems 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3788 AIAA-2013-3789 AIAA-2013-3790 Solid Rocket Motor Design Using a Rapid Solid Rocket Motor Design Prediction of In-flight Radio Frequency Modified Ant Colony Optimization G. Smit, J. Knoetze, Stellenbosch University, Attenuation by a Rocket Plume by Metaheuristic with Local Search Matieland, South Africa; F. Steyn, C. Rousseau, Applying CFD/FDTD Coupling Capability Rheinmetall Denel Munition, Somerset K. Kinefuchi, K. Okita, I. Funaki, T. Abe, Z. Kiyak, R. Hartfield, Auburn University, West, South Africa; E. De Kock, Stellenbosch Japan Aerospace Exploration Agency Auburn, AL University, Matieland, South Africa (JAXA), Tsukuba, Japan 51 Monday, 15 July 2013 82-NW-6 Tech Museum of Innovation Off-Site Reception Off-Site 1830 - 2000 hrs Monday, 15 July 2013 83-SB-4 Speakers’ Briefing Individual Session Rooms 1830 - 1900 hrs Monday, 15 July 2013 84-ABPSI-6 Propulsion Aerodynamics Workshop II 211 B Chaired by: B. MCKAY, Lockheed Martin Aeronautics 1900 hrs 1930 hrs 2000 hrs 2030 hrs 2100 hrs 2130 hrs Oral Presentation (Invited) AIAA-2013-3792 AIAA-2013-3793 AIAA-2013-3794 AIAA-2013-3795 AIAA-2013-3796 Introduction to the Air Breathing BCFD Analysis for the 1st AIAA Inlet CFD Results: Comparison of Pressure-based Coupled Simulation CFD Simulation for S-Duct Test Case A Comparison of Several CFD Propulsion Invited Session on Propulsion Workshop: S-Duct Solver, Turbulence Model, Grid of Pressure Recovery and Distortion Using Overset Grids Codes with Experimental Data in a Diffusing S-Duct Prediction and Results Density, and Topology in an S-Duct L. Gea, The Boeing Company, Huntington Diffusing S-Duct Validation A. Dorgan, C. Winkler, The Boeing N. Domel, D. Baruzzini, Lockheed Martin S. Kumar, ANSYS, Inc., Hinjewadi, India Beach, CA A. Delot, ONERA, Meudon, France; R. B. McKay, AIAA ABPSI TC, Mercer Island, WA Company, Hazelwood, MO Corporation, Fort Worth, TX Scharnhorst, The Boeing Company, St. Louis, MO Tuesday Tuesday, 16 July 2013 85-NW-7 Tuesday Networking Coffee & Pastries Exhibit Hall 2 0700 - 0800 hrs Tuesday, 16 July 2013 86-PLNRY-2 Propulsion and Power Systems of the Future Exhibit Hall 1 0800 - 0900 hrs Keynote Address Henner Wapenhans Head of Technology Strategy, Rolls-Royce Group plc Tuesday, 16 July 2013 87-PLNRY-3 A New Industrial Revolution for a Sustainable Energy Future 212 A & C 0800 - 0900 hrs Access to affordable and reliable energy has been a cornerstone of the world’s increasing prosperity and economic growth since the beginning of the industrial revolution. Our use of energy in the twenty-first century must also be sustainable. This talk will provide a techno- economic snapshot of the current energy landscape and identify several research and development opportunities and challenges to create the foundation for this new industrial revolution. Keynote Address Arun Majumdar Director of Energy Initiatives, Google Tuesday, 16 July 2013 88-NW-8 Networking Coffee Break Exhibit Hall 2 0900 - 1000 hrs Tuesday, 16 July 2013 89-SB-5 Speakers’ Briefing Individual Session Rooms 0930 - 1000 hrs

52 Tuesday, 16 July 2013 90-ABPSI-7 Propeller Systems 210 E Chaired by: J. LITT, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3797 AIAA-2013-3798 AIAA-2013-3799 AIAA-2013-3800 Influence of a Planetary CFD computation of in-plane Active Flow Control for Interaction Assessment of Advanced Grid Differential Gear on Counter propeller shaft loads Noise Reduction of Contra-Rotating Strategies for Aero-Acoustics on Rotating Fan Performance L. Ruiz-Calavera, D. Perdones-Diaz, Airbus, Open Rotors Open Rotor Applications T. Otten, T. Lengyel-Kampmann, E. Nicke, Getafe, Spain R. Akkermans, A. Stuermer, J. Delfs, N. Ben Nasr, B. Ortun, ONERA, Meudon, German Aerospace Center (DLR), Cologne, German Aerospace Center (DLR), France; A. Chelius, S. Canard-Caruana, Germany Braunschweig, Germany ONERA, Châtillon, France Tuesday, 16 July 2013 91-APC-3 Advanced Concepts and Planning 210 F Chaired by: R. CHASE, Booz Allen Hamilton and J. ROBINSON, Retired f/Boeing 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3801 AIAA-2013-3802 AIAA-2013-3803 AIAA-2013-3804 Long Term Space Objectives Using Commercial Space with Technology Advanced Space Transportation ISRU Propellant Selection for Space Optonal Roadmaps Maturation Concepts and Propulsion Technologies Exploration Vehicles E. Henderson, R. Rhodes, J. Robinson, R. Rhodes, Self, Cape Canaveral, FL; for a New Delivery Paradigm T. Chen, NASA Marshall Space Flight Self, Dickinson, TX C. McCleskey, NASA Kennedy Space J. Robinson, Propellant Supply Technology, Center, Huntsville, AL; D. Thorpe, Thortek Center, Cape Canaveral, FL; J. Robinson, Seal Beach, CA; C. McCleskey, R. Rhodes, Labs, Inc., Irvine, KY Propellant Supply Technology, Seal NASA Kennedy Space Center, Cape Canaveral, Beach, CA FL; R. Lepsch, NASA Langley Research Center, Hampton, VA; T. Chen, NASA Marshall Space Flight Center, Huntsville, AL; C. Joyner, Pratt & Whitney, West Palm Beach, FL; D. Levack, Pratt & Whitney, Canoga Park, CA Tuesday, 16 July 2013 92-APS-4 Hybrid Power Systems 212 B Chaired by: M. LIFFRING, Boeing Commercial Airplanes 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3805 AIAA-2013-3806 AIAA-2013-3807 AIAA-2013-3808 Energy Optimization of an Aircraft Hybrid-Electric Propulsion Systems Performance Analysis of Fan- Flywheel Energy Recovery and Focused on Component Sizing and for Aircraft Driving Electric Motors in a Fuel- Storage System from Aircraft Control Architecture Interactions C. Friedrich, P. Robertson, University of Cell Hybrid Powered Propulsion Brakes R. Roberts, D. Decker, Wright State Cambridge, Cambridge, United Kingdom System for Aviation M. Conteh, E. Nsofor, Southern Illinois University, Dayton, OH K. Okai, H. Fujiwara, Japan Aerospace University, Carbondale, IL Exploration Agency (JAXA), Tokyo, Japan; H. Nomura, Nihon University, Chiba, Japan; T. Tagashira, R. Yanagi, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan Tuesday, 16 July 2013 93-EC-4 Cooling 212 A & C Chaired by: G. LANDIS, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3809 AIAA-2013-3810 AIAA-2013-3811 4 kW Power Thermoacoustic Stirling The Research on Flow Capacity of Characteristics of Thermoacoustic Heat Engine Test Results Capillary Pump in the AMTEC Sound Generator and Its Application to M. Haberbusch, C. Nguyen, J. Ickes, T. C. Zhou, Z. Song, Harbin Engineering Refrigerator Hui, Sierra Lobo, Inc., Milan, OH University, Harbin, China N. Maruyama, Y. Iwasaki, M. Saito, Y. Kitaide,

53 Mie University, Tsu, Japan; K. Takiguchi, S. Ishida, Fuji Electric, Yokkaichi, Japan; T. Tsuchiya, M. Hirota, Mie University, Tsu, Japan Tuesday, 16 July 2013 94-EC-5 Stirling System Testing 212 D Chaired by: T. CHAN, Lockheed Martin Space Systems 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3812 AIAA-2013-3813 AIAA-2013-3814 Test Program for Advanced Stirling Performance Measurement of Small Radioisotope Power System Radioisotope Generator Hardware Advanced Stirling Convertors Testing at NASA Glenn Research at NASA Glenn Research Center (ASC-E3) Center E. Lewandowski, M. Dolloff, S. Oriti, M. Roth, S. Oriti, NASA Glenn Research Center, G. Dugala, NASA Glenn Research Center, NASA Glenn Research Center, Cleveland, OH Cleveland, OH Cleveland, OH Tuesday, 16 July 2013 95-ECS-1 Ignition Characterization and Analysis 210 A Chaired by: L. YANG and D. JACKSON, ATK Space Systems 1000 hrs 1100 hrs 1130 hrs AIAA-2013-3815 AIAA-2013-3816 AIAA-2013-3817 Ignition Transfer Effectiveness from Primers to Physically Separated Characterization of PVU-2/A An Experimental and Numerical Study Pyrotechnic Boosters Percussion Primer Output Energy on Exploding Foil Initiators (EFIs) L. Yang, Self, La Canada Flintridge, CA H. Lee, Chemring Energetic Devices, S. Koc, M. Yilmaz, ROKETSAN Missile Downers Grove, IL; M. Bichay, Naval Industries, Inc., Ankara, Turkey; A. Ulas, Surface Warfare Center, Indian Head, MD; Middle East Technical University, Ankara, J. Baglini, Exodynamics Technology, Inc., Turkey; B. Kizilkaya, ROKETSAN Missile Phoenix, AZ Industries, Inc., Ankara, Turkey Tuesday, 16 July 2013 96-EERE-5 Sustainable Energy Solutions 214 Chaired by: E. KHALIL, Cairo University; N. GHADDAR, American University of Beirut and D. MUTH, Idaho National Lab 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3818 AIAA-2013-3819 AIAA-2013-3820 XPrize 100mpge City-Highway Math Group Maximum Power Tracking Effective Desiccant Model for Electric-Hybrid Competition among Distributed Power Sources Dehumidification System with Vehicles K. Siri, The Aerospace Corporation, El Two-Stage Evaporative Cooling for F. Wyczalek, Energy Independence Segundo, CA Hot and Humid Climates Foundation, Bloomfield Hills, MI; M. K. Ghali, M. Hourani, N. Ghaddar, Wyczalek, General Motors Corporation, American University of Beirut, Beirut, Warren, MI; T. Wyczalek, Magna Exteriors and Lebanon Interiors, Novi, MI Tuesday, 16 July 2013 97-EP-1 Electrospray Propulsion I 210 B Chaired by: M. GAMERO, University of California, Irvine and T. COLES 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3821 AIAA-2013-3822 AIAA-2013-3823 AIAA-2013-3824 Numerical Simulation of Colloid In situ study of ionic liquid Taylor Electrospray from an Ionic Liquid Fabrication of Electrospray Thrusters Thrusters and Taylor Cone-Jets cones using electron microscopy Ferrofluid utilizing the Rosensweig by Sintering Glass Microspheres A. Borner, P. Wang, Z. Li, D. Levin, K. Terhune, L. King, Michigan Technological Instability J. Xie, M. Canonica, P. Lozano, Massachusetts Pennsylvania State University, University University, Houghton, MI E. Meyer, L. King, Michigan Technological Institute of Technology, Cambridge, MA Park, PA University, Houghton, MI Tuesday, 16 July 2013 54 98-EP-2 Plasma Thruster Modeling I 210 C Chaired by: D. KING, Aerojet 1000 hrs AIAA-2013-3825 Three Dimensional Simulation of Ion Thruster Plumes with AMR and Parallelization Strategies B. Korkut, P. Wang, Z. Li, D. Levin, Pennsylvania State University, State College, PA Tuesday, 16 July 2013 99-EP-3 Helicon Thrusters 112 Chaired by: M. WALKER, Georgia Institute of Technology and T. LIU, University of Michigan 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3828 AIAA-2013-3829 AIAA-2013-3830 Comparison of Plasma Disgnostics Development of Superconducting Numerical and Experimental for an Argon and Helium Gas Magnets for a Helicon Plasma Measurements in a Helicon-IEC Helicon Thruster Thruster Thruster A. Faust, R. Sedwick, University of J. Vitucci, R. Sedwick, University of A. Krishnamurthy, B. Ulmen, G. Chen, P. Maryland, College Park, College Park, MD Maryland, College Park, College Park, MD Keutelian, G. Miley, University of Illinois, Urbana-Champaign, Urbana, IL Tuesday, 16 July 2013 100-HR-2 Swirling Oxidizer Flows 210 D Chaired by: S. CLAFLIN, Pratt & Whitney Rocketdyne and B. MADHANABHARATAM, Space Propulsion Group, Inc. 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3831 AIAA-2013-3832 AIAA-2013-3833 AIAA-2013-3834 Small-Scale Hybrid Rocket Test Stand Development of a Counter-Rotating Flash Pyrolysis of High Density UAH Tactical Missile System Design & Characterization of Swirl Injectors Vortex Pair (CVP) Mixer for PolyEthylene of a Surface to Air Missile for M. Summers, Arizona State University, Aerospace Applications N. Gascoin, University of Orléans, Bourges, Missile Defense Tempe, AZ; J. Dennis, Purdue University, West J. Park, S. Heister, J. Sullivan, Purdue France M. Hitt, L. Kalathas, J. Coogan, N. Lafayette, IN; J. Villarreal, Raytheon Company, University, West Lafayette, IN Slegers, University of Alabama, Huntsville, Tucson, AZ Huntsville, AL Tuesday, 16 July 2013 101-HSABP-6 Hypersonic Air-Breathing Propulsion Concepts 231 Chaired by: D. MUSIELAK, University of Texas at Arlington 1000 hrs AIAA-2013-3835 Minimizing Corner Interactions Generated By Oblique Shock Waves In Supersonic Inlets By Optimization Methods B. Lee, University of California, Santa Barbara, Santa Barbara, CA; M. Liou, NASA Glenn Research Center, Cleveland, OH

55 Tuesday, 16 July 2013 102-ITAR-1 Liquid Rocket Propulsion/Solid Rocket Propulsion/System Concepts and Supporting Propulsion Technologies (ITAR Restricted Session) 210 H Chaired by: D. SHAFER, GE Aviation and H. ORAVEC, Univeristy of Akron 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3836 AIAA-2013-3837 AIAA-2013-3838 AIAA-2013-3839 Design, Development and Testing Solid Rocket Motor Nozzle Material The Mechanical and Sealing Development of Propellant of the Antares Pogo Suppressor Performance (ITAR Restricted Performance of an Atomic Oxygen Feed, Thrust Measurement, and (ITAR Restricted Paper) Paper) Pretreated Subscale Candidate Automation Controls Systems for D. Ransom, Southwest Research Institute, A. Cortopassi, J. Boyer, Pennsylvania State Silicone Elastomer Docking Seal Testing LOX/LCH4 Reaction Control San Antonio, TX; B. Winters, Orbital University, University Park, PA; H. Martin, (ITAR Restricted Paper) Thrusters (ITAR Restricted Paper) Sciences Corporation, Dulles, VA ; K. Kuo, Pennsylvania State University, H. Oravec, N. Garafolo, C. Daniels, A. Acosta-Zamora, A. Choudhuri, University University Park, PA University of Akron, Akron, OH of Texas, El Paso, El Paso, TX Tuesday, 16 July 2013 103-LP-7 Rocket Nozzles 211 C Chaired by: V. AHUJA, CRAFT Tech and D. KIRK, Florida Institute of Technology 1000 hrs 1030 hrs AIAA-2013-3840 AIAA-2013-3841 Flow Separation in Rocket Nozzles Transitional Behavior of Dual Bell - An Overview Nozzles: Contour Optimization R. Stark, German Aerospace Center (DLR), C. Genin, R. Stark, D. Schneider, German Lampoldshausen, Germany Aerospace Center (DLR), Lampoldshausen, Germany Tuesday, 16 July 2013 104-LP-8 Propellant Storage and Management I 211 A Chaired by: B. WINTERS, Orbital Sciences Corporation and D. SARGENT, Federal Aviation Administration 1000 hrs 1030 hrs AIAA-2013-3842 AIAA-2013-3843 Analytical Sloshing Model and CFD Numerical Analysis on Boiling Analysis for the Exomars Mission Flow in Surface Tension Dominant M. Lazzarin, A. Bettella, M. Manente, Environment HIT09, Padova, Italy; R. Da Forno, MDA, Y. Umemura, T. Himeno, T. Watanabe, Treviso, Italy University of Tokyo, Tokyo, Japan Tuesday, 16 July 2013 105-LP-9 Modeling and Simulation of Engine Heat Transfer I 230 A Chaired by: K. KREINER, The Boeing Company 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3844 AIAA-2013-3845 AIAA-2013-3846 Cooling Analysis for Rocket Engine Numerical evaluation of heat Comparison of Finite Element Combustion Chamber with High exchange mechanism by slit analysis and experimental results Fidelity Simulation resonators of a combustion chamber type TMF D. Watanabe, K. Imai, A. Ogawara, Mitsubishi Y. Morii, K. Kuzuu, T. Shimizu, Japan panel test Heavy Industries, Ltd., Komaki, Japan; K. Aerospace Exploration Agency (JAXA), J. Riccius, W. Bouajila, E. Zametaev, Kawatsu, H. Negishi, Y. Daimon, N. Tani, Sagamihara, Japan German Aerospace Center (DLR), N. Yamanishi, H. Sunakawa, A. Kurosu, T. Lampoldshausen, Germany Kobayashi, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan

56 Tuesday, 16 July 2013 106-LP-10 Green Propellant Infusion Mission (GPIM) 230 B Chaired by: T. POURPOINT, Purdue University and S. MILLER, Aerojet 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3847 AIAA-2013-3848 AIAA-2013-3849 AIAA-2013-3850 Green Propellant Infusion Mission Implementation of the Green Green Propellant Infusion Mission Green Propellant Infusion Mission Program Overview Propellant Infusion Mission (GPIM) Propulsion System Development Plume Impingement Analysis C. McLean, Ball Aerospace & Technologies on a Ball Aerospace BCP-100 R. Spores, Aerojet, Redmond, WA J. Yim, B. Reed, NASA Glenn Research Corporation, Boulder, CO Spacecraft Bus Center, Cleveland, OH; C. McLean, Ball W. Deininger, Ball Aerospace & Aerospace & Technologies Corporation, Technologies Corporation, Boulder, CO Boulder, CO Tuesday, 16 July 2013 107-LP-11 Injectors II 211 D Chaired by: E. BESNARD, California State University-Long Beach 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3851 AIAA-2013-3852 AIAA-2013-3853 Experimental Studies of Uni- Combustion Characteristics on a Investigation of a Single Injector with element Shear Coaxial Injectors for Coaxial-Porous Injector Applied High Frequency Pressure LOX/CH4 Propulsion Research D. Kim, G. Lee, I. Lee, J. Koo, Korea Disturbances For Applications To Liquid J. Flores, L. Sanchez, A. Choudhuri, V. Aerospace University, Goyang, South Korea Rocket Engine Combustion Instabilities Dorado, University of Texas, El Paso, El J. Bennewitz, D. Lineberry, R. Frederick, Paso, TX University of Alabama, Huntsville, Huntsville, AL Tuesday, 16 July 2013 108-PANEL-9 Emerging Technologies for the Next Generation of Aircraft Systems Exhibit Hall 3 1000 - 1200 hrs The panelists will discuss government and industry perspectives on emerging aircraft systems technologies for the next generation. Moderator: David Eames, Director, NASA Programs and Advanced System Studies, Rolls-Royce Corporation Panelists: Fayette Collier Ron Kawai Kenneth Martin Michael Winter Project Manager, Environmentally Responsible Aviation Project Propulsion Specialist Manager-Conceptual Design Chief Engineer for Technology NASA Langley Research Center Boeing Research and Technology Lockheed Martin Corporation Pratt & Whitney

Tuesday, 16 July 2013 109-PP-2 Dealing with the Changing Aerospace Business Environment: A Commercial Aviation Perspective 230 C 1000 - 1200 hrs Jim Peterson Director of Engineering for Propulsion Systems Division Boeing Commercial Airplanes Interview by Guy Norris, Senior Editor, Aviation Week Tuesday, 16 July 2013 110-SCP-2 Spacecraft Thrusters 211 B Chaired by: A. REISZ, Reisz Engineers 1000 hrs 1030 hrs 1100 hrs AIAA-2013-3854 AIAA-2013-3855 AIAA-2013-3856 57 Design of a Cold-Gas The construction of the life prediction Improved Design and Micropropulsion system for LISA model of 1N and 4N monopropellant Characterization of MicroNewton Pathfinder thrusters Torsional Balance Thrust Stand G. Morris, Astrium, Stevenage, United G. Fujii, D. Goto, H. Kagawa, S. Murayama, A. Cofer, S. Heister, A. Alexeenko, Purdue Kingdom; C. Edwards, ESA, Noordwijk, The K. Kajiwara, Japan Aerospace Exploration University, West Lafayette, IN Netherlands Agency (JAXA), Ibaraki, Japan; H. Ikeda, N. Shinozaki, E. Yabuhara, IHI Corporation, Gunma, Japan Tuesday, 16 July 2013 111-SCP-3 Advanced Seals Session I 210 G Chaired by: B. STEINETZ, NASA Glenn Research Center and N. SARAWATE, GE Global Research 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation (Invited) Oral Presentation (Invited) AIAA-2013-3859 AIAA-2013-3860 Overview of Advanced Seals Turbomachinery Sealing Technology Design, Manufacture And Testing The Design and Performance Challenges and Opportunities - Survey of Past Success and Of Variable Bristle Diameter Brush Evaluation of a Novel Air/oil B. Steinetz, P. Dunlap, NASA Glenn Strategy for Future Development Seals Separator for Use in a Miniature Jet Research Center, Cleveland, OH; N. J. Kirk, General Electric Company, X. Zheng, G. Lu, M. Mack, D. Trivedi, Engine Sarawate, General Electric Company, Cincinnati, OH N. Sarawate, C. Wolfe, General Electric E. Topal, TUSAS Engine Industries, Inc., Niskayuna, NY Company, Schenectady, NY Eskisehir, Turkey; S. Acarer, Izmir Institute of Technology, Izmir, Turkey; T. Kirgiz, TUSAS Engine Industries, Inc., Eskisehir, Turkey Tuesday, 16 July 2013 112-SR-2 Nozzle Materials and Slag accumulation 111 Chaired by: M. BERDOYES, Herakles and R. ELLIS 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3861 AIAA-2013-3862 AIAA-2013-3863 AIAA-2013-3864 Investigation of Slag Accumulation Analyzing ablative and combustion HERAKLES thermal-structural An Investigation of Compressive in Solid Rocket Motors characteristics of thermoplastic composite materials boost rocket and Shear Strength of Char from C. JasperLal, P. Sridharan, K. Krishnaraj, V. polyurethane nanocomposites nozzle performance Polymer Nanocomposites for Srinivasan, Vikram Sarabhai Space Centre, D. Wong, M. Jaramillo, J. Koo, University A. Lacombe, HERAKLES, Le Haillan, France Propulsion Applications Thiruvananthapuram, India of Texas, Austin, Austin, TX; H. Stretz, M. Jaramillo, J. Koo, University of Texas, P. Ambuken, Tennessee Technological Austin, Austin, TX University, Cookeville, TN; D. Pinero, University of Texas, Austin, Austin, TX Tuesday, 16 July 2013 113-SR-3 Combustion Instability 114 Chaired by: D. GREATRIX, Ryerson University and C. ROUSSEAU, Denel (Pty) Ltd. 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3865 AIAA-2013-3866 AIAA-2013-3867 AIAA-2013-3868 Biglobal Stability of Compressible Biglobal Stability of Compressible ARIANE 5 MPS ARTA 5 bench firing POD-X Program: towards the SRM Flowfields. Part 1: Planar Flowfields. Part 2: Application to test: evolution of third segment Pressure Oscillation Demonstrator first Formulation Solid Rocket Motors Integrated Frontal Thermal firing test M. Akiki, J. Batterson, J. Majdalani, M. Akiki, J. Batterson, J. Majdalani, Protection and impact on pressure G. Mastrangelo, T. Morillon, University of Tennessee Space Institute, University of Tennessee Space Institute, oscillations phenomena EUROPROPULSION, Suresnes, France; D. Tullahoma, TN Tullahoma, TN E. Bucci, Avio S.p.A., Colleferro, Italy Scoccimarro, E. Lambiase, Avio S.p.A., Colleferro, Italy; E. Gautronneau, L. Paradis, 58 L. Guenot, HERAKLES, Bordeaux, France; P. Planquart, von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium; N. Cesco, P. Supie’, French Space Agency (CNES), Paris, France; J. Breteau, ESA, Paris, France Tuesday, 16 July 2013 114-TM-3 Aerospace and Terrestrial Power Systems Thermal Management I 213 Chaired by: C. TARAU, Advanced Cooling Technologies and S. SPENCER, Naval Research Laboratory 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-3869 AIAA-2013-3870 AIAA-2013-3871 AIAA-2013-3872 Thermal Energy Storage for a Dish Spray-Cooling for Wind-Based Testing of Thermal Energy Storage Design and Production Stirling Concentrated Solar Power Compressed Air Energy Storage for a Dish-Stirling Concentrated of Composite Structures: System C. Qin, E. Loth, University of Virginia, Solar Power System Thermoplastic Wind Turbine Blades J. Thayer, Thermacore, Inc., Lancaster, PA; Charlottesville, Charlottesville, VA; P. Li, R. Galbraith, Infinia Corporation, Ogden, R. Amano, L. Forsythe, P. Mohan Das, R. Galbraith, Infinia Corporation, Ogden, T. Simon, J. Van De Ven, University of UT; S. Qiu, Temple University, Philadelphia, University of Wisconsin, Milwaukee, UT; J. Rosenfeld, C. Dyson, Thermacore, Minnesota, Minneapolis, Minneapolis, MN; S. PA Milwaukee, WI Inc., Lancaster, PA Crane, A. Pourmousa, LightSail Energy, Inc., Oakland, CA Tuesday, 16 July 2013 115-NW-9 IECEC Awards Luncheon Exhibit Hall 1 1200 - 1400 hrs Woodrow Whitlow Associate Administrator for Mission Support Directorate, NASA Tuesday, 16 July 2013 116-SB-6 Speakers’ Briefing Individual Session Rooms 1230 - 1300 hrs Tuesday, 16 July 2013 117-ABPSI-8 Integrated Propulsion and Configuration 210 E Chaired by: C. GAHARAN, Lockheed Martin Corporation 1300 hrs 1330 hrs 1400 hrs AIAA-2013-3873 AIAA-2013-3874 AIAA-2013-3875 Characteristics of Bio-Ethanol Fueled Electrical Propulsion: Flying Test Bed Design of a 5 Kilogram Solar- GG-cycle Air Turbo Ramjet Engine for Platform Development and System Powered Unmanned Airplane for Supersonic UAV along Flight Trajectory Level Simulation Perpetual Solar Endurance Flight R. Minato, K. Mizobata, K. Higashino, N. H. SMAOUI, E. Joubert, M. Lotufo Lopes, S. Montgomery, N. Mourtos, San Jose Tanatsugu, Muroran Institute of Technology, EADS, Suresnes, France; D. Esteyne, Aéro State University, San Jose, CA Muroran, Japan Composites Saintonge (ACS), Royan, France Tuesday, 16 July 2013 118-APC-4 Advanced Space Propulsion Concepts I 210 F

59 Chaired by: T. CHEN, NASA 1300 hrs 1330 hrs 1400 hrs AIAA-2013-3876 AIAA-2013-3877 AIAA-2013-3878 The Challenges of Ambient Plasma Ion Electrospray Propulsion System Magnetoplasma Sail with Equatorial Wave Propulsion Feasibility Study for various Ring-current J. Gilland, G. Williams, Ohio Aerospace Satellite Missions and Architectures I. Funaki, Japan Aerospace Exploration Agency Institute, Brookpark, OH S. Arestie, C. Whitlock, P. Lozano, (JAXA), Sagamihara, Japan; Y. Kajimura, Massachusetts Institute of Technology, Akashi National College of Technology, Cambridge, MA Akashi, Japan; Y. Ashida, H. Yamakawa, Kyoto University, Uji, Japan; H. Nishida, Tokyo University of Agriculture and Technology, Koganei, Japan; Y. Oshio, Graduate University for Advanced Studies, Sagamihara, Japan; K. Ueno, I. Shinohara, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; H. Yamamura, Y. Yamagiwa, Shizuoka University, Hamamatsu, Japan Tuesday, 16 July 2013 119-EP-4 Electrospray Propulsion II 210 B Chaired by: L. KING, Michigan Technological University and C. COFFMAN 1300 hrs 1330 hrs 1400 hrs AIAA-2013-3879 AIAA-2013-3880 AIAA-2013-3881 Characterization of a CubeSat The Expansion of Colloid Thruster Physical Limitations on the Lifetime compatible magnetically levitated Beams and its Dependence on of Ionic Liquid Ion Sources thrust balance for electrospray Emission Temperature N. Brikner, P. Lozano, Massachusetts propulsion systems M. Gamero, University of California, Irvine, Institute of Technology, Cambridge, MA F. Hicks, L. Perna, C. Coffman, P. Lozano, Irvine, CA Massachusetts Institute of Technology, Cambridge, MA Tuesday, 16 July 2013 120-EP-5 Plasmas in Propulsion 211 B Chaired by: E. CHOUEIRI, Princeton University and M. BOSS, European Aeronautic Defence and Space Company 1300 hrs 1330 hrs AIAA-2013-3882 AIAA-2013-3883 Development of a Green Propellant Numerical Simulations of a Beating Station-Keeping Thruster using a Electrostatic Wave Powered Dielectric Barrier Discharge Magnetic Null Thruster P. Saripalli, R. Sedwick, University of M. Feldman, E. Choueiri, Princeton Maryland, College Park, College Park, MD University, Princeton, NJ Tuesday, 16 July 2013 121-EP-6 Plasma Thruster Modeling II 211 C Chaired by: L. BRIEDA, Particle In Cell Consulting LLC and T. MATLOCK 1300 hrs 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3885 AIAA-2013-3886 AIAA-2013-3887 AIAA-2013-3888 The Effectiveness of Magnetic Validation of Fully-Kinetic Particle- Hybrid-PIC modeling of a high- Modeling Ion Thruster Shielding in High-Isp Hall Thrusters in-Cell Model Optimized for Multi- voltage, high-specific-impulse Hall Contamination: from Grid Erosion I. Mikellides, Jet Propulsion Laboratory, thruster Adaptability thruster to Thruster Plume California Institute of Technology, A. Pang, L. Boulanger, Massachusetts B. Smith, I. Boyd, University of Michigan, D. Han, J. Wang, University of Southern Pasadena, CA Institute of Technology, Cambridge, MA; Ann Arbor, Ann Arbor, MI; H. Kamhawi, California, Los Angeles, CA Y. Raitses, Princeton University, Princeton, NASA Glenn Research Center, Cleveland, NJ; M. Martinez-Sanchez, Massachusetts OH Institute of Technology, Cambridge, MA Tuesday, 16 July 2013 60 122-EP-7 Ion Engines I 211 D Chaired by: D. GOEBEL, Jet Propulsion Laboratory and B. SMITH 1300 hrs 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3889 AIAA-2013-3890 AIAA-2013-3891 AIAA-2013-3892 Numerical Life Qualification of NEXT Ion Engine Plume Deposition Expanded Throttling Capabilities of Annular Engine Development Ion Thruster’s Ion Optics using the Rates: QCM Measurements the NEXT Thruster Status JIEDI Tool M. Crofton, J. Nocerino, J. Young, The M. Patterson, G. Soulas, NASA Glenn M. Patterson, NASA Glenn Research H. Watanabe, Japan Aerospace Exploration Aerospace Corporation, El Segundo, CA; Research Center, Cleveland, OH; J. Young, Center, Cleveland, OH; J. Foster, University Agency (JAXA), Sagamihara, Japan; M. M. Patterson, G. Soulas, NASA Glenn M. Crofton, The Aerospace Corporation, El of Michigan, Ann Arbor, Ann Arbor, MI; Nakano, Tokyo Metropolitan College of Research Center, Cleveland, OH Segundo, CA J. Young, M. Crofton, The Aerospace Industrial Technology, Arakawa-Ku, Japan; Corporation, El Segundo, CA Y. Kajimura, Akashi National College of Technology, Akashi, Japan; I. Funaki, R. Takaki, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Tuesday, 16 July 2013 123-HR-3 Internal Ballistics Modeling II 210 D Chaired by: J. MAJDALANI, University of Tennessee Space Institute and B. MADHANABHARATAM, Space Propulsion Group, Inc. 1300 hrs 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3893 AIAA-2013-3894 AIAA-2013-3895 AIAA-2013-3896 Three-dimensional Numerical Optical Investigation of the Numerical model for hybrid rocket Combustion Instability Involving Simulation of Two-phase Flow in Combustion Process in Paraffin- internal ballistic Vortex Shedding in Hybrid Rocket Hybrid Rocket Motor based Hybrid Rocket Fuels D. Fedele, F. Ponti, University of Bologna, Motors X. Li, H. Tian, N. Yu, G. Cai, Beihang M. Kobald, H. Ciezki, S. Schlechtriem, Forlì, Italy; A. Annovazzi, Avio S.p.A., D. Pastrone, M. Codegone, C. Novara, University, Beijing, China German Aerospace Center (DLR), Colleferro, Italy; R. Bertacin, University of Technical University of Turin, Turin, Italy Hardthausen, Germany Bologna, Forlì, Italy Tuesday, 16 July 2013 124-HR-4 Novel Motor Operating Conditions I 211 A Chaired by: S. WHITMORE, Utah State University and K. HORI, Japan Aerospace Exploration Agency (JAXA) 1300 hrs 1330 hrs 1400 hrs AIAA-2013-3897 AIAA-2013-3898 AIAA-2013-3899 Numerical Investigation of Hybrid Advanced CFD Investigation for Hybrid Rocket Propulsion and Rocket Combustion Chamber Predicting Regression Rate in In-Situ Propellant Production for Transient Behavior Hybrid Rockets Future Mars Missions F. Barato, M. Faenza, D. Pavarin, A. Bettella, M. Lazzarin, M. Faenza, D. Pavarin, A. A. Boiron, B. Cantwell, Stanford University, N. Bellomo, University of Padua, Padua, Italy Bettella, A. Englaro, University of Padua, Stanford, CA Padova, Italy Tuesday, 16 July 2013 125-HSABP-7 Innovative Scramjet Concepts (Invited Session) 231 Chaired by: H. HASSAN, North Carolina State University and E. AXDAHL, NASA Langley Research Center 1300 hrs 1330 hrs 1400 hrs AIAA-2013-3900 AIAA-2013-3901 AIAA-2013-3902 Mitigation of Autoignition Due to Excitation Modes of Ramp Injectors A numerical study of flow and Premixing in a Hypervelocity Flow for Supersonic Combustion Engines flame dynamics in a hydrocarbon- Using Active Wall Cooling L. Massa, University of Texas, Arlington, fueled dual-combustion ramjet E. Axdahl, A. Kumar, NASA Langley Research Arlington, TX L. Zhang, V. Yang, Georgia Institute of Center, Hampton, VA; A. Wilhite, National Technology, Atlanta, GA; H. Sung, Korea Institute of Aerospace, Hampton, VA Aerospace University, Goyang, South Korea Tuesday, 16 July 2013

61 126-LP-12 Propellant Storage and Management II 210 C Chaired by: D. GUADAGNOLI, Orbital Sciences Corporation and G. GRAYSON, Boeing Defense, Space & Security 1300 hrs 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3903 AIAA-2013-3904 AIAA-2013-3905 AIAA-2013-3906 Update on SPHERES-Slosh for Cryogenic Propellant Management Passive Phase Separation in Experimental Investigation on Acquisition of Liquid Slosh Data Sounding Rocket Experiments on Cryogenic Upper Stage Tanks Heat Exchange and Pressure Drop aboard the ISS TEXUS 48 P. Behruzi, J. Klatte, G. Netter, Astrium, Enhanced by Vertical Sloshing S. Chintalapati, C. Holicker, R. Schulman, P. Behruzi, J. Klatte, N. Fries, A. Schuette, Bremen, Germany T. Himeno, D. Haba, K. Ishikawa, Y. B. Wise, G. Lapilli, H. Gutierrez, D. Kirk, B. Schmitz, H. Koehler, Astrium, Bremen, Umemura, C. Inoue, T. Watanabe, Florida Institute of Technology, Melbourne, Germany University of Tokyo, Tokyo, Japan; S. FL Nonaka, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Tuesday, 16 July 2013 127-LP-13 Modeling and Simulation of Engines and Propulsion Systems 230 A Chaired by: P. ALLIOT, Snecma S.A. 1300 hrs 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3907 AIAA-2013-3908 AIAA-2013-3909 AIAA-2013-3910 An End-to-End High Fidelity Numerical Computational Prediction of the Modelling and Simulation of ATV Characteristics of Expander Bleed Simulation of the LE-X Engine - Thrust Characteristics of a Small Pressure Control Assembly Slam Cycle and Full Expander Cycle Influence of Coolant Leakage on Thruster at Low Pressure Condition Start C. Sezaki, A. Ogawara, Mitsubishi Heavy Engine Power Balance - J. Ahn, D. Lee, Sejong University, Seoul, F. Di Matteo, M. De Rosa, M. Marchionni, Industries, Ltd., Nagoya, Japan N. Tani, K. Ogura, N. Yamanishi, H. Negishi, South Korea ESA, Noordwijk, The Netherlands H. Sunakawa, T. Kobayashi, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan Tuesday, 16 July 2013 128-LP-15 Liquid Propulsion History I: LOX/HC Propulsion I: Goddard - Peenemuende - Sputnik (8K71PS/8A91 R-7), Vanguard, Juno 1 to Titan, Atlas, Falcon and Beyond 230 B 1300 - 1500 hrs Chaired by: K. PUGMIRE, Spincraft and B. AUSTIN, IN Space LLC More than a ‘history session’: In 1922 Robert H. Goddard selected his alternative rocket concept, proposed independently by Hermann Oberth in Germany and also noted by Konstantin E. Tsiolkovsky, a liquid-fuel rocket with two lines running into its combustion chamber feeding a liquid hydrocarbon and liquid oxygen. By 1926 he had tested the first liquid fueled engine and on March 16, 1926, Goddard flight-tested a gasoline/LOX rocket. Lessons Learned from the Past Can Be Stepping Stones to a Greater Capability for Propulsion and Will Help Shape Our Future Directions L. Caveny

Introduction and Comments - Goddard, Oberth, Konstantin E. Tsiolkpvsky Robert L. Sackheim

Peenemuende Roots and Lessons Viking-Vanguard (X-405) and Redstone-Juno 1 David RS-27, MD-1, MA-5A -7, LR-89 -105, H-1, F-1, S-3D, RS-84 (Atlas, European Experience Dietrich Haeseler Christensen, Robert L. Sackheim Delta, Thor, Saturn 1B & V, Jupiter) Dieter Preclik Steve Bouley, Brian Anderson

Tuesday, 16 July 2013 129-NFF-4 Fusion and Alternative Nuclear Concepts I 113 Chaired by: R. SEDWICK, University of Maryland and E. DAVIS, Institute for Advanced Studies at Austin 1300 hrs 1330 hrs 1400 hrs AIAA-2013-3911 AIAA-2013-3912 AIAA-2013-3913 Confinement Mechanisms and A Particle-in-cell Simulation for Propellantless Propulsion with Fusion Propulsion the Traveling Wave Direct Energy Negative Matter Generated by High A. Taits, CDI Corporation, Jupiter, FL Converter (TWDEC) for Fusion Electrostatic Potentials

62 Propulsion M. Tajmar, Dresden University of A. Chap, University of Maryland, College Park, Technology, Dresden, Germany College Park, MD; J. Scott, NASA Johnson Space Center, Houston, TX; A. Tarditi, Electric Power Research Institute, Inc., Knoxville, TN Tuesday, 16 July 2013 130-PANEL-10 Disruptive Aircraft & Propulsion Technologies for the Future Exhibit Hall 3 1300 - 1500 hrs The Panelists will discuss government and industry perspective on disruptive technologies that will yield alternative propulsion cycles in a not distant future. Moderators: David Eames, Director, NASA Programs and Advanced System Studies, Rolls-Royce Corporation Panelists: Marty Bradley Dale Carlson John Kusnierek Nateri Madavan Technical Fellow General Manager Technology Strategy Director, Business Development Deputy Project Scientist, Fixed Wing Project Boeing Research and Technology GE Aviation Rolls-Royce North American Technologies, Inc. NASA Ames Research Center

Tuesday, 16 July 2013 131-PP-3 Dealing with the Changing Aerospace Business Environment: A Military Aviation Perspective 230 C 1300 - 1500 hrs Alton Romig VP and General Manager of Advanced Development Programs, Skunk Works Lockheed Martin Corporation Interview by Guy Norris, Senior Editor, Aviation Week Tuesday, 16 July 2013 132-SCP-4 Advanced Seals Session II 210 G Chaired by: B. STEINETZ, NASA Glenn Research Center and P. DUNLAP, NASA Glenn Research Center 1300 hrs 1330 hrs 1400 hrs Oral Presentation (Invited) AIAA-2013-3914 AIAA-2013-3915 Characterizing Multi-Scale Transient Simulations of Elastomer Seal Coatings for Viscoelasticity of Polymers : A Rotordynamic Problems with Adhesion Mitigation and Protection Transient Sealing Perspective Whirling Motion from Ultraviolet Radiation A. Thatte, General Electric Company, C. Kannepalli, V. Ahuja, A. Hosangadi, H. de Groh, B. Puleo, NASA Glenn Niskayuna, NY Combustion Research and Flow Research Center, Cleveland, OH Technology, Inc., Pipersville, PA Tuesday, 16 July 2013 133-SR-4 Flow Effects in Solid Rocket Motors 111 Chaired by: B. LEARY, Johns Hopkins University Applied Physics Laboratory and E. CAVALLINI, University of Roma “La Sapienza” 1300 hrs 1330 hrs 1400 hrs 1430 hrs AIAA-2013-3916 AIAA-2013-3917 AIAA-2013-3918 AIAA-2013-3919 Asymptotic Adaptation of the Implementation of an Internal Laminar-Turbulent Transition Characterization of Particle Taylor-Culick Mean Flow Profile to Ballistics Module in OpenFOAM® Investigation in a Solid Rocket Motor Trajectories in Solid Rocket Motors Rockets with Non-Circular Grain E. De Kock, G. Smit, University of Representative Cold Flow Setup J. Majdalani, A. Katta, T. Barber, University Perforations Stellenbosch, Stellenbosch, South Africa; B. Gazanion, French Space Agency (CNES), of Tennessee Space Institute, Tullahoma, J. Majdalani, University of Tennessee C. Rousseau, Rheinmetall Denel Munition, Paris, France; F. Chedevergne, X. de Saint TN; B. Maicke, Pennsylvania State Space Institute, Tullahoma, TN Somerset West, South Africa; A. Steenkamp, Victor, J. Estivalezes, G. Casalis, ONERA, University, Harrisburg, PA Flamengro, Pretoria, South Africa Toulouse, France Tuesday, 16 July 2013 63 134-ST-1 Space Transportation I 112 Chaired by: M. SIR, The Aerospace Corporation 1300 hrs 1330 hrs 1400 hrs AIAA-2013-3920 AIAA-2013-3921 AIAA-2013-3922 SLS Capabilities to Support an An In-Line Reusable Launch Vehicle Study on Alternative Cargo Launch Earth-Moon L-Point Node for Lunar Concept Using Confined Load- Options from the Lunar Surface Missions Bearing Frozen Propellants C. Blomberg, University of Colorado, B. Donahue, The Boeing Company, A. Baran, M. Anderson, J. Auxt, Louisiana Boulder, Boulder, CO; Z. Zulkefli, Case Huntsville, AL State University, Baton Rouge, LA Western University, Cleveland, OH; S. Rich, University of Washington, Seattle, Seattle, WA; S. Howe, Center for Space Nuclear Research, Idaho Falls, ID Tuesday, 16 July 2013 135-SB-7 Speakers’ Briefing Individual Session Rooms 1400 - 1430 hrs Tuesday, 16 July 2013 136-APS-3 Advanced Space Power Generation Designs & Status 212 A & C Chaired by: J. HAINES, Retired - formerly ESA/ESTEC and A. BAISDEN, JHU/Applied Physics Laboratory 1430 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Keynote Address AIAA-2013-3923 AIAA-2013-3924 AIAA-2013-3925 AIAA-2013-3926 Energy Conversion Initiatives at Regenerative Fuel Cell for High NASA’s Radioisotope Power Systems Multi Mission Radioisotope Effect of Pressure Recovery on Lockheed Martin Power Space System Applications Program Status Thermoelectric Generator (MMRTG) Triple Spool Turbofan Engine E. Allen, Lockheed Martin Corporation, S. Okaya, IHI Corporation, Tomioka, Japan L. Dudzinski, NASA Headquarters, Performance Data and Application Performance Bethesda, MD Washington, DC; J. Hamley, T. Sutliff, to Life Modeling E. Khalil, Cairo University, Cairo, Egypt; J. Zakrajsek, P. McCallum, NASA Glenn T. Hammel, R. Bennett, R. Sievers, S. E. AbdelGhany, Aviation Institute, Cairo, Research Center, Cleveland, OH Keyser, Teledyne Energy Systems, Inc., Egypt; M. Fouad, Cairo University, Cairo, Hunt Valley, MD; W. Otting, L. Gard, Pratt Egypt; A. El-Sayed, Zagazig University, & Whitney, Canoga Park, CA Zagazig, Egypt Tuesday, 16 July 2013 137-EC-6 Thermoelectric Devices and Systems 212 D Chaired by: J. FLEURIAL, Jet Propulsion Lab; S. BUX, Jet Propulsion Laboratory and J. SCHREIBER, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2013-3927 AIAA-2013-3928 AIAA-2013-3929 AIAA-2013-3930 AIAA-2013-3931 Engineering of Novel Development of High Efficiency Life Validation of Advanced, High 1 kW Small Fission Heat Pipe-cooled Simulation Analysis of the High- Thermoelectric Materials and Segmented Thermoelectric Couples Efficiency Thermoelectric Materials Thermoelectric Power System Design power Thermoelectric Generation Devices for Next Generation, Long T. Caillat, S. Firdosy, B. Li, C. Huang, V. and Components Concept and Technology Maturat System Based on Strong Coupling Life, 20% Efficient Space Power Ravi, N. Keyawa, H. Anjunyan, J. Paik, T. Caillat, J. Paik, C. Huang, J. Fleurial, Jet J. Fleurial, J. Chase, P. Gogna, S. Firdosy, B. Mechanism Systems D. Uhl, J. Chase, L. Lara, J. Fleurial, Jet Propulsion Laboratory, California Institute Li, N. Keyawa, G. Nakatsukasa, B. Nesmith, Z. Zhang, Y. Chen, South China University J. Fleurial, S. Bux, T. Caillat, Jet Propulsion Propulsion Laboratory, California Institute of Technology, Pasadena, CA Jet Propulsion Laboratory, California Institute of of Technology, Guangzhou, China of Technology, Pasadena, CA 64 Laboratory, California Institute of Technology, Pasadena, CA Technology, Pasadena, CA Tuesday, 16 July 2013 138-TFES-2 Combustion 213 Chaired by: K. BRYDEN, Iowa State University; B. KHANDELWAL, The University of Sheffield and A. CHOUDHURI, University of Texas at El Paso 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3932 AIAA-2013-3933 AIAA-2013-3934 AIAA-2013-3935 AIAA-2013-3936 AIAA-2013-3937 Characterization of Swirling Flame Temperature and Species Some Fluid Dynamic Aspects of Numerical and Experimental Study Experimental Analysis on Emission Comparison of Jet Fuel produced Distributed Combustion Calculations with an Excel/VBA Fires of the Effect of Momentum-Flux Production and Performance of by Shale oil and Biomass: A. Khalil Hasan, A. Gupta, University of Computer Code for General Fuel-Air D. Lilley, Lilley & Associates, Stillwater, OK Ratio on Temperature Uniformity in Stressed 100 % SPK, Stressed Fully Manufacturing, Emission and Maryland, College Park, College Park, MD Combustion the Combustor Formulated Synthetic Jet Fuel, Jet Performance D. Lilley, Lilley & Associates, Stillwater, OK R. Amano, A. Gupta, M. Ibrahim, B. A-1 in a Small Gas Turbine Engine V. Shankar, B. Khandelwal, S. Blakey, C. Wiegand, University of Wisconsin, B. Khandelwal, E. Ubogu, M. Akram, S. Wilson, University of Sheffield, Sheffield, Milwaukee, Milwaukee, WI Blakey, C. Wilson, University of Sheffield, United Kingdom Sheffield, United Kingdom Tuesday, 16 July 2013 139-TM-4 Heating and Cooling of Buildings I 212 B Chaired by: E. KHALIL, Cairo University and J. DARKWA, University of Nottingham-Ningbo 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3938 AIAA-2013-3939 AIAA-2013-3940 AIAA-2013-3941 AIAA-2013-3942 AIAA-2013-3943 AIAA-2013-3944 Effect of Horizontal Projections in Load Shape Extrapolation and Multiple Thermal Simulation and Evaluation PCM Solar Energy Storage for Outlook of Innovative Energy Energy Modelling of District Cooling Numerical Investigations of Flow Vertical Separation of Windows Regression of Energy Stocks within the of a Double Skin Façade System High-Efficiency Energy Utilization Efficient Designs of Low Carbon Plant in Egypt Patterns and Thermal Comfort in M. Ibrahim, October 6 University, 6th of University of Lagos J. Darkwa, Y. Lin, University of in Buildings Buildings E. Khalil, M. Fouad, H. Safwat, E. Abuo Air-Conditioned Lecture Room October City, Egypt A. Bakare, E. Ogedengbe, University of Lagos, Nottingham, Ningbo, China O. Alajo, E. Nsofor, V. Ibekwe, Southern E. Khalil, J. Jarman, Cairo University, ElKassem, Cairo University, Cairo, Egypt T. Abou-deif, E. Khalil, Cairo University, Akoka, Nigeria Illinois University, Carbondale, IL Cairo, Egypt Cairo, Egypt Tuesday, 16 July 2013 140-TM-5 Heating and Cooling of Buildings II 214 Chaired by: E. KHALIL, Cairo University and J. DARKWA, University of Nottingham-Ningbo 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2013-3945 AIAA-2013-3946 AIAA-2013-3947 AIAA-2013-3948 Effect of Fire Location on Effect of Fire Heat Release Rate on Effect of Window Configurations on Potential of Solar Applications in Temperature, Velocity, Visibility and Temperature, Velocity, Visibility and Fire Spread in Buildings Residential Buildings in the Gulf CO Concentration Distributions in CO Concentration Distributions in M. Ibrahim, A. Sharaf ELDin, October 6 Countries Under Ground Tunnel Under Ground Tunnel University, 6th of October City, Egypt; R. Farhat, American University of Beirut, A. Bayomy, E. ElBialy, E. Khalil, A. A. Bayomy, E. ElBialy, E. Khalil, A. M. Fayek AbdRabbo, Benha University, Beirut, Lebanon; W. Chakroun, Kuwait Medhat, Cairo University, Cairo, Egypt Medhat, Cairo University, Cairo, Egypt Cairo, Egypt; A. Mostafa Ayoub, Egyptian University, Kuwait, Kuwait; N. Ghaddar, University for Administration Science and K. Ghali, American University of Beirut, Technology, Cairo, Egypt Beirut, Lebanon Tuesday, 16 July 2013 141-NW-10 Networking Coffee Break Exhibit Hall 2 1500 - 1600 hrs Tuesday, 16 July 2013 142-SB-8 Speakers’ Briefing Individual Session Rooms 1530 - 1600 hrs Tuesday, 16 July 2013 143-ABPSI-9 Engine Systems Integration II 210 E Chaired by: N. HERRING, United Technologies Research Center 65 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2013-3949 AIAA-2013-3950 AIAA-2013-3951 AIAA-2013-3952 AIAA-2013-3953 Three dimensional numerical Fluidic Throat Choking in a Application of Back-Step Coanda Elimination of the Horse Shoe The Effects of Freestream investigation of the clustered linear Convergent-Divergent Nozzle Flap for the Supersonic Co-flowing Vortex in Axial Turbine Vane Turbulence on Serpentine Diffuser aerospike nozzle’s flow affected R. Starkey, University of Colorado, Fluidic Thrust Vector Control Cascades via Airfoil Shape Distortion Patterns by changing the distance between Boulder, Boulder, CO Y. Lee, M. Song, H. Chang, Korea Optimization J. Johnson, Brigham Young University, neighboring cell nozzles Aerospace University, Koyang, South M. Attia, S. Manoharan, V. Shulman, Provo, UT; W. Copenhaver, Air Force T. Miyazawa, A. Matsuo, Keio University, Korea; Y. Cho, Microfriend, Seoul, South Embry-Riddle Aeronautical University, Research Laboratory, Wright-Patterson Yokohama, Japan; H. Takahashi, T. Korea Daytona Beach, FL; L. Lachmann, Altran AFB, OH; S. Gorrell, Brigham Young Tomita, S. Tomioka, Japan Aerospace Technology, Paris, France University, Provo, UT Exploration Agency (JAXA), Kakuda, Japan Tuesday, 16 July 2013 144-APC-5 Advanced Rocket Propulsion Concepts II 210 F Chaired by: J. ROBINSON, Retired f/Boeing 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3954 AIAA-2013-3955 AIAA-2013-3956 Proposed Flight Research of a Dual- Advanced Design of a Multi- Performance Analysis of an Bell Rocket Nozzle Using the NASA Thruster LOX/Propylene Aerospike Integrated Multi-Mode Chemical F-15 Airplane Engine Monopropellant Inductive Plasma D. Jones, T. Bui, NASA Dryden Flight Research J. Meiss, E. Besnard, California State Thruster Center, Edwards, CA; J. Ruf, NASA Marshall University, Long Beach, CA S. Berg, J. Rovey, Missouri University of Space Flight Center, Huntsville, AL Science and Technology, Rolla, MO Tuesday, 16 July 2013 145-CS-1 Propulsion Challenges for Commercial Reusable Space Vehicles 210 A 1600 - 1830 hrs Moderator: Bruce Pittman, NASA Space Portal/Emerging Space Office Panelists: Frank Zegler Tom Mueller Tim Pickens Greg Mungas Senior Staff Advanced Programs Vice President of Propulsion Development Chief Propulsion Engineer CEO and Founder ULA SpaceX Moon Express Firestar Technologies

Tuesday, 16 July 2013 146-ECS-2 Energetic Devices - Modeling and Analysis 112 Chaired by: H. LEE, Chemring Energetic Devices 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3957 AIAA-2013-3958 AIAA-2013-3959 AIAA-2013-3960 Numerical Characterization of Ignition Threshold Energy Structural Analysis of Solid Aerospace Ordnance Evolution Detonator Performance in an Determination for Reactive Propellant Grain using Explicit Overview Explosive Bolt Device Materials Using a Pneumatic Dynamics Method for Ignition J. Scott, United Launch Alliance, H. Lee, Chemring Energetic Devices, Impact Testing Appartus Pressurization Centennial, CO Downers Grove, IL G. Knowlton, P. Martellaro, Reactive R. Hsiao, Pacific Scientific Energetic Metals International, Inc., King of Materials Company, Hollister, CA Prussia, PA Tuesday, 16 July 2013 147-EDU-1 Engineering Education in a New Fiscal Reality 230 C 66 1600 - 1800 hrs Moderator: Daniel Kirk, Associate Department Head, Mechanical and Aerospace Engineering Department, Florida Institute of Technology Panelists: Scott Hubbard Gary Kawahara Don Jaekle Michael Winter Professor VP & General Manager Owner Chief Engineer for Technology Stanford University ATK Commerce MD Technologies Pratt & Whitney

Tuesday, 16 July 2013 148-EP-8 Micropropulsion I 210 B Chaired by: E. PENCIL, NASA Glenn Research Center and D. FEILI, Giessen University 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3961 AIAA-2013-3962 AIAA-2013-3963 Micro-Cathode Arc Thruster (mCAT) Bimodal Propulsion System Using Measurements and Analysis of Weakly updated design and performance Ionic Liquid Propellant for Pico- and Ionized Plasma in a Permanent D. Chiu, G. Teel, T. Zhuang, A. Shashurin, Nano-satellite Applications Magnet Cusp within the region Near M. Keidar, George Washington University, K. Masuyama, P. Lozano, Massachusetts the Anode Surface Washington, DC Institute of Technology, Cambridge, MA B. Dankongkakul, S. Araki, R. Wirz, University of California, Los Angeles, Los Angeles, CA Tuesday, 16 July 2013 149-HR-5 Paraffin Fuels I 210 D Chaired by: D. PASTRONE, Politecnico di Torino and J. DAVITIAN, The Aerospace Corporation 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3964 AIAA-2013-3965 AIAA-2013-3966 AIAA-2013-3967 Kinetic Modelling of High Density Methodologies for Detailed Performance of Dicyclopentadiene Development and Testing of a PolyEthylene Pyrolysis: Part 2. Chemistry Computation, Application (DCPD)/Gaseous Oxygen Based Green Monopropellant Ignition Reduction of existing detailed to Hybrid Rocket Combustion Hybrid Rocket Propellants with System mechanism Chamber Simulations Pyrophoric Fuel Additives S. Whitmore, D. Merkley, M. Judson, S. N. Gascoin, University of Orléans, Bourges, N. Gascoin, University of Orléans, Bourges, S. Shark, C. Zaseck, T. Pourpoint, S. Son, S. Eilers, Utah State University, Logan, UT France France Heister, Purdue University, West Lafayette, IN Tuesday, 16 July 2013 150-HR-6 Paraffin Fuels II 211 A Chaired by: A. KARABEYOGLU, Space Propulsion Group Inc. and S. COOGAN, Southwest Research Institute 1600 hrs 1630 hrs 1700 hrs AIAA-2013-3968 AIAA-2013-3969 AIAA-2013-3970 Characterization and Evaluation of Kinetic Modelling of High Density Combustion of Boron and High Energy Hydrocarbon Additives PolyEthylene Pyrolysis: Part 1. Fluorocarbon Solid Fuels in a for Paraffin-Fuel Hybrid Rockets Comparison of existing models Hybrid Rocket R. Jaffe, NASA Ames Research Center, Moffett N. Gascoin, University of Orléans, Bourges, T. Connell, Pennsylvania State University, Field, CA; A. Karabeyoglu, B. Evans, Space France University Park, PA; G. Risha, Pennsylvania Propulsion Group, Inc., Sunnyvale, CA; G. State University, Altoona, PA; R. Yetter, Zilliac, NASA Ames Research Center, Moffett Pennsylvania State University, University Field, CA; M. Sherburn, Australian National Park, PA; G. Young, Naval Surface Warfare

67 University, Canberra, Australia Center, Indian Head, MD Tuesday, 16 July 2013 151-HSABP-8 Pulse/Rotating Detonation Systems 231 Chaired by: T. O’BRIEN, Aerojet Rocketdyne 1600 hrs 1630 hrs AIAA-2013-3971 AIAA-2013-3972 Parametric Cycle Analysis of Experimental Investigation of Continuous Rotating Detonation Hysteresis Phenomenon for a Ejector-Augmented Rocket Engine Scramjet Engine H. Cao, University of Texas, Arlington, J. Chang, L. Wang, Harbin Institute of Arlington, TX Technology, Harbin, China Tuesday, 16 July 2013 152-HSABP-9 Numerical Analysis of Supersonic Combustion Systems, Scramjets III 230 A Chaired by: V. TANGIRALA, General Electric 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2013-3973 AIAA-2013-3974 AIAA-2013-3975 AIAA-2013-3976 AIAA-2013-3977 Experimental study on Dynamic Numerical Investigation on the Performance of Corrugated Limiting Numerical Solution of the Flowfield Aerothermodynamic Design Characteristics of Combustion Mode Effects of Cavity in Solid Fuel Tab in Presence of Sharp Corners in an Aluminized Gel Fuel Ramjet Optimization in Hypersonic Flows Transition Scramjet E. Rathakrishnan, S. Srivastava, Indian E. Matsibeker, B. Natan, Technion--Israel S. Eyi, Middle East Technical University, W. Bao, Q. Yang, J. Chang, M. Guo, Harbin H. Tao, Z. Wei, Beijing Institute of Institute of Technology Kanpur, Kanpur, India Institute of Technology, Haifa, Israel Ankara, Turkey Institute of Technology, Harbin, China Technology, Beijing, China Tuesday, 16 July 2013 153-ITAR-3 Propellants and Combustion/High Speed Air-Breathing (ITAR Restricted Session) 210 H Chaired by: D. SHAFER, GE Aviation and T. KAEMMING, Innovative Scientific Solutions 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3978 AIAA-2013-3979 AIAA-2013-3980 AIAA-2013-3981 An Experimental Investigation Investigations of Step Flameholders A Novel Active Combustion Control Hydrocarbon/Air Testing of a of Micro-Channel Catalyst Bed for a Scramjet Combustor (ITAR Concept for High-Frequency Unique Rotating Detonation Engine for a Hydrogen Peroxide Micro- Restricted Paper) Modulation of Atomized Fuel Flow Design (ITAR Restricted Paper) Propulsion System (ITAR Restricted J. Tam, Taitech, Inc., Beavercreek, OH; K. (ITAR Restricted Paper) R. Dyer, The Boeing Company, St. Louis, Paper) Hsu, Innovative Scientific Solutions, Inc., M. Caspermeyer, K. Meyer, H. Jansen, S. MO; A. Naples, T. Kaemming, J. Hoke, Z. Garcia, A. Choudhuri, University of Beavercreek, OH; M. Gruber, Air Force Holen, Jansen’s Aircraft Systems Controls, Innovative Scientific Solutions, Inc., Texas, El Paso, El Paso, TX Research Laboratory, Wright-Patterson Inc., Tempe, AZ; S. Starin, Avior Control Dayton, OH; F. Schauer, Air Force Research AFB, OH Technologies, Inc., Boulder, CO; D. Beaver, Laboratory, Wright-Patterson AFB, OH Dynic Labs, Inc., St. Louis, MO Tuesday, 16 July 2013 154-LP-16 Propellant Storage and Management III 211 D Chaired by: G. GRAYSON, Boeing Defense, Space & Security and D. GUADAGNOLI, Orbital Sciences Corporation 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3982 AIAA-2013-3983 AIAA-2013-3984 AIAA-2013-3985 Warm Pressurization Gas Effects on Liquid Nitrous Oxide BLEVE Tests Demise Characteristics Evaluation Basic Design and Fundamental the Liquid Hydrogen Bubble Point D. Sargent, Y. Tran, Federal Aviation for Melting Promotion Type Tank Data Acquisition Test of Reentry J. Hartwig, J. McQuillen, D. Chato, NASA Administration, Washington, DC T. Masuoka, I. Masuda, K. Kajiwara, Melting Promotion Type Satellite’s Glenn Research Center, Cleveland, OH Japan Aerospace Exploration Agency Propellant Tank (JAXA), Tsukuba, Japan; K. Yamada, IHI I. Masuda, T. Masuoka, K. Kajiwara, Corporation, Tomioka, Japan 68 Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; K. Yamada, IHI Corporation, Tomioka, Japan Tuesday, 16 July 2013 155-LP-17 Liquid Rocket Engines III 210 C Chaired by: S. MILLER, Aerojet and A. DEVEREAUX, Surrey Satellite Technology Ltd (SSTL) 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3986 AIAA-2013-3987 AIAA-2013-3988 AIAA-2013-3989 Performance of 1-N class liquefied Test and Evaluation of a 70 N-class Green Propulsion Advancement Development of Mono/Bi- gas propellant thruster Hydrazine Thruster for Application - Challenging the Maturity of Propellant Propulsion System for A. Kakami, University of Miyazaki, Miyazaki, to the Precise Attitude Control of Monopropellant Hydrazine Microsatellites and Planning of Japan; M. Yamanaka, T. Matsushita, S. Space Vehicles R. Masse, Aerojet, Redmond, WA; R. Space Demonstration Watanabe, T. Tachibana, Kyushu Institute of H. Jung, J. Kim, J. Kim, Pukyong National Sackheim, Consultant, Huntsville, AL S. Nishikizawa, T. Ohira, H. Sahara, Tokyo Technology, Kitakyushu, Japan University, Busan, South Korea Metropolitan University, Tokyo, Japan Tuesday, 16 July 2013 156-LP-18 Modeling and Simulation of Instabilities I 211 C Chaired by: T. HINERMAN, Pratt & Whitney-Rocketdyne 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2013-3990 AIAA-2013-3991 AIAA-2013-3992 AIAA-2013-3993 AIAA-2013-3994 Combustion Instability Mechanisms Considerations for Pressure Computational and Experimental The Generalized Rayleigh Criterion Influence of Boundary Condition in a Pressure-coupled Gas-gas Coupling Calculations in Investigation of Transverse and other Entropic Contributions to Treatment on Longitudinal Mode Coaxial Rocket Injector Combustion Instability Combustion Instabilities Combustion Instability Combustion Instability Predictions M. Harvazinski, Air Force Research Laboratory, J. Batterson, E. Jacob, Gloyer-Taylor K. Shipley, C. Morgan, W. Anderson, E. Jacob, J. Batterson, P. Gloyer, Gloyer- M. Harvazinski, D. Talley, V. Sankaran, Edwards AFB, CA; C. Huang, Purdue University, Laboratories, Tullahoma, TN Purdue University, West Lafayette, IN; Taylor Laboratories, Tullahoma, TN Air Force Research Laboratory, Edwards West Lafayette, IN; V. Sankaran, Air Force M. Harvazinski, V. Sankaran, Air Force AFB, CA Research Laboratory, Edwards AFB, CA; T. Research Laboratory, Edwards AFB, CA Feldman, W. Anderson, C. Merkle, Purdue University, West Lafayette, IN; D. Talley, Air Force Research Laboratory, Edwards AFB, CA Tuesday, 16 July 2013 157-LP-19 Modeling and Simulation of Engine Heat Transfer II 211 B Chaired by: M. NARAGHI, Manhattan Colege 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3995 AIAA-2013-3996 AIAA-2013-3997 AIAA-2013-3998 Supercritical Methane Heat Transfer Numerical Study of Enhancement Conjugated Combustion and Heat Quasi-2D Modeling of High-Aspect- Modeling in Rocket Engine Cooling of Regenerative Cooling Using Ribs Transfer Modeling for Full-Scale Ratio-Cooling-Channel Flows Channels C. Carpenter, S. Verma, J. Kapat, Regeneratively Cooled Thrust M. Pizzarelli, F. Nasuti, M. Onofri, M. Pizzarelli, F. Nasuti, M. Onofri, University of Central Florida, Orlando, FL Chambers University of Rome “La Sapienza’’, University of Rome “La Sapienza”’, Rome, Rome, Italy

69 H. Negishi, Y. Daimon, H. Kawashima, N. Italy; P. Roncioni, R. Votta, F. Battista, Yamanishi, Japan Aerospace Exploration Italian Aerospace Research Center (CIRA), Agency (JAXA), Tsukuba, Japan Capua, Italy Tuesday, 16 July 2013 158-LP-20 Liquid Propulsion History II: LOX/Hydrocarbon Propulsion: Liquid Propulsion Capability At Crossroads; Where Do We Go From Here? 230 B 1600 - 1830 hrs Chaired by: K. PUGMIRE, Spincraft and B. AUSTIN, IN Space LLC Introduction and Welcome Dr. Sandra Magnus Executive Director, AIAA

Russian, Ukraine developments (R-7 Sputnik, Vostok, Voskhod, Soyuz) Evolution and Promise of the Pintle Engine Family Round Table LOX/HC Propulsion: Enabling Missions and Development Initiatives, (NK-33) (RD-8, -58, -107, -0124, -191, -170, -180) (TRW- 13K, 40K) (Merlin - Falcon) US LOX/HC Propulsion Development Options Going Forward Igor Novkov, Roscosmos, Vladimir Chvanov, NPO-Energomash Tom Mueller Sackheim, Mueller, Starke, Bouley, Lyles Dale Thomas Associate Director NASA Marshall Space Flight Center Tuesday, 16 July 2013 159-NFF-5 Nuclear Thermal Propulsion II: Engine Modeling 113 Chaired by: J. WARREN, NASA Headquarters and S. BOROWSKI, NASA Glenn Research Center 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-3999 AIAA-2013-4000 AIAA-2013-4001 Oral Presentation (Invited) A Comparison of Materials Issues Analysis of NTR Engines Utilizing Nuclear Thermal Rocket Simulation Point of Departure Designs for Small for Cermet and Graphite-Based Prismatic Fuel Elements Derived in NPSS and Full Size NTR Engines using NERVA NTP Fuels from the GE-710 Program M. Belair, C. Sarmiento, T. Lavelle, NASA Composite and Cermet Reactor Fuels M. Stewart, Vantage Partners, LLC, J. FIttje, Vantage Partners, LLC, Cleveland, Glenn Research Center, Cleveland, OH S. Borowski, NASA Glenn Research Center, Cleveland, OH; B. Schnitzler, Self, Idaho OH; B. Schnitzler, Department of Energy, Cleveland, OH; B. Schnitzler, Idaho National Falls, ID Idaho Falls, ID Laboratory, Idaho Falls, ID Tuesday, 16 July 2013 160-PANEL-11 DoD Energy Panel Exhibit Hall 3 1600 - 1830 hrs As the largest federal user of energy, the Department of Defense (DoD) has played the leading role in the advancement of energy and propulsion systems and innovations for terrestrial and aerospace applications. More recently, energy considerations have become a prime focus in military operations, with various initiatives underway in operational energy efficiency (in addition to installation energy), renewable energy initiatives, and energy-based acquisition and lifecycle management. This special session presents perspectives from the DoD and DoE and is focused on DoD Energy challenges and issues, Strategy/Policy, priorities, initiatives and opportunities. Participants: Department of the Navy, U.S. Air Force, U.S. Army, Office of the Secretary of Defense, U.S. Department of Energy Speakers include: Vice Admiral Philip H. Cullom Lieutenant General William M. Faulkner Deputy Chief of Naval Operations for Fleet Readiness and Logistics, U.S. Navy Deputy Commandant, Installations and Logistics, U.S. Marine Corps and others Tuesday, 16 July 2013 70 161-SCP-5 Integrated Modeling and Simulation 210 G Chaired by: J. CHENOWETH, CRAFT Tech 1600 hrs 1630 hrs AIAA-2013-4002 AIAA-2013-4003 Model-Based Control of a Nonlinear Pattern Classification of a Civilian Aircraft Engine Simulation using an Turbofan’s State Space for Real- Optimal Tuner Kalman Filter Approach Time Surrogate Modeling J. Connolly, J. Csank, NASA Glenn Research M. Ozcan, B. Kestner, J. Tai, D. Mavris, Center, Cleveland, OH; A. Chicatelli, Vantage Georgia Institute of Technology, Atlanta, Partners, LLC, Brookpark, OH; J. Kilver, Ohio GA State University, Columbus, OH Tuesday, 16 July 2013 162-SCP-6 Systems Design, Engineering and Analysis I 114 Chaired by: F. CHANDLER, Boeing Defense, Space & Security 1600 hrs 1630 hrs 1700 hrs AIAA-2013-4004 AIAA-2013-4005 AIAA-2013-4006 Three-Axis Fluidic Thrust Vectoring Test Novel MEMS Position Sensors for Modular Electric Power Systems for Stand for a MIni Gas Turbine Engine Aerospace Applications Aerospace Applications M. Bonnici, R. Starkey, University of Y. Kim, H. Choi, Y. Lee, Agency for S. Steffan, Moog, Inc., East Aurora, NY Colorado, Boulder, Boulder, CO Defense Development, Daejeon, South Korea Tuesday, 16 July 2013 163-SR-5 Propellant effects on Internal Ballistics and Performance 111 Chaired by: H. CIEZKI, DLR - German Aerospace Center and Y. CHEN, National Space Organization Taiwan 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2013-4007 AIAA-2013-4008 AIAA-2013-4009 AIAA-2013-4010 Influence of Initial Propellant ARIANE 5 MPS ARTA 5 bench Study on the Effect of Propellant Propellant Trade-off Analysis for Temperature on Solid Rocket firing test: overview on propellant Entrapment in the Loose Flap Region Upper Stage Solid Rocket Motors Internal Ballistics modifications and their ballistic on solid Rocket Motor Performance Performance D. Greatrix, Ryerson University, Toronto, effect P. Sridharan, H. Harold, C. JasperLal, P. E. Cavallini, D. Bianchi, B. Favini, M. Canada E. Bucci, Avio S.p.A., Colleferro, Italy Balachandran, V. Srinivasan, Vikram Sarabhai Digiacinto, University of Rome “La Sapienza”, Space Centre, Thiruvananthapuram, India Rome, Italy; F. Serraglia, ESA, Rome, Italy Tuesday, 16 July 2013 164-SB-9 Speakers’ Briefing Individual Session Rooms 1830 - 1900 hrs Tuesday, 16 July 2013 165-APC-6 Advanced Space Propulsion Concepts II 210 F Chaired by: J. ROBINSON, Retired f/Boeing 1900 hrs 1930 hrs 2000 hrs AIAA-2013-4011 AIAA-2013-4012 AIAA-2013-4013 Staged Laser Sail Propulsion for Cold Gas Micro Propulsion for 2-Dimensional Numerical Interstellar and Extrasolar Flight: European Science Missions : status Simulation on MHD Hall Accelerator Novel Concepts on development and realization Connections for Advance Propulsion R. Ganapathy, M. Shoukath A, P. Johnson, activities for Lisa Pathfinder, using the CIP Method 71 B. Vivek, Hindusthan Educational Microscope and forthcoming Euclid, U. Spadavecchia, T. Sasaki, T. Kikuchi, T. Institutions, Coimbatore, India following the successful delivery of Aso, N. Harada, Nagaoka University of the first FM for GAIA Program Technology, Nagaoka, Japan G. Matticari, Selex ES, Florence, Italy Tuesday, 16 July 2013 166-EDU-2 Propulsion Education I 230 C Chaired by: R. TYSON, NASA and J. MILLER, George C. Marshall Space Flight Center 1900 hrs 1930 hrs 2000 hrs 2030 hrs AIAA-2013-4014 AIAA-2013-4015 AIAA-2013-4016 AIAA-2013-4017 Reliability Enhancement of LE-X 2DZAP: A Program for Simulating Student Investigation of Rapid Project Based Learning in Engine for Next Japanese Flagship Air-Launched Missiles Prototyping Technology for Hybrid Spacecraft Design Launch Vehicle H-X A. Pavacic, Self, Mundelein, IL Rocket Motor Fuel Grains N. Robinson, University of Texas, El Paso, R. Yonezawa, M. Shigeizumi, K. Hirata, M. Degges, P. Taraschi, J. Syphers, Alfred El Paso, TX Shizuoka Institute of Science and University, Alfred, NY; D. Armold, J. Boyer, Technology, Hamamatsu City, Japan K. Kuo, Pennsylvania State University, University Park, PA Tuesday, 16 July 2013 167-LP-22 Combustion Devices I 211 B Chaired by: D. JENSEN, Jentec 1900 hrs 1930 hrs 2000 hrs AIAA-2013-4018 AIAA-2013-4019 AIAA-2013-4020 Design and Validation of a Bomb Simulating Full-Scale Transverse Rocket engine noise reductions by Reactor for Liquid Hypergolic Combustion Instabilities in a Lab- water injection at DLR test bench P8 Propellants scale Facility P. Kallina, C. Böhm, G. Kruhsel, German J. Dennis, S. Son, T. Pourpoint, Purdue J. Quinlan, B. Zinn, Georgia Institute of Aerospace Center (DLR), Hardthausen, University, West Lafayette, IN Technology, Atlanta, GA Germany Tuesday, 16 July 2013 168-SR-6 SRTC Special Session: M Prevost and F Blomshield (Testing and Experimental Combustion Instability) 111 Chaired by: D. GREATRIX, Ryerson University and J. MAJDALANI, University of Tennessee Space Institute 1900 hrs 1930 hrs 2000 hrs 2030 hrs Oral Presentation (Invited) Oral Presentation (Invited) AIAA-2013-4022 AIAA-2013-4023 Development of the T-burner and ONERA’s Propulsion Laboratory Reduction of SRM Pressure Experimental Combustion its Role in Making Solid Rocket Adventure: Forty Years of Firing Oscillations Through the Use of Instability Data Analysis using Motors a Practical Tool in Space Tests Fuel Grains with Different Burn different theoretical Models Exploration M. Prévost, ONERA, Mauzac, France Velocities J. Knoetze, Stellenbosch University, J. Spurling, Naval Air Warfare Center, J. Anthoine, P. Jézéquel, P. Prévot, M. Stellenbosch, South Africa; C. Rousseau, China Lake, CA Prévost, ONERA, Mauzac, France; G. Rheinmetall Denel Munition, Cape Town, Casalis, ONERA, Toulouse, France South Africa Wednesday Wednesday, 17 July 2013 169-NW-11 Wednesday Networking Coffee & Pastries Exhibit Hall 2 0700 - 0800 hrs Wednesday, 17 July 2013 170-PLNRY-4 Hypersonic Propulsion, Leveraging Today to Deliver Unique Capabilities in the Future Exhibit Hall 1 0800 - 0900 hrs Keynote Spearker Mark Lewis

72 Director, Science and Technology Policy Institute Wednesday, 17 July 2013 171-PLNRY-5 Power Generation and Processing Challenges for Near-Term High Power Solar Electric Propulsion 212 A & C 0800 - 0900 hrs Keynote Speaker Roger M. Myers Executive Director, Electric Propulsion and Integrated Systems, Aerojet Rocketdyne Wednesday, 17 July 2013 172-NW-12 Networking Coffee Break Exhibit Hall 2 0900 - 0930 hrs Wednesday, 17 July 2013 173-SB-10 Speakers’ Briefing Individual Session Rooms 0900 - 0930 hrs Wednesday, 17 July 2013 174-APC-7 SOA Propulsion Concepts 111 Chaired by: J. ROBINSON, Retired f/Boeing 0930 hrs 1000 hrs AIAA-2013-4024 AIAA-2013-4025 Determination of Liquid/Gas Interface Discharge and Operational and Liquid Center of Mass for GPM Conditions of an Inertial Tank with PMD Using Surface Evolver Electrostatic Confinement Device D. Benson, NASA Goddard Space Flight C. Syring, G. Herdrich, University of Center, Greenbelt, MD Stuttgart, Stuttgart, Germany Wednesday, 17 July 2013 175-APS-5 Spacecraft Solar Power & Solar Array Designs 212 D Chaired by: S. GASNER, LMSSC and M. PATEL, US Merchant Marine Academy 0930 hrs 1000 hrs 1030 hrs AIAA-2013-4026 AIAA-2013-4027 AIAA-2013-4028 Electromagnetically Clean Solar In-Orbit (LEO) Point by Point Analysis of Solar Cell Efficiency Array Panels for the Magnetospheric Characterisation of Solar String for Venus Atmosphere and Surface Multiscale Spacecraft Technology Missions T. Stern, Vanguard Space Technologies, Inc., P. Alcindor, R. Kimber, R. Randles, Surrey G. Landis, E. Haag, NASA Glenn Research San Diego, CA; T. Parfet, Emcore Corporation, Satellite Technology, Ltd., Guildford, Center, Cleveland, OH Albuquerque, NM; M. Wrosch, Vanguard United Kingdom Space Technologies, Inc., San Diego, CA; A. Anders, Emcore Corporation, Albuquerque, NM; E. McNaul, Vanguard Space Technologies, Inc., San Diego, CA; J. Lyons, A. Aldape, NASA Goddard Space Flight Center, Greenbelt, MD Wednesday, 17 July 2013 176-EC-7 Energy Harvesting 212 A & C Chaired by: S. ORITI, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2013-4029 AIAA-2013-4030 AIAA-2013-4031 AIAA-2013-4032 Entropy and the Fallacy of Waste Hybrid Energy Harvester Using Studies on Capacitor Coupled Power Experimental Investigation of Heat Recovery Piezoelectric and Pyroelectric Extraction from an MHD generator the Performance of Flutter-Based J. Reyes, Self, Phoenixville, PA Properties of PZT-5A Ceramics S. Takayanagi, T. Sasaki, T. Kikuchi, T. Microgenerators A. Koyuncuoglu, O. Özyurt, T. Okutucu, Aso, N. Harada, Nagaoka University of R. Kafafy, A. Javeed, M. Idres, S. Ihsan, 73 H. Külah, O. Zorlu, Middle East Technical Technology, Nagaoka, Japan International Islamic University Malaysia, University, Ankara, Turkey Kuala Lumpur, Malaysia Wednesday, 17 July 2013 177-EP-9 Electrospray Propulsion III 210 D Chaired by: N. BRIKNER, Massachusetts Institute of Technology and M. TAJMAR, Dresden University of Technology 0930 hrs 1000 hrs 1030 hrs AIAA-2013-4033 AIAA-2013-4034 AIAA-2013-4035 Investigating the Transport of Slit FEEP Thruster Performance with On the Manufacturing and Emission Net Charge and Contaminants in Ionic Liquid Propellant Characteristics of Dielectric Electrospray Thrusters S. Marcuccio, Pisa University, Pisa, Italy; Electrospray Sources T. Coles, P. Lozano, Massachusetts Institute N. Giusti, P. Pergola, Alta S.p.A., Pisa, Italy C. Coffman, P. Lozano, Massachusetts of Technology, Cambridge, MA Institute of Technology, Cambridge, MA Wednesday, 17 July 2013 178-EP-10 Hollow Cathodes 211 A Chaired by: J. SZABO, Busek Co., Inc. and I. MIKELLIDES, Jet Propulsion Laboratory 0930 hrs 1000 hrs AIAA-2013-4036 AIAA-2013-4037 Modeling and Development of Effect of a Low Work Function the RF-Controlled Hollow Cathode Insert on Hollow Cathode Concept Temperature and Operation M. Plasek, C. Wordingham, E. Choueiri, L. Rand, J. Williams, Colorado State Princeton University, Princeton, NJ University, Fort Collins, CO Wednesday, 17 July 2013 179-HR-7 Fuel Regression Characterization 211 C Chaired by: S. WHITMORE, Utah State University and B. WAXMAN, Stanford University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-4038 AIAA-2013-4039 AIAA-2013-4040 AIAA-2013-4041 AIAA-2013-4042 Experimental Study of Vegetal Based Fuel regression-rate characterization Effects of Multi-Section Swirl Injection Longitudinally-Variable Hybrid UAH Sounding Rocket Project with Polyurethane Fuel filled with Paraffin on a lab-scale hybrid rocket burning Method on Fuel Regression Rate of Rocket Regression Rate Model with Guided Parafoil Recovery Particles for Hybrid Rocket Motors N2O and paraffin-based propellants High Density Polyethylene Fueled Radiation and Boundary Layer M. Becnel, R. Frederick, University of L. Rocco, Flowtest Aerospace Research, F. Scaramuzzino, Second University of Hybrid Rocket Engine Effects Alabama, Huntsville, Huntsville, AL Caieras, Brazil; S. Gomes, L. Nunes Almeida, Naples, Naples, Italy; C. Carmicino, G. Festa, S. Oyama, Y. Hirata, K. Araki, K. Ohe, S. Aso, S. Eilers, S. Whitmore, Utah State Avibrás Aerospace Industry, Jacareí, Brazil; University of Naples “Federico II”, Naples, Y. Tani, Kyushu University, Fukuoka, Japan; T. University, Logan, UT J. Rocco, K. Iha, Aeronautical Institute of Italy; A. Viviani, Second University of Naples, Shimada, Japan Aerospace Exploration Agency Technology, São José dos Campos, Brazil Naples, Italy; A. Russo, University of Naples (JAXA), Kanagawa, Japan “Federico II”, Naples, Italy Wednesday, 17 July 2013 180-HR-8 Novel Motor Operating Conditions II 211 D Chaired by: A. GANY, Technion - Israel Institute of Technology and B. CANTWELL, Stanford University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2013-4043 AIAA-2013-4044 AIAA-2013-4045 AIAA-2013-4046 Hybrid Rocket Performance with Optimization of a H2O2 Gas Comparison of Nitrous Oxide and Comparison of Approximate Varying Additive Concentrations Generator for a Hybrid Rocket Carbon Dioxide with Applications to and Exact Approaches for the R. Kafafy, M. Azami, M. Idres, Engine Self-Pressurizing Propellant Tank Optimization of Hybrid-Rocket International Islamic University Malaysia, M. Faenza, F. Moretto, A. Bettella, D. Dynamics Upper-Stage Kuala Lumpur, Malaysia Pavarin, University of Padua, Padua, Italy J. Zimmerman, B. Cantwell, Stanford L. Casalino, D. Pastrone, F. Simeoni,

74 University, Stanford, CA; G. Zilliac, NASA Technical University of Turin, Turin, Italy Ames Research Center, Moffett Field, CA; B. Waxman, Stanford University, Stanford, CA Wednesday, 17 July 2013 181-HR-9 New Approaches to Hybrid Motor Development 211 B Chaired by: B. MADHANABHARATAM, Space Propulsion Group, Inc. and J. MAJDALANI, University of Tennessee Space Institute 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-4047 AIAA-2013-4048 AIAA-2013-4049 AIAA-2013-4050 AIAA-2013-4051 Firing tests of hybrid engine with Scale Effects on Combustion Sorbitol-Based Hybrid Fuel Studies Small Rocket Launch Experiment Ignition Characteristics of HAN varying oxidizer nature and Characteristics of CAMUI-type with Nitrous Oxide for the Stratos II using Low Melting Point Thermoplastic Liquid for Gas-Hybrid Rockets operating conditions Hybrid Rocket Motors Sounding Rocket Fuel/N2O Hybrid Rocket S. Onodaka, K. Sakaue, R. Noguchi, T. N. Gascoin, University of Orléans, Bourges, H. Nagata, T. Ishiyama, Y. Inaba, R. T. Knop, B. Zandbergen, A. Cervone, Y. Wada, R. Kato, Akita University, Akita, Kuwahara, Nihon University, Funabashi, France Kanai, M. Wakita, T. Totani, Hokkaido R. Huijsman, S. Powell, R. Werner, J. Japan; N. Kato, Katazen Corporation, Oobu, Japan; X. Yu, H. Shibamoto, Hosoya Pyro- University, Sapporo, Japan; T. Uematsu, Ehlen, F. Lindemann, J. Wink, C. Becker, Japan; K. Hori, Japan Aerospace Exploration Engineering Company, Ltd., Akiruno, Japan Camuispaceworks Company, Ltd., Akabira, K. Samarawickrama, Delft University of Agency (JAXA), Sagamihara, Japan Japan Technology, Delft, The Netherlands Wednesday, 17 July 2013 182-ITAR-4 Pressure Gain Combustion: VULCAN Program Overview (ITAR Restricted Session) 210 H 0930 - 1200 hrs Chaired by: C. BROPHY, Naval Postgraduate School and V. TANGIRALA, General Electric This panel will include discussions on the VULCAN Program Overview and the VULCAN Phase II program activities and risk reduction activities. Moderators: Christopher Brophy, Naval Postgraduate School and Venkat Tangirala, GE Global Research Panelists: Arther Mabbett Adam Holley Pete Jardine Fred Schauer Defense Advanced Research Projects Agency (DARPA) Pratt & Whitney Rocketdyne GE Aviation Air Force Research Lab United Technologies Research Center

Wednesday, 17 July 2013 183-LP-23 Monopropellant Catalyst Development and Decomposition Phenomena 210 A Chaired by: T. POURPOINT, Purdue University 0930 hrs 1000 hrs AIAA-2013-4052 AIAA-2013-4053 Hydrazine decomposition Improving and Testing S-405 phenomena observed by Neutron Catalyst radiography at a catalyst bed E. Wucherer, W. Witty, B. Chenevert, O. H. Kagawa, T. Nagata, T. Masuoka, K. Morgan, Aerojet, Redmond, WA Kajiwara, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; Y. Saitoh, Y. Kawabata, University of Kyoto, Kumatori, Japan 75 Wednesday, 17 July 2013 184-LP-24 Liquid Rocket Engines IV 210 B Chaired by: J. SCHNACKEL, United Launch Alliance and J. SAUER, Orbital Technologies Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2013-4054 AIAA-2013-4055 AIAA-2013-4056 AIAA-2013-4057 The VINCI upper stage engine: New Upper Stage Expander Cycles Hot-Firing Test of Methane-Fueled Development of the A5ME upper toward the demonstration of V. Balepin, ATK, Ronkonkoma, NY Rocket Engine under High Altitude stage maturity Condition P. Alliot, Snecma, Vernon, France; A. Juhls, J. Delange, E. Edeline, P. Alliot, Snecma, S. Ueda, T. Tomita, T. Onodera, Japan Astrium, Bremen, Germany; J. Delange, Vernon, France; A. Lekeux, French Space Aerospace Exploration Agency (JAXA), E. Edeline, M. Thalamy, Snecma, Vernon, Agency (CNES), Paris, France Kakuda, Japan; Y. Kano, I. Kubota, T. France Munenaga, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan Wednesday, 17 July 2013 185-LP-26 Modeling and Simulation of Instabilities II 231 Chaired by: T. HINERMAN, Pratt & Whitney-Rocketdyne and D. LINEBERRY, UAH Propusion Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2013-4058 AIAA-2013-4059 AIAA-2013-4060 AIAA-2013-4061 Numerical Simulations of Instabilities On the Reduction of Unsteady CFD A Helmholtz-type Numerical An order estimation of the acoustic in Single-Hole Orifice Elements to Determine the Sources and Sinks Simulation of Thermo-acoustic losses inside a simulated liquid rocket V. Ahuja, A. Hosangadi, Combustion Research of Unsteady Energy Instabilities in a 3-D Rijke Tube chamber and Flow Technology, Inc., Pipersville, PA; E. Jacob, Gloyer-Taylor Laboratories, K. Cengiz, Y. Ozyoruk, Middle East T. Shimizu, Y. Morii, Japan Aerospace M. Hitt, D. Lineberry, University of Alabama, Tullahoma, TN Technical University, Ankara, Turkey Exploration Agency (JAXA), Sagamihara, Huntsville, Huntsville, AL Japan; Y. Daimon, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan Wednesday, 17 July 2013 186-LP-27 Combustion Devices II 210 F Chaired by: J. LOCKE, United Technologies Research Center and R. BALLARD, NASA Marshall Space Flight Center 0930 hrs 1000 hrs 1030 hrs AIAA-2013-4062 AIAA-2013-4063 AIAA-2013-4064 Design and Analysis for Reusable Development of Ultra Lean Burn The Influence of Annular Jet Liquid Rocket Engine Chamber Preburners for Small Liquid Rockets Dynamics on Swirl-coaxial Injection T. Chen, J. Yang, P. Jin, G. Cai, Beihang I. Moon, S. Lee, I. Moon, Korea Aerospace During Self-pulsations University, Beijing, China Research Institute, Daejeon, South Korea C. Eberhart, D. Lineberry, R. Frederick, University of Alabama, Huntsville, Huntsville, AL Wednesday, 17 July 2013 187-LP-28 Turbomachinery II 210 E Chaired by: D. RANSOM, Southwest Research Institute and B. MARCU, SpaceX 0930 hrs 1000 hrs 1030 hrs AIAA-2013-4065 AIAA-2013-4066 AIAA-2013-4067 Experimental Validation of a Reduced Preliminary Test of Turbopump Analysis about Machinability of Order for Radial Turbopump Design Using Radial Turbine Driven by Superalloys applied on Turbines of LRE D. Valentini, University of Pisa, Pisa, Italy; Hydrogen Peroxide Gas Generator Turbopumps A. Pasini, Alta S.p.A., Pisa, Italy; G. Pace, D. Park, S. Kwon, Korea Advanced O. Loureda, J. Gomes, Technological University of Pisa, Pisa, Italy; L. Torre, Alta Institute of Science and Technology, Institute of Aeronautics (ITA), São José dos S.p.A., Pisa, Italy; L. d’Agostino, University of Daejeon, South Korea Campos, Brazil; W. Vireira, Acrux Aerospace Pisa, Pisa, Italy Technologies, São José dos Campos, Brazil Wednesday, 17 July 2013 76 188-LP-29 Modeling and Simulation of Injector and Chamber Flows 230 A Chaired by: D. KIRK, Florida Institute of Technology and C. KIRCHBERGER 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-4068 AIAA-2013-4069 AIAA-2013-4070 AIAA-2013-4071 AIAA-2013-4072 Continuous Phase Propellant Free-surface Flow Simulation of Exact Solution of the Bidirectional Large Eddy Simulation of Shear Numerical Investigation on Flow Injection Model for Liquid Rocket Impinging Jet Nozzles for Liquid- Vortex in a Conically-Shaped Coaxial Rocket Injector: Real Fluid in the Variable Area Cavitating Engines propellant Thrusters Cyclonic Chamber with Constant Effects Venturi D. Banuti, K. Hannemann, German J. Kouwa, S. Matsuno, IHI Corporation, Angular Momentum J. Hickey, P. Ma, Stanford University, Stanford, P. Zeng, H. Tian, N. Yu, G. Cai, Beihang Aerospace Center (DLR), Göttingen, Yokohama, Japan; C. Inoue, T. Himeno, T. Barber, J. Majdalani, University of CA; M. Ihme, University of Michigan, Ann University, Beijing, China Germany T. Watanabe, University of Tokyo, Tokyo, Tennessee Space Institute, Tullahoma, TN Arbor, Ann Arbor, MI; S. Thakur, Streamline Japan Numerics, Inc., Gainesville, FL Wednesday, 17 July 2013 189-NFF-6 Fusion and Alternative Nuclear Concepts II 112 Chaired by: B. CASSENTI, University of Connecticut and R. SEDWICK, University of Maryland 0930 hrs 1000 hrs AIAA-2013-4073 AIAA-2013-4074 Propulsion and Trajectory Antimatter Propulsion Considerations for Low Thrust Solar S. Pranav, Sri Ramakrishna Engineering System Missions College, Coimbatore, India B. Cassenti, University of Connecticut, Storrs, Storrs, CT Wednesday, 17 July 2013 190-NFF-7 Nuclear Thermal Propulsion III: Missions, Vehicles and Architectures 113 Chaired by: M. BULMAN, Aerojet Rocketdyne and J. WARREN, NASA Headquarters 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation (Invited) AIAA-2013-4075 AIAA-2013-4076 Oral Presentation (Invited) The Nuclear Thermal Propulsion Stage Thrust Vector Control for Nuclear A One-year Round Trip Crewed A Nuclear Cryogenic Propulsion (NTPS): A “Workhorse” Space Asset Thermal Rockets Mission to Mars using Bimodal Stage for Near-Term Space Missions Supporting Exploration, Commercial C. Ensworth, NASA Glenn Research Center, Nuclear Thermal and Electric M. Houts, T. Kim, W. Emrich, H. Gerrish, Development and Human Settlement Cleveland, OH Propulsion (BNTEP) NASA Marshall Space Flight Center, of the Moon L. Burke, S. Borowski, D. McCurdy, T. Huntsville, AL; S. Borowski, NASA Glenn S. Borowski, NASA Glenn Research Center, Packard, NASA Glenn Research Center, Research Center, Cleveland, OH Cleveland, OH; D. McCurdy, Vantage Partners, Cleveland, OH LLC, Brookpark, OH; L. Burke, NASA Glenn Research Center, Cleveland, OH Wednesday, 17 July 2013 191-PANEL-12 High Speed Propulsion Development and Implementatino Exhibit Hall 3 0930 - 1200 hrs Moderator: Mark Lewis, Director, Science and Technology Policy Institute Panelists: John Korte John Kusnierek Gerald (Scott) Cruzen Curtis Berger Steven Beckel Research Directorate Chief Engineer for Hypersonics Director, Business Development Vice President, Advanced Design and Technology Director, Hypersonic Programs Director, Advanced Propulsion Business Development NASA LaRC Rolls-Royce North American Technologies, Inc. Williams International Co., LLC Aerojet Rocketdyne ATK

Wednesday, 17 July 2013 77 192-PP-4 Public-Private Partnerships to Accelerate Technology Transition 230 C 0930 - 1200 hrs Panel will discuss barriers to effective innovation and technology transition to the aerospace industry as well as potential pathways to improved technology maturation and transition. Moderator: Graham Warwick, Senior Editor, Technology, Aviation Week Panelists: Alton Romig Dale Carlson Alan Epstein Mark Anderson Jaiwon Shin Vice President & General Manager of Advanced General Manager Technology Strategy Vice President Technology & Environment Director, Flight Sciences Technology, Phantom Associate Administrator Aeronautics Development Programs, Skunk Works GE Aviation Pratt & Whitney Works, NASA Lockheed Martin Corporation The Boeing Company

Wednesday, 17 July 2013 193-SR-7 SRM Throttleability Using Pintle Nozzles and Novel Techniques 230 B Chaired by: R. ELLIS and D. BIANCHI, Sapienza University of Rome 0930 hrs 1000 hrs 1030 hrs AIAA-2013-4078 AIAA-2013-4079 AIAA-2013-4080 Throttleable solid propellant Cold Tests and the Dynamic A Study on the Performance microthruster using laser-assisted Characteristics of the Pintle Type Characteristics of Blunt Body Pintle combustion Solid Rocket Motor Nozzle A. Kakami, University of Miyazaki, H. Ko, Microfriend, Seoul, South Korea; J. Lee, Agency for Defense Development, Miyazaki, Japan; T. Hamada, M. J. Lee, Agency for Defense Development, Daejeon, South Korea; H. Ko, Microfriend, Shimoda, T. Tachibana, Kyushu Institute of Daejeon, South Korea Seoul, South Korea Technology, Kitakyushu, Japan Wednesday, 17 July 2013 194-SR-8 Particle Effects on Combustion Instability and Agglomeration 210 G Chaired by: J. MAJDALANI, University of Tennessee Space Institute and C. ROUSSEAU, Denel (Pty) Ltd. 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2013-4081 AIAA-2013-4082 AIAA-2013-4083 AIAA-2013-4084 Uniform Particle Regression and Nonuniform Particle Regression A new Eulerian Multi-Fluid model for Numerical Simulation of Particle Solid Rocket Combustion Instability and Solid Rocket Combustion bi-component polydisperse sprays: Breakup/Coalescence Processes in Suppression Instability Suppression an essential approach to evaluate the Shock Waves D. Greatrix, Ryerson University, Toronto, D. Greatrix, Ryerson University, Toronto, impact of aluminum combustion on K. Park, S. Heister, Purdue University, Canada Canada Solid Rocket Motor instabilities West Lafayette, IN A. Sibra, J. Dupays, ONERA, Palaiseau, France; F. Laurent, M. Massot, National Center for Scientific Research (CNRS), Châtenay-Malabry, France Wednesday, 17 July 2013 195-SR-9 Nozzle and Internal Ballistic Prediction 114 Chaired by: B. LEARY, Johns Hopkins University Applied Physics Laboratory and M. LANGHENRY, Raytheon Missile Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2013-4085 AIAA-2013-4086 AIAA-2013-4087 AIAA-2013-4088 A Versatile Tool for Modelling Solid Three Dimensional Rocket Nozzle Solid rocket motor grain burn Thermal Decomposition Kinetics Propulsion Stages Design Using Adjoint Method back analysis using level set Studies of Ammonium Perchlorate A. Pasini, Alta S.p.A., Pisa, Italy; D. S. Eyi, Middle East Technical University, methods and Monte-Carlo volume - HTPB /Al/AP Solid Propellants Valentini, University of Pisa, Pisa, Italy; Ankara, Turkey; M. Yumusak, ROKETSAN integration formulated with Iron Oxide burning L. Torre, Alta S.p.A., Pisa, Italy; G. Pace, Missile Industries, Inc., Ankara, Turkey W. Sullwald, G. Smit, Stellenbosch rate catalyst in Nano and Micro scale

78 University of Pisa, Pisa, Italy; R. Biesbroek, University, Stellenbosch, South Africa; A. L. Nunes Almeida, A. Martins, S. Gomes, F. ESA, Noordwijk, The Netherlands Steenkamp, Flamengro, Pretoria, South Cunha, Avibrás Aerospace Industry, Jacareí, Africa; C. Rousseau, Rheinmetall Denel Brazil; J. Rocco, K. Iha, Aeronautical Institute Munition, Somerset West, South Africa of Technology, São José dos Campos, Brazil Wednesday, 17 July 2013 196-TFES-1 Gaseous Fuels 214 Chaired by: K. BRYDEN, Iowa State University; B. KHANDELWAL, The University of Sheffield and A. CHOUDHURI, University of Texas at El Paso 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2013-4089 AIAA-2013-4090 AIAA-2013-4091 AIAA-2013-4092 Experiments on Stability of Syngas Effect of pressure on NO kinetics in Effects of Diluents, Firing Input and Effect of Particle Density on the Combustion in a Trapped Vortex Syngas Combustion Hydrogen Content on Premixed Hydrodynamic Behavior of a Gas- Combustor A. Sahu, R. Ravikrishna, Indian Institute of Oxy-Syngas Flames Solid Fluidized Bed S. Krishna, R. Ravikrishna, Indian Institute Science, Bangalore, India M. de la Torre, N. Love, A. Choudhuri, M. Sarker, N. Love, A. Choudhuri, of Science, Bangalore, India University of Texas, El Paso, El Paso, TX University of Texas, El Paso, El Paso, TX Wednesday, 17 July 2013 197-TM-6 Aerospace and Terrestrial Power Systems Thermal Management II 213 Chaired by: C. TARAU, Advanced Cooling Technologies and S. SPENCER, Naval Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2013-4093 AIAA-2013-4094 AIAA-2013-4095 AIAA-2013-4096 AIAA-2013-4097 Effect of Shaped Holes and Density Influence of Exhaust Collector Drop Impact on Nanotextured Experimental Investigation of Effects of Roughness-Induced Ratio on Film Cooling Effectiveness Box Flow Conditioning on Diffuser Surfaces Different Cooling Methods for Boundary Layer on Leak Propagation on Blade Surface Pressure Recovery and System K. Krishnan, E. Loth, University of Virginia, Photovoltaic Module and Detection in Gas Pipes E. Khalil, M. Shahat, M. Fouad, Cairo Performance Charlottesville, Charlottesville, VA O. Abdellatif, Benha University, Cairo, A. Adesina, E. Ogedengbe, University of University, Cairo, Egypt A. Bravato, J. Hodges, J. Kapat, University Egypt Lagos, Akoka, Nigeria; A. Odeshi, University of of Central Florida, Orlando, FL Saskatchewan, Saskatoon, Canada Wednesday, 17 July 2013 198-TM-7 Spacecraft and Lunar/Mars/Venus Surface Thermal Management II 212 B Chaired by: M. CHOI, NASA-Goddard Space Flight Center and S. SPENCER, Naval Research Laboratory 0930 hrs 1000 hrs AIAA-2013-4098 AIAA-2013-4099 Design and Analysis of JMAPS Using Paraffin with -10˚C to 10˚C Instrument Thermal Control System Melting Point for Payload Thermal T. Hoang, TTH Research, Inc., Clifton, VA; Energy Storage in SpaceX Dragon D. Wilson, Praxis, Inc., Alexandria, VA; Trunk K. Weldy, R. Baldauff, Naval Research M. Choi, NASA Goddard Space Flight Laboratory, Washington, DC Center, Greenbelt, MD Wednesday, 17 July 2013 199-NW-13 JPC Awards Luncheon Exhibit Hall 1 1200 - 1400 hrs Wednesday, 17 July 2013 200-SB-11 Speakers’ Briefing Individual Session Rooms 1400 - 1430 hrs Wednesday, 17 July 2013 201-ECS-3 Energetic Devices and Materials - Design and Application 214 Chaired by: J. BAGLINI, Exodynamics Technology Incorporated 1430 hrs 1530 hrs 1600 hrs AIAA-2013-4100 AIAA-2013-4101 AIAA-2013-4102 79 Mars Science Laboratory (MSL) and the “Curiosity” Rover Pyrotechnic Infrared Camouflage of the Zirconium powders and ZrNi Mechanisms, Heritage and Implementation Warfighter’s Equipment through alloy powders used as energetic R. Webster, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA Enhanced Coating Technology materials within pyrotechnic L. Nunes Almeida, A. Martins, S. Gomes, applications S. Aramaki, R. Pinto, F. Cunha, Avibrás G. Wilfing, Rockwood Lithium, GmbH, Aerospace Industry, Jacareí, Brazil Frankfurt, Germany Wednesday, 17 July 2013 202-EDU-3 Technology, Education and NASA’s New Asteroid Grand Challenge 230 C 1430 - 1630 hrs NASA Technology and education-focused opportunities in the new fiscal reality. Overview of NASA’s new “Protect the Planet Grand Challenge”, in which we invite worldwide participation with NASA on discovering all the asteroid threats to human population and figuring out what to do about them - both science and technology research have a stake in it. Mason Peck NASA Chief Technologist Wednesday, 17 July 2013 203-EDU-4 Propulsion Education II 211 B Chaired by: R. TYSON, NASA and E. FLEEMAN 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2013-4103 AIAA-2013-4104 AIAA-2013-4105 AIAA-2013-4106 AIAA-2013-4107 AIAA-2013-4108 A New Approach to Propulsion Hybrid Rocket Design/Build/Test Design, Analysis, Fabrication, Ground- Overview of Combustion Characterization of Combustion The UAH 2013 University Student System Development, Brazilian Course at Purdue University Test, and Flight of a Two-Stage Hybrid Instabilities in Liquid Rocket Performance of Hydrocarbon Fuels Launch Initiative Project Style E. Miklaszewski, J. Dadson, D. Fox, D. and Solid Rocket Engines - Coupling Mechanisms & using a Bi-Propellant Rocket Engine D. Lineberry, A. Patel, M. Denny, R. Nardi, V. Perez, Inotech Ltda, São José Kees, L. Larson, J. Rideout, J. Stevens, D. Gerson, E. Prince, K. Anderson, I. Ravlich, Control Techniques J. Koeck, J. Sell, D. Bittner, G. Risha, S. Harrison, University of Alabama, dos Campos, Brazil T. Pourpoint, Purdue University, West A. Kotine, E. Flores, J. Riel, S. Krishnamoorthy, J. Bennewitz, R. Frederick, University of Pennsylvania State University, Altoona, PA Huntsville, Huntsville, AL Lafayette, IN A. Fidalgo, P. Kaur, K. Freeman, A. Fickes, Alabama, Huntsville, Huntsville, AL Stanford University, Stanford, CA Wednesday, 17 July 2013 204-EP-11 Ion Engines II 210 E Chaired by: J. POLK, Jet Propulsion Laboratory and M. CELIK, Bogazici University 1430 hrs 1500 hrs 1530 hrs AIAA-2013-4109 AIAA-2013-4110 AIAA-2013-4111 Ion Accelerator Currents Beyond 2D Fluid Model for Axisymmetric Plume Characterization of the NEXT the Child-Langmuir Limit RF Ion Thruster Cylindrical Thruster Under Extended Throttle O. Biblarz, Naval Posgraduate School, Discharge Chamber Conditions Monterey, CA E. Turkoz, M. Celik, Bogazici University, J. Young, M. Crofton, The Aerospace Istanbul, Turkey Corporation, El Segundo, CA; M. Patterson, NASA Glenn Research Center, Cleveland, OH Wednesday, 17 July 2013 205-EP-12 Qualification and Operation of EP Systems 212 D Chaired by: V. HRUBY, Busek Co, Inc. and V. KHAYMS, Lockheed Martin Space Systems 1430 hrs 1500 hrs 1530 hrs AIAA-2013-4112 AIAA-2013-4113 AIAA-2013-4114 In-Flight Operation of the Dawn Ion Qualification of the PPS-1350 Hall Update On the Operational Status of Propulsion System Through Year plasma thruster at 2.5 kW the International Space Station Plasma One of Cruise to Ceres O. Duchemin, S. Zurbach, F. Marchandise, Contactor Hollow Cathode Assemblies C. Garner, M. Rayman, California Institute N. Cornu, Snecma, Vernon, France for July 2011-May 2013 of Technology, Pasadena, CA H. Kamhawi, J. Yim, M. Patterson, P. Dalton, NASA Glenn Research Center, Cleveland, OH Wednesday, 17 July 2013

80 206-EP-14 Hall Thrusters 210 D Chaired by: B. JORNS, Electric Propulsion Laboratory, Inc. and R. HOFER, Jet Propulsion Laboratory 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2013-4115 AIAA-2013-4116 AIAA-2013-4117 AIAA-2013-4118 AIAA-2013-4119 Iodine Plasma Species in a Hall Mode Transitions in Hall Effect Conducting Wall Hall Thrusters A New Method for Analyzing Near- Low Frequency Plasma Oscillations Effect Thruster Plume Thrusters D. Goebel, R. Hofer, I. Mikellides, I. Katz, Field Faraday Probe Data of Hall in a 6-kW Magnetically Shielded J. Szabo, M. Robin, Busek Company, Inc., M. Sekerak, M. McDonald, University of Jet Propulsion Laboratory, California Thrusters Hall Thruster Natick, MA Michigan, Ann Arbor, Ann Arbor, MI; R. Hofer, Institute of Technology, Pasadena, CA W. Huang, R. Shastry, D. Herman, B. Jorns, R. Hofer, Jet Propulsion J. Polk, Jet Propulsion Laboratory, California G. Soulas, H. Kamhawi, NASA Glenn Laboratory, California Institute of Institute of Technology, Pasadena, CA; B. Research Center, Cleveland, OH Technology, Pasadena, CA Longmier, A. Gallimore, University of Michigan, Ann Arbor, Ann Arbor, MI; D. Brown, Air Force Research Laboratory, Edwards AFB, CA Wednesday, 17 July 2013 207-EP-15 Micropropulsion II 211 A Chaired by: J. VITUCCI and D. CHIU 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2013-4120 AIAA-2013-4121 AIAA-2013-4122 AIAA-2013-4123 AIAA-2013-4124 Near Plume Modeling of a Micro A Radio Frequency Plasma Micro- Power Train Configuration Study Characteristics of a Pulsed Plasma Experimental Characterization of Cathode Arc Thruster Thruster: Characterization of on a Pulsed Plasma Thruster with Thruster Using Dimethyl Ether as Radio Frequency Microthermal L. Brieda, Particle In Cell Consulting, Various Discharge Gases Through State-of-the-Art High Current Liquid Propellant Thruster Performance LLC, Falls Church, VA; T. Zhuang, M. Optical Diagnostics Monitors S. Masui, M. Chiba, Kyushu Institute of S. Williams, I. Hrbud, Purdue University, Keidar, George Washington University, A. Greig, C. Charles, R. Boswell, Australian M. Lau, G. Herdrich, University of Technology, Fukuoka, Japan; A. Kakami, West Lafayette, IN Washington, DC National University, Canberra, Australia Stuttgart, Stuttgart, Germany; N. Karrer, University of Miyazaki, Miyazaki, Japan; T. Swiss Federal Institute of Technology, Tachibana, Kyushu Institute of Technology, Zurich, Switzerland Fukuoka, Japan Wednesday, 17 July 2013 208-EP-16 Applications of Electric Propulsion 212 A & C Chaired by: A. FAUST 1430 hrs 1500 hrs AIAA-2013-4125 AIAA-2013-4126 On the scaling of electric thrusters for Finding a Way: Boeing’s All Electric asteroid capture and return missions Propulsion Satellite J. Little, E. Choueiri, Princeton University, S. Feuerborn, J. Perkins, D. Neary, The Princeton, NJ Boeing Company, El Segundo, CA Wednesday, 17 July 2013 209-EP-17 Facilities Effects and Interactions with Materials 212 B Chaired by: A. GALLIMORE, University of Michigan and J. LITTLE, Princeton University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2013-4127 AIAA-2013-4128 AIAA-2013-4129 AIAA-2013-4130 AIAA-2013-4131 AIAA-2013-4132 3D Model for Atomic Sputtering Wall Material Effects on Sheath Evaluation of a Plasma Impedance Experimental and Numerical Thrust Augmentation by Charge The Plasma-Material Interactions of Heterogeneous Ceramic Potential Profile Probe in a Time-varying Non- Investigations of Vacuum Exchange Facility at UCLA Compounds S. Langendorf, M. Walker, Georgia Institute of uniform Plasma Chamber Effects on Plasma Plume M. Crofton, J. Pollard, The Aerospace T. Matlock, R. Conversano, D. Goebel, R. A. Schinder, M. Walker, J. Rimoli, Georgia Technology, Atlanta, GA; L. Rose, M. Keidar, M. Hopkins, L. King, Michigan Measurements Corporation, El Segundo, CA Wirz, University of California, Los Angeles, Institute of Technology, Atlanta, GA George Washington University, Washington, Technological University, Houghton, MI J. Polansky, K. Chou, J. Wang, University Los Angeles, CA DC; L. Brieda, Particle in Cell Consulting, LLC, of Southern California, Los Angeles, CA Falls Church, VA Wednesday, 17 July 2013 210-HR-10 Analytic Modeling of Hybrid Motors 211 C

81 Chaired by: S. COOGAN, Southwest Research Institute and B. WAXMAN, Stanford University 1430 hrs 1500 hrs 1530 hrs AIAA-2013-4133 AIAA-2013-4134 AIAA-2013-4135 Performance Modeling of the Model of Hybrid Rocket Combustion Micro and Full-Scale Experiments Phoenix-2A Hybrid Sounding in Classical Hybrid Rocket Motors on Hybrid Rocket Fuel and Prelude Rocket using the HYROPS Software T. Morita, Tokai University, Hiratsuka, to Hybrid Rocket Combustor F. Leverone, M. Brooks, J. Pitot, L. Japan; S. Yuasa, Tokyo Metropolitan Simulations Roberts, K. Veale, University of KwaZulu- University, Hino, Japan; T. Shimada, Japan N. Gascoin, University of Orléans, Bourges, Natal, Durban, South Africa Aerospace Exploration Agency (JAXA), France Sagamihara, Japan; S. Yamaguchi, Tokai University, Hiratsuka, Japan Wednesday, 17 July 2013 211-HR-11 Testing of Hybrid Motors 211 D Chaired by: B. CANTWELL, Stanford University and B. EVANS, Space Propulsion Group Inc. 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2013-4137 AIAA-2013-4138 AIAA-2013-4139 AIAA-2013-4140 AIAA-2013-4141 Hybrid Engine Development, Launches of Hybrid Rockets with Laboratory Scale Hybrid Rocket Development and Flight Testing of Test of Hybrid Rocket Fuel Grains Education and Outreach at Munich’s Wax Fuel HTPB Fuel Grain Performance a Hybrid Rocket Booster for UAV with Swirl Patterns Fabricated Using Scientific Workgroup for Rocketry H. Kawai, J. Harada, A. Banno, J. Oguro, Enhancement and Manufacturing Assisted Take Off Rapid Prototyping Technology and Spaceflight (WARR) I. Nakagawa, Tokai University, Hiratsuka, Techniques A. Bettella, F. Moretto, University of D. Armold, J. Boyer, K. Kuo, Pennsylvania S. Sudhof, Technical University of Munich, Japan S. Radinsky, J. Herrmann, L. Maltbie, J. Padua, Padua, Italy; E. Geremia, HIT09, State University, State College, PA; J. Munich, Germany Vanherweg, D. DeTurris, California State Padova, Italy; N. Bellomo, D. Pavarin, Fuller, J. Desain, T. Curtiss, The Aerospace Polytechnic University, San Luis Obispo, CA University of Padua, Padua, Italy; D. Corporation, Los Angeles, CA Petronio, HIT09, Padova, Italy Wednesday, 17 July 2013 212-ITAR-5 Thermal Management & Enegy Conversion Device Technologies (ITAR Restricted Session) 210 H Chaired by: C. TARAU, Advanced Cooling Technologies; D. SHAFER, GE Aviation and M. CHOI, NASA-Goddard Space Flight Center 1430 hrs 1500 hrs AIAA-2013-4142 AIAA-2013-4143 Loop Heat Pipe Deployable Radiator( Cylindrical Energy Storage Cooling LHP/DR) Engineering Development Architectures (ITAR Restricted Unit, EDU (ITAR Restricted Paper) Paper) S. Semenov, N. Gernert, Thermacore, Inc., G. Foshage, M. Bryant, RCT Systems, Lancaster, PA; B. Gardner, D. Bauer, B. Blake, Linthicum, MD Lockheed Martin Corporation, Sunnyvale, CA Wednesday, 17 July 2013 213-LP-30 Combustion Chamber Heat Transfer 210 F Chaired by: V. AHUJA, CRAFT Tech and M. MEYER, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs AIAA-2013-4144 AIAA-2013-4145 AIAA-2013-4146 Assessment of Film Cooling An Experimental Investigation on Design of an Experimental Campaign Characteristics in a GOX/ Kerosene the Steady State Heat Transfer on Methane Regenerative Liquid Rocket Combustion Chamber Characteristics of Liquid Methane Rocket Engine Cooling System C. Kirchberger, G. Schlieben, O. Haidn, A. Trejo, C. Garcia, A. Choudhuri, University R. Votta, F. Battista, M. Ferraiuolo, P. Roncioni, Technical University of Munich, Garching, of Texas, El Paso, El Paso, TX V. Salvatore, P. De Matteis, Italian Aerospace Germany Research Center (CIRA), Capua, Italy Wednesday, 17 July 2013

82 214-LP-31 Liquid Rocket Engines V 210 B Chaired by: C. KIRCHBERGER and S. FORDE, Aerojet Rocketdyne 1430 hrs 1500 hrs 1530 hrs AIAA-2013-4147 AIAA-2013-4148 AIAA-2013-4149 The Development Results of Main A Decade of Success and Innovation Development of the Bantam Family Engine (HBT-5) for HTV for Evolved Expendable Launch of Aerojet Rocketdyne Commercial Y. Tashiro, N. Matsuda, IHI Corporation, Vehicle Liquid Propulsion Systems Rocket Engines Gunma, Japan; S. Takata, Japan Aerospace I. Dawson, P. Dowler, G. Kontogiannis, G. D. Levack, W. Sack, Pratt & Whitney, Exploration Agency (JAXA), Ibaraki, Japan Pech, United Launch Alliance, Centennial, CO Canoga Park, CA Wednesday, 17 July 2013 215-LP-33 Ignition Systems 114 Chaired by: P. ALLIOT, Snecma S.A. and T. POURPOINT, Purdue University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2013-4150 AIAA-2013-4151 AIAA-2013-4152 AIAA-2013-4153 AIAA-2013-4154 Basic Characteristics of Reaction Feasibility Study of Low Frequency An Experimental Evaluation Effect of Jet Momentum Ratio and Hypergolic Propellant Ignition Initiation System Using Dishcharge Plasma for Bipropellant Thruster of a Torch Ignition System for Equivalence Ratio on the Ignition Phenomenon with Oxidizer Two- Plasma for 1N-class Thruster with Ignition Propulsion Research Process of TMEDA and White Phase Flow Injection Green Propellants T. Nagata, Japan Aerospace Exploration J. Flores, L. Sanchez, V. Dorado, A. Fuming Nitric Acid (WFNA) Y. Matsuura, Y. Tashiro, IHI Corporation, T. Iizuka, T. Shindo, J. Sato, Y. Sato, S. Agency (JAXA), Tsukuba, Japan; E. Choudhuri, University of Texas, El Paso, D. Bittner, J. Sell, G. Risha, Pennsylvania Gunma, Japan Kawabata, J. Aoyagi, H. Takegahara, Tokyo Besnard, California State University, Long El Paso, TX State University, Altoona, PA Metropolitan University, Hino, Japan; T. Beach, CA Nagata, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan Wednesday, 17 July 2013 216-LP-34 Liquid Rocket Combustion Modeling 111 Chaired by: D. PRECLIK, Astrium, an EADS Company and E. BESNARD, California State University-Long Beach 1430 hrs 1500 hrs 1530 hrs AIAA-2013-4155 AIAA-2013-4156 AIAA-2013-4157 Comparison of Reactive Flow Numerical Simulation of Kinetics Modeling of Hypergolic Simulations for a LOX/CH4 Uni- Combustion of Unlike Impinging Propellants element Rocket Jets Near a Wall S. Sardeshmukh, S. Heister, Purdue University, A. French, P. Roncioni, Italian Aerospace K. Park, S. Sardeshmukh, S. Heister, H. West Lafayette, IN; V. Sankaran, Air Force Research Center (CIRA), Capua, Italy Wang, Purdue University, West Lafayette, Research Laboratory, Edwards AFB, CA; H. IN Wang, Purdue University, West Lafayette, IN Wednesday, 17 July 2013 217-LP-35 German Liquid Rocket Propulsion (Invited) 210 A 1430 - 1730 hrs Chaired by: H. CIEZKI, DLR - German Aerospace Center

T. Kranz, DLR - Space Administration, et. al. N. Adams, Technical University Munich, et al. M. Oschwald, DLR - Institute of Space Propulsion, et al. Liquid Rocket Propulsion: Securing Europe’s Access to Space in a Changing Environment Concept and Operation of the Collaborative Research Center TRR 40 on Fundamental Research Activities on Liquid Rocket Research at DLR Institute of Space Propulsion Technologies of Liquid Rocket Propulsion A. Haberzettl, DLR - Institute of Space Propulsion, et al. G. Langel, Astrium, et al. G. Hagemann, Astrium, et al. DLR Lampoldshausen - Leading Edge Test Facilities for Propulsion System Development Rocket Propulsion System Developments in Germany and International Cooperations Technology Developments for Rocket Propulsion Systems in Germany and Qualification

83 Wednesday, 17 July 2013 218-NFF-8 Nuclear Thermal Propulsion IV: Testing and Programmatics 113 Chaired by: C. ENSWORTH, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2013-4158 AIAA-2013-4159 Oral Presentation (Invited) Oral Presentaiton (Invited) AIAA-2013-4161 Atmospheric Plasma Re-Entry Fuel Recapturing Graphite-Based Fuel Status on the Development Fuel Element Testing in the New Affordable Development and Failure Analysis Of Tungsten-Based Element Technology for Nuclear of Cermet Fuels for a Nuclear NTREES Facility Configuration Qualification Strategy for Nuclear Nuclear Thermal Rocket Fuel Thermal Propulsion Cryogenic Propulsion Stage (NCPS) W. Emrich, NASA Marshall Space Flight Thermal Propulsion T. Smith, G. Teel, M. Keidar, George M. Trammell, Oak Ridge National R. Hickman, J. Broadway, O. Mireles, D. Center, Huntsville, AL H. Gerrish, G. Doughty, NASA Marshall Washington University, Washington, DC Laboratory, Oak Ridge, TN Cavender, NASA Marshall Space Flight Space Flight Center, Huntsville, AL; S. Center, Huntsville, AL Bhattacharyya, RENMAR Enterprises, Inc., North Augusta, SC Wednesday, 17 July 2013 219-PANEL-13 The Aerospace Industry Coping with the Current Fiscal Environment 230 B 1430 - 1730 hrs The Panelists will provide a senior level perspective and discussion on how our Propulsion Industry is coping with and adjusting to maintain success in the current challenging fiscal environment. Moderator: Sandra Magnus, Executive Director, AIAA Panelists: Jaiwon Shin Henner Wapenhans Jim Maser Dale Carlson Ray Johnson NASA Associate Administrator for Aeronautics Head of Technology Strategy, Rolls-Royce Group plc Vice President for Corporate Strategy and Development General Manager Technology Strategy Vice President Space Launch Operations Gen Corp GE Aviation The Aerospace Corporation Wednesday, 17 July 2013 221-SCP-7 Systems Design, Engineering and Analysis II 231 Chaired by: A. TAITS, CDI-Aerospace 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2013-4162 AIAA-2013-4163 AIAA-2013-4164 AIAA-2013-4165 AIAA-2013-4166 AIAA-2013-4167 Prediction of Spacecraft Remaining Development of Chemical Development of an Instrument for Software for Design and Analysis of Aspects of Technology Program Influence Analysis of Geometrical Life - Challenges and Achievements Propulsion System for a Versatile Comparative Propulsion System Liquid Rocket Engine System Planning: Top-Down to Bottom-Up Parameters of Detonation Initiation R. Nariyoshi, S. Chernikov, B. Yendler, Lander Demonstrator Platform Studies S. Lee, T. Roh, Inha University, Incheon, J. Gilland, Ohio Aerospace Institute, with Hot Jet by Adaptive Mesh YSPM, Saratoga, CA D. Fiot, V. Coipeau, EADS, Les Mureaux, R. Gabrielli, University of Stuttgart, Stuttgart, South Korea Brookpark, OH Refinement Method France; P. Martin, L. Souverein, Space Germany; D. Petkow, ESA, Noordwijk, The X. Cai, J. Liang, Z. Lin, National University Transportation GmbH, Munich, Germany Netherlands; G. Herdrich, C. Lange, T. Mayer, of Defense Technology, Changsha, China; H. Roeser, University of Stuttgart, Stuttgart, F. Zhuang, Institute of Command and Germany Technology of Equipment, Beijing, China Wednesday, 17 July 2013 222-SR-10 Solid Fueled Famjet/Scramjet and Novel Propellants 230 A Chaired by: M. LANGHENRY, Raytheon Missile Systems 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2013-4168 Oral Presentation (Invited) AIAA-2013-4170 AIAA-2013-4171 Electrical Solid Propellants: A Applications of ramjets in tactical Combustion Characteristics of Development of AP/HTPB based Safe, Micro to Macro Propulsion missiles Boron Particles for Ducted Rockets Fuel-rich Propellant for Solid Technology K. Naumann, Bayern-Chemie, Traunstein, - Effects of Pressure Propellant Ramjet W. Sawka, M. McPherson, Digital Solid Germany N. Suzuki, T. Kuwahara, Nihon University, J. nanda, P. Ramakrishna, Indian Institute State Propulsion, LLC, Reno, NV Funabashi, Japan of Technology Madras, Chennai, India

84 Wednesday, 17 July 2013 223-SR-11 SRM Systems 210 G Chaired by: R. BLACK, Aerojet Rocketdyne and B. LEARY, Johns Hopkins University Applied Physics Laboratory 1430 hrs 1500 hrs 1530 hrs AIAA-2013-4172 AIAA-2013-4173 AIAA-2013-4174 VEGA Solid Rocket Motors Flight Solid Rocket Motors Technologies Numerical Simulation of the Performances results For Ariane 6 Zefiro 9 Performance Using a New F. Giliberti, M. Angelone, M. Fiorillo, Avio D. Boury, HERAKLES, Le Haillan, France; Dynamic SRM Ballistic Simulator S.p.A., Colleferro, Italy; C. Milana, ELV E. Robert, French Space Agency (CNES), R. Bertacin, F. Ponti, University of Bologna, S.p.A., Colleferro, Italy; F. Serraglia, ESA, Paris, France Bologna, Italy; A. Annovazzi, Avio S.p.A., Frascati, Italy Colleferro, Italy Wednesday, 17 July 2013 224-ST-2 Space Transportation II 213 Chaired by: M. SIR, The Aerospace Corporation 1430 hrs 1500 hrs 1530 hrs AIAA-2013-4175 AIAA-2013-4176 AIAA-2013-4177 The Benefits of an Advanced How Many Engines Should a Rocket The Utilization of Launch Vehicles Booster Competition for NASA’s Have? Core Stages and Propellant Depots Space Launch System G. Landis, NASA Glenn Research Center, for Human Space Exploration A. Crocker, S. Cook, K. Doering, Dynetics, Cleveland, OH A. Wilhite, D. Arney, P. Chai, S. Currey, Inc., Huntsville, AL; R. Bachtel, Pratt & Georgia Institute of Technology, Atlanta, Whitney, DeSoto, CA GA Author/Session Chair Index AbdelGhany, E., 136-APS-3 Arney, D., 224-ST-2 Benjamin, P., 10-EC-1 Bryant, M., 212-ITAR-5 Chelius, A., 90-ABPSI-7 Abdellatif, O., 197-TM-6 Asghar, A., 17-GTE-6 Bennett, R., 136-APS-3 Bryden, K., 138-TFES-2, 196-TFES-1 Chen, C., 57-TM-2, 63-EERE-4 Abe, T., 81-SR-1 Ashida, Y., 118-APC-4 Bennewitz, J., 107-LP-11, 203-EDU-4 Bucci, E., 113-SR-3, 163-SR-5 Chen, G., 99-EP-3 Abou-deif, T., 139-TM-4 Ashkar, H., 63-EERE-4 Benson, D., 174-APC-7 Bui, T., 144-APC-5 Chen, H., 60-ABPSI-5 Abuo ElKassem, E., 139-TM-4 Aso, S., 18-HR-1, 179-HR-7 Berdoyes, M., 112-SR-2 Bulman, M., 190-NFF-7 Chen, M., 57-TM-2 Acarer, S., 111-SCP-3 Aso, T., 165-APC-6, 176-EC-7 Berg, S., 144-APC-5 Burke, L., 190-NFF-7 Chen, S., 74-PC-13 Acosta-Zamora, A., 102-ITAR-1 Attaphong, C., 37-EERE-2 Bernstein, J., 14-GTE-2 Burkhalter, J., 40-GTE-8 Chen, T., 8-APC-1, 91-APC-3, 118-APC-4, 186-LP-27 Adesina, A., 197-TM-6 Attia, M., 39-GTE-7, 60-ABPSI-5, 143-ABPSI-9 Bertacin, R., 123-HR-3, 223-SR-11 Bushman, S., 68-LP-5 Chen, Y., 20-LP-1, 24-PC-1, 137-EC-6, 163-SR-5 Agarwal, R., 43-HSABP-2 Austin, B., 128-LP-15, 158-LP-20 Berton, J., 16-GTE-5 Butler, M., 61-APS-2 Chenevert, B., 183-LP-23 Agresta, A., 16-GTE-5, 44-HSABP-3, 62-EERE-3 Auxt, J., 134-ST-1 Besnard, E., 107-LP-11, 144-APC-5, 215-LP-33, Bux, S., 137-EC-6 Chenoweth, J., 161-SCP-5 Ahn, J., 66-HSABP-5, 127-LP-13 Axdahl, E., 66-HSABP-5, 125-HSABP-7 216-LP-34 Cadou, C., 49-PC-6 Chernikov, S., 221-SCP-7 Ahuja, V., 103-LP-7, 132-SCP-4, 185-LP-26, 213-LP-30 Azami, M., 180-HR-8 Bettella, A., 104-LP-8, 124-HR-4, 180-HR-8, 211-HR-11 Cai, G., 123-HR-3, 186-LP-27, 188-LP-29 Chernoray, V., 14-GTE-2 Aintablian, H., 9-APS-1 Bacha, C., 68-LP-5 Bhangale, R., 76-PC-15 Cai, X., 221-SCP-7 Chi, H., 43-HSABP-2 Ajmani, K., 41-GTE-9 Bachtel, R., 224-ST-2 Bhattacharyya, S., 218-NFF-8 Caillat, T., 137-EC-6 Chiba, M., 207-EP-15 Akbari, P., 63-EERE-4 Bade Shrestha, S., 55-PC-12 Bianchi, D., 18-HR-1, 163-SR-5, 193-SR-7 Canard-Caruana, S., 90-ABPSI-7 Chicatelli, A., 161-SCP-5 Akhil, A., 38-GEPC-1 Baglini, J., 95-ECS-1, 201-ECS-3 Biao, L., 43-HSABP-2 Canonica, M., 97-EP-1 Chinnathambi, P., 50-PC-7 Akiki, M., 113-SR-3 Bailey, J., 6-ABPSI-1 Biblarz, O., 204-EP-11 Cantwell, B., 18-HR-1, 124-HR-4, 180-HR-8, 211-HR-11 Chintalapati, S., 126-LP-12 Akkermans, R., 90-ABPSI-7 Baisden, A., 136-APS-3 Bichay, M., 95-ECS-1 Cao, H., 151-HSABP-8 Chiu, D., 148-EP-8, 207-EP-15 Akram, M., 138-TFES-2 Bakare, A., 139-TM-4 Biesbroek, R., 195-SR-9 Caramia, G., 42-GTE-10 Cho, M., 12-ES-1 Alajo, O., 139-TM-4 Balachandran, P., 163-SR-5 Bittner, D., 203-EDU-4, 215-LP-33 Carmicino, C., 179-HR-7 Cho, Y., 143-ABPSI-9 Alcindor, P., 175-APS-5 Baldauff, R., 198-TM-7 Black, R., 81-SR-1, 223-SR-11 Carpenter, C., 68-LP-5, 157-LP-19 Choi, C., 69-LP-6 Aldape, A., 175-APS-5 Balepin, V., 184-LP-24 Blake, B., 212-ITAR-5 Carr, G., 61-APS-2 Choi, H., 162-SCP-6 Alexeenko, A., 110-SCP-2 Ballard, R., 186-LP-27 Blakey, S., 138-TFES-2 Carrotte, J., 7-ABPSI-2 Choi, J., 43-HSABP-2 Allan, W., 17-GTE-6 Banno, A., 211-HR-11 Blanc, T., 13-GTE-1 Carter, C., 44-HSABP-3, 65-HSABP-4 Choi, M., 57-TM-2, 198-TM-7, 212-ITAR-5

85 Allcorn, E., 28-SCP-1 Banuti, D., 188-LP-29 Blodgett, K., 6-ABPSI-1 Casalino, L., 16-GTE-5, 180-HR-8 Chou, K., 209-EP-17 Allen, E., 136-APS-3 Bao, W., 152-HSABP-9 Blomberg, C., 134-ST-1 Casalis, G., 133-SR-4, 168-SR-6 Chou, T., 24-PC-1 Allen, M., 68-LP-5 Baran, A., 134-ST-1 Blot, D., 64-GTE-14 Caspermeyer, M., 153-ITAR-3 Choudhuri, A., 102-ITAR-1, 107-LP-11, 138-TFES-2, Alliot, P., 127-LP-13, 184-LP-24, 215-LP-33 Barata, J., 6-ABPSI-1 Bodart, J., 19-HSABP-1 Cassenti, B., 70-NFF-1, 189-NFF-6 153-ITAR-3, 196-TFES-1, 213-LP-30, 215-LP-33 AlShoaibi, A., 62-EERE-3 Barato, F., 124-HR-4 Böhm, C., 167-LP-22 Catalano, L., 42-GTE-10 Choueiri, E., 120-EP-5, 178-EP-10, 208-EP-16 Alsultan, A., 36-EERE-1 Barber, T., 133-SR-4, 188-LP-29 Boiron, A., 124-HR-4 Caux-Brisebois, V., 25-PC-3 Chowdhury, A., 49-PC-6, 76-PC-15, 79-PC-18 Amano, R., 36-EERE-1, 114-TM-3, 138-TFES-2 Barbour, E., 27-PC-5 Bonnici, M., 162-SCP-6 Cavallini, E., 133-SR-4, 163-SR-5 Chuck, C., 60-ABPSI-5 Ambekar, A., 49-PC-6, 76-PC-15, 79-PC-18 Barone, D., 32-ABPSI-3 Borner, A., 97-EP-1 Cavender, D., 218-NFF-8 Chue, R., 74-PC-13 Ambrose, H., 11-EC-2 Barthmes, S., 39-GTE-7 Borowski, S., 159-NFF-5, 190-NFF-7 Celik, M., 204-EP-11 Ciezki, H., 51-PC-8, 123-HR-3, 163-SR-5, 217-LP-35 Ambuken, P., 112-SR-2 Baruzzini, D., 84-ABPSI-6 Boss, M., 9-APS-1, 120-EP-5 Cengiz, K., 185-LP-26 Claflin, S., 100-HR-2 Anand, M., 25-PC-3, 51-PC-8 Basavanahalli, R., 46-LP-3 Boswell, R., 207-EP-15 Cervone, A., 181-HR-9 Clark, R., 55-PC-12 Anders, A., 175-APS-5 Bateup, M., 44-HSABP-3 Bouajila, W., 105-LP-9 Cesco, N., 113-SR-3 Cluff, R., 69-LP-6 Anderson, K., 203-EDU-4 Batonneau, Y., 79-PC-18 Boulanger, L., 121-EP-6 Chai, P., 224-ST-2 Codegone, M., 123-HR-3 Anderson, M., 134-ST-1 Batterson, J., 113-SR-3, 156-LP-18 Bourguignon, E., 9-APS-1 Chakroun, W., 140-TM-5 Cofer, A., 110-SCP-2 Anderson, W., 25-PC-3, 29-TM-1, 77-PC-16, 156-LP-18 Battista, F., 157-LP-19, 213-LP-30 Boury, D., 223-SR-11 Challa, S., 49-PC-6, 76-PC-15, 79-PC-18 Coffman, C., 119-EP-4, 177-EP-9 Andersson, N., 20-LP-1 Bauer, D., 212-ITAR-5 Boy, C., 70-NFF-1 Chambers, R., 9-APS-1 Coil, M., 79-PC-18 Andriani, R., 16-GTE-5, 44-HSABP-3, 62-EERE-3 Bayomy, A., 140-TM-5 Boyd, I., 121-EP-6 Chan, T., 11-EC-2, 94-EC-5 Coipeau, V., 221-SCP-7 Angelone, M., 223-SR-11 Beach, T., 17-GTE-6 Boyer, J., 102-ITAR-1, 166-EDU-2, 211-HR-11 Chandler, F., 162-SCP-6 Coles, T., 97-EP-1, 177-EP-9 Anjunyan, H., 137-EC-6 Beard, C., 7-ABPSI-2 Bradley, M., 38-GEPC-1 Chang, G., 57-TM-2 Connell, T., 150-HR-6 Annovazzi, A., 123-HR-3, 223-SR-11 Beaver, D., 153-ITAR-3 Bravato, A., 14-GTE-2, 197-TM-6 Chang, H., 143-ABPSI-9 Conners, T., 38-GEPC-1 Anthoine, J., 168-SR-6 Beckel, S., 65-HSABP-4 Breteau, J., 113-SR-3 Chang, J., 151-HSABP-8, 152-HSABP-9 Connolly, J., 161-SCP-5 Aoyagi, J., 215-LP-33 Becker, C., 181-HR-9 Brieda, L., 121-EP-6, 207-EP-15, 209-EP-17 Chap, A., 129-NFF-4 Conrad, M., 50-PC-7 Araki, K., 18-HR-1, 179-HR-7 Becnel, M., 179-HR-7 Brikner, N., 119-EP-4, 177-EP-9 Charles, C., 207-EP-15 Conteh, M., 92-APS-4 Araki, S., 148-EP-8 Behruzi, P., 126-LP-12 Broadway, J., 218-NFF-8 Chase, J., 137-EC-6 Conversano, R., 209-EP-17 Aramaki, S., 201-ECS-3 Belair, M., 159-NFF-5 Brooks, M., 210-HR-10 Chase, R., 91-APC-3 Convery, J., 41-GTE-9 Arestie, S., 118-APC-4 Bellomo, N., 124-HR-4, 211-HR-11 Brophy, C., 53-PC-10, 182-ITAR-4 Chato, D., 154-LP-16 Coogan, J., 100-HR-2 Armold, D., 166-EDU-2, 211-HR-11 Ben Nasr, N., 90-ABPSI-7 Brown, D., 206-EP-14 Chedevergne, F., 133-SR-4 Coogan, S., 150-HR-6, 210-HR-10 Arndt, C., 25-PC-3 Benchergui, D., 38-GEPC-1 Brown, G., 64-GTE-14 Chehroudi, B., 76-PC-15 Cook, S., 224-ST-2 Author/Session Chair Index Copenhaver, W., 143-ABPSI-9 Desmidt, H., 13-GTE-1 Fan, X., 43-HSABP-2, 55-PC-12 Gabrielli, R., 221-SCP-7 Gomes, J., 187-LP-28 Cornell, P., 10-EC-1, 29-TM-1, 57-TM-2 DeTurris, D., 211-HR-11 Farag, A., 57-TM-2 Gafni, G., 65-HSABP-4 Gomes, S., 179-HR-7, 195-SR-9, 201-ECS-3 Cornu, N., 205-EP-12 Devereaux, A., 155-LP-17 Farhat, R., 140-TM-5 Gaharan, C., 117-ABPSI-8 Gong, C., 44-HSABP-3 Cortopassi, A., 102-ITAR-1 Di Matteo, F., 127-LP-13 Faust, A., 99-EP-3, 208-EP-16 Gaitonde, D., 66-HSABP-5 Gorrell, S., 13-GTE-1, 15-GTE-3, 40-GTE-8, 69-LP-6, Couey, P., 40-GTE-8 Digiacinto, M., 163-SR-5 Favini, B., 163-SR-5 Galantini, P., 9-APS-1 143-ABPSI-9 Crane, S., 114-TM-3 Doering, K., 224-ST-2 Fayek AbdRabbo, M., 140-TM-5 Galbraith, R., 114-TM-3 Goto, D., 110-SCP-2 Crawford, M., 64-GTE-14 Dolan, B., 26-PC-4 Fedele, D., 123-HR-3 Gallimore, A., 206-EP-14, 209-EP-17 Gotzig, U., 79-PC-18 Crocker, A., 224-ST-2 Dolloff, M., 94-EC-5 Feili, D., 148-EP-8 Gamero, M., 97-EP-1, 119-EP-4 Goyne, C., 44-HSABP-3, 65-HSABP-4 Crofton, M., 122-EP-7, 204-EP-11, 209-EP-17 Domel, N., 84-ABPSI-6 Feldman, M., 120-EP-5 Gamma, F., 16-GTE-5, 44-HSABP-3, 62-EERE-3 Graham, P., 7-ABPSI-2 Csank, J., 161-SCP-5 Donahue, B., 134-ST-1 Feldman, T., 156-LP-18 Ganapathy, R., 165-APC-6 Grannan, N., 39-GTE-7 Cunha, F., 195-SR-9, 201-ECS-3 Dooley, M., 38-GEPC-1 Feng, S., 51-PC-8 Gandhi, R., 49-PC-6, 76-PC-15, 79-PC-18 Gray, J., 27-PC-5 Curgus, D., 38-GEPC-1 Dorado, V., 67-LP-4, 107-LP-11, 215-LP-33 Fernelius, M., 40-GTE-8 Gany, A., 12-ES-1, 74-PC-13, 180-HR-8 Grayson, G., 126-LP-12, 154-LP-16 Currey, S., 224-ST-2 Dorgan, A., 60-ABPSI-5, 84-ABPSI-6 Ferraiuolo, M., 213-LP-30 Garafolo, N., 102-ITAR-1 Greatrix, D., 113-SR-3, 163-SR-5, 168-SR-6, 194- Curriston, D., 40-GTE-8 Doughty, G., 218-NFF-8 Festa, G., 179-HR-7 Garcia, C., 213-LP-30 SR-8 Curtiss, T., 211-HR-11 Dowler, P., 214-LP-31 Feuerborn, S., 208-EP-16 Garcia, Z., 153-ITAR-3 Greig, A., 207-EP-15 d’Agostino, L., 67-LP-4, 69-LP-6, 187-LP-28 Driscoll, R., 15-GTE-3, 53-PC-10 Fiala, T., 78-PC-17 Gard, L., 136-APS-3 Gruber, M., 153-ITAR-3 Da Forno, R., 104-LP-8 Duchemin, O., 205-EP-12 Fickes, A., 203-EDU-4 Gardner, B., 212-ITAR-5 Grunder, Z., 67-LP-4 Dadone, A., 42-GTE-10 Dudzinski, L., 136-APS-3 Fidalgo, A., 203-EDU-4 Gardner, R., 10-EC-1 Guadagnoli, D., 126-LP-12, 154-LP-16 Dadson, J., 203-EDU-4 Dugala, G., 94-EC-5 Fiebig, M., 68-LP-5 Garner, C., 205-EP-12 Guenot, L., 113-SR-3 Dahms, R., 52-PC-9 Dukale, A., 76-PC-15 Fiorillo, M., 223-SR-11 Gascoin, N., 65-HSABP-4, 100-HR-2, 149-HR-5, Guntu, S., 40-GTE-8 Daimon, Y., 55-PC-12, 67-LP-4, 74-PC-13, 105-LP-9, Dunlap, P., 111-SCP-3, 132-SCP-4 Fiot, D., 221-SCP-7 150-HR-6, 181-HR-9, 210-HR-10 Guo, M., 152-HSABP-9 157-LP-19, 185-LP-26 Dupays, J., 194-SR-8 Firdosy, S., 137-EC-6 Gasner, S., 175-APS-5 Guo, T., 15-GTE-3 Dale, M., 39-GTE-7 Duque, E., 13-GTE-1 FIttje, J., 159-NFF-5 Gatto, C., 28-SCP-1, 67-LP-4 Guo, Y., 49-PC-6 Dally, B., 78-PC-17 Duven, D., 11-EC-2 Flamm, J., 32-ABPSI-3 Gauer, M., 79-PC-18 Gupta, A., 36-EERE-1, 62-EERE-3, 138-TFES-2

86 Dalton, P., 205-EP-12 Dyer, R., 153-ITAR-3 Fleeman, E., 203-EDU-4 Gautronneau, E., 113-SR-3 Gutierrez, H., 126-LP-12 Daniels, C., 102-ITAR-1 Dyson, C., 114-TM-3 Fleurial, J., 137-EC-6 Gawahara, K., 53-PC-10 Gutmark, E., 15-GTE-3, 26-PC-4, 53-PC-10 Dankongkakul, B., 148-EP-8 Ealy, B., 14-GTE-2 Flores, E., 203-EDU-4 Gazanion, B., 133-SR-4 Guynn, M., 16-GTE-5 Darbandi, M., 35-EC-3 Eberhart, C., 186-LP-27 Flores, J., 107-LP-11, 215-LP-33 Gea, L., 84-ABPSI-6 Haag, E., 175-APS-5 Darkwa, J., 139-TM-4, 140-TM-5 Edeline, E., 184-LP-24 Flynt, G., 14-GTE-2 Gejji, R., 25-PC-3 Haba, D., 126-LP-12 Davis, E., 129-NFF-4 Edlinger, E., 70-NFF-1 Forde, S., 214-LP-31 Genin, C., 103-LP-7 Haberbusch, M., 93-EC-4 Davitian, J., 18-HR-1, 149-HR-5 Edwards, C., 35-EC-3, 110-SCP-2 Forness, J., 75-PC-14 Geremia, E., 211-HR-11 Hagenmaier, M., 65-HSABP-4 Dawson, D., 19-HSABP-1 Ehlen, J., 181-HR-9 Forsythe, L., 114-TM-3 Gernert, N., 212-ITAR-5 Haidn, O., 213-LP-30 Dawson, I., 214-LP-31 Eilers, S., 149-HR-5, 179-HR-7 Foshage, G., 212-ITAR-5 Gerrish, H., 190-NFF-7, 218-NFF-8 Haines, J., 136-APS-3 de Groh, H., 132-SCP-4 Ekici, K., 13-GTE-1 Foster, J., 122-EP-7 Gerson, D., 203-EDU-4 Haller, W., 16-GTE-5 De Kock, E., 81-SR-1, 133-SR-4 Ekkad, S., 64-GTE-14 Fouad, M., 136-APS-3, 139-TM-4, 197-TM-6 Ghaddar, N., 36-EERE-1, 37-EERE-2, 62-EERE-3, Halliwell, I., 40-GTE-8 De la Cruz, F., 9-APS-1 El-Sayed, A., 136-APS-3 Fox, D., 203-EDU-4 63-EERE-4, 96-EERE-5, 140-TM-5 Hamada, T., 193-SR-7 de la Torre, M., 196-TFES-1 ElBialy, E., 140-TM-5 Fraeman, M., 11-EC-2 Ghali, K., 63-EERE-4, 96-EERE-5, 140-TM-5 Hamley, J., 136-APS-3 De Matteis, P., 213-LP-30 Elitzur, S., 12-ES-1 Frankel, A., 68-LP-5 Ghezzi, U., 16-GTE-5 Hammel, T., 136-APS-3 de O. Cachuté, L., 29-TM-1 Ellis, D., 57-TM-2 Frankford, D., 11-EC-2 Gibson, E., 28-SCP-1 Han, D., 121-EP-6 De Rosa, M., 127-LP-13 Ellis, R., 112-SR-2, 193-SR-7 Frederick, M., 38-GEPC-1 Giel, T., 20-LP-1 Händel, D., 39-GTE-7 de Saint Victor, X., 133-SR-4 Emrich, W., 190-NFF-7, 218-NFF-8 Frederick, R., 107-LP-11, 179-HR-7, 186-LP-27, Giliberti, F., 223-SR-11 Hannemann, K., 188-LP-29 Deans, M., 54-PC-11 Engelbrecht, C., 68-LP-5 203-EDU-4 Gilland, J., 118-APC-4, 221-SCP-7 Haobo, H., 51-PC-8 Decker, D., 92-APS-4 Englaro, A., 124-HR-4 Freeman, K., 203-EDU-4 Giusti, N., 177-EP-9 Har-Lev, D., 65-HSABP-4 Degges, M., 166-EDU-2 Ensworth, C., 190-NFF-7, 218-NFF-8 French, A., 216-LP-34 Gloyer, P., 46-LP-3, 156-LP-18 Harada, J., 211-HR-11 Deininger, W., 106-LP-10 Erickson, R., 77-PC-16 Friedrich, C., 92-APS-4 Goebel, D., 122-EP-7, 206-EP-14, 209-EP-17 Harada, N., 165-APC-6, 176-EC-7 Del Rosario, R., 8-APC-1 Eriksson, L., 20-LP-1 Fries, N., 126-LP-12 Goeke, J., 26-PC-4 Hardi, J., 78-PC-17 Delange, J., 184-LP-24 Esteyne, D., 117-ABPSI-8 Fu, Q., 46-LP-3 Gogna, P., 137-EC-6 Harold, H., 163-SR-5 Delfs, J., 90-ABPSI-7 Estivalezes, J., 133-SR-4 Fujii, G., 110-SCP-2 Goldin, G., 49-PC-6 Harrison, S., 203-EDU-4 Delot, A., 84-ABPSI-6 Evans, B., 18-HR-1, 150-HR-6, 211-HR-11 Fujiwara, H., 92-APS-4 Goljenboom, J., 10-EC-1 Hartenstine, J., 29-TM-1 Dennis, J., 100-HR-2, 167-LP-22 Eyi, S., 152-HSABP-9, 195-SR-9 Fukui, M., 66-HSABP-5 Gollahalli, S., 37-EERE-2 Hartfield, R., 40-GTE-8, 81-SR-1 Denny, M., 203-EDU-4 Ezekoye, O., 28-SCP-1 Fuller, J., 211-HR-11 Gollor, M., 9-APS-1 Hartwig, J., 154-LP-16 Desain, J., 211-HR-11 Faenza, M., 124-HR-4, 180-HR-8 Funaki, I., 81-SR-1, 118-APC-4, 122-EP-7 Golubev, M., 14-GTE-2 Harvazinski, M., 156-LP-18 Author/Session Chair Index Hasegawa, S., 33-ABPSI-4 Huang, W., 206-EP-14 Joyner, C., 91-APC-3 Kikuchi, T., 165-APC-6, 176-EC-7 Kulkarni, S., 17-GTE-6 Hassan, H., 19-HSABP-1, 125-HSABP-7 Hui, T., 93-EC-4 Ju, Y., 53-PC-10 Kilver, J., 161-SCP-5 Kumar, A., 125-HSABP-7 Hathaway, M., 8-APC-1 Huijsman, R., 181-HR-9 Judson, M., 149-HR-5 Kim, D., 107-LP-11 Kumar, S., 84-ABPSI-6 Hawkins, J., 32-ABPSI-3 Hupfer, A., 13-GTE-1 Juhls, A., 184-LP-24 Kim, J., 69-LP-6, 155-LP-17 Kuo, K., 102-ITAR-1, 166-EDU-2, 211-HR-11 He, B., 51-PC-8, 76-PC-15 Hurwitz, F., 57-TM-2 Jung, H., 155-LP-17 Kim, S., 19-HSABP-1 Kurosu, A., 105-LP-9 He, G., 19-HSABP-1 Husaboe, T., 25-PC-3 Kaemming, T., 153-ITAR-3 Kim, T., 190-NFF-7 Kuwahara, T., 181-HR-9, 222-SR-10 Heath, C., 25-PC-3 Hyams, D., 17-GTE-6 Kafafy, R., 176-EC-7, 180-HR-8 Kim, Y., 52-PC-9, 162-SCP-6 Kuznetsov, A., 65-HSABP-4 Heister, S., 41-GTE-9, 75-PC-14, 100-HR-2, Hynes, T., 16-GTE-5 Kagawa, H., 20-LP-1, 110-SCP-2, 183-LP-23 Kimber, R., 175-APS-5 Kuzuu, K., 105-LP-9 110-SCP-2, 149-HR-5, 194-SR-8, 216-LP-34 Ibekwe, V., 139-TM-4 Kajimura, Y., 118-APC-4, 122-EP-7 Kinefuchi, K., 81-SR-1 Kwon, O., 10-EC-1 Henderson, E., 91-APC-3 Ibrahim, M., 138-TFES-2, 139-TM-4, 140-TM-5 Kajiwara, K., 110-SCP-2, 154-LP-16, 183-LP-23 King, D., 98-EP-2 Kwon, S., 187-LP-28 Hendricks, E., 16-GTE-5, 64-GTE-14 Ibrahim, S., 62-EERE-3 Kakami, A., 155-LP-17, 193-SR-7, 207-EP-15 King, L., 97-EP-1, 119-EP-4, 209-EP-17 Lacaze, G., 52-PC-9 Henne, P., 38-GEPC-1 Ickes, J., 93-EC-4 Kalathas, L., 100-HR-2 Kirchberger, C., 188-LP-29, 213-LP-30, 214-LP-31 Lachmann, L., 143-ABPSI-9 Herdrich, G., 174-APC-7, 207-EP-15, 221-SCP-7 Idres, M., 176-EC-7, 180-HR-8 Kallina, P., 167-LP-22 Kirgiz, T., 111-SCP-3 Lacombe, A., 112-SR-2 Herman, D., 206-EP-14 Iha, K., 179-HR-7, 195-SR-9 Kamhawi, H., 121-EP-6, 205-EP-12, 206-EP-14 Kirik, J., 44-HSABP-3, 65-HSABP-4 LaFavor, J., 10-EC-1 Herring, N., 143-ABPSI-9 Ihme, M., 188-LP-29 Kanai, R., 181-HR-9 Kirk, D., 103-LP-7, 126-LP-12, 188-LP-29 Lai, A., 24-PC-1 Herrmann, J., 211-HR-11 Ihsan, S., 176-EC-7 Kang, S., 80-PC-19 Kirk, J., 111-SCP-3 Lam, G., 9-APS-1 Hickey, J., 188-LP-29 Iizuka, T., 215-LP-33 Kannepalli, C., 132-SCP-4 Kitaide, Y., 93-EC-4 Lambiase, E., 113-SR-3 Hickman, R., 218-NFF-8 Ikeda, H., 110-SCP-2 Kano, Y., 184-LP-24 Kiyak, Z., 81-SR-1 Landis, G., 61-APS-2, 93-EC-4, 175-APS-5, 224-ST-2 Hicks, F., 119-EP-4 Ilott, J., 17-GTE-6 Kapat, J., 14-GTE-2, 42-GTE-10, 64-GTE-14, Kizilkaya, B., 95-ECS-1 Lange, C., 221-SCP-7 Higashino, K., 117-ABPSI-8 Imai, K., 105-LP-9 157-LP-19, 197-TM-6 Klatte, J., 126-LP-12 Langendorf, S., 209-EP-17 Himeno, T., 46-LP-3, 104-LP-8, 126-LP-12, 188-LP-29 Inaba, Y., 181-HR-9 Karabeyoglu, A., 150-HR-6 Klausmann, J., 39-GTE-7 Langhenry, M., 81-SR-1, 195-SR-9, 222-SR-10 Hinerman, T., 156-LP-18, 185-LP-26 Ingenito, A., 16-GTE-5, 44-HSABP-3, 62-EERE-3 Karaki, S., 63-EERE-4 Klebanoff, L., 38-GEPC-1 Lapilli, G., 126-LP-12 Hiraiwa, T., 53-PC-10, 65-HSABP-4 Inoue, C., 46-LP-3, 126-LP-12, 188-LP-29 Karimi, A., 50-PC-7 Knoetze, J., 24-PC-1, 80-PC-19, 81-SR-1, 168-SR-6 Lara, L., 137-EC-6 Hirata, K., 166-EDU-2 Inuzuka, I., 45-LP-2 Karrer, N., 207-EP-15 Knop, T., 181-HR-9 Larson, L., 41-GTE-9, 203-EDU-4

87 Hirata, Y., 18-HR-1, 179-HR-7 Ishida, S., 93-EC-4 Kasahara, J., 53-PC-10 Knowlton, G., 146-ECS-2 Larusson, R., 20-LP-1 Hirota, M., 93-EC-4 Ishikawa, K., 126-LP-12 Kato, K., 33-ABPSI-4 Ko, H., 193-SR-7 Lau, M., 207-EP-15 Hitt, M., 100-HR-2, 185-LP-26 Ishiyama, T., 181-HR-9 Kato, N., 181-HR-9 Kobald, M., 123-HR-3 Laurent, F., 194-SR-8 Hoang, T., 198-TM-7 Isikveren, A., 8-APC-1 Kato, R., 181-HR-9 Kobayashi, T., 105-LP-9, 127-LP-13 Lavelle, T., 159-NFF-5 Hochwarter, D., 70-NFF-1 Ivanov, M., 79-PC-18 Katta, A., 133-SR-4 Koc, S., 95-ECS-1 Lazzarin, M., 104-LP-8, 124-HR-4 Hodges, J., 42-GTE-10, 197-TM-6 Iwasaki, Y., 93-EC-4 Katz, I., 206-EP-14 Kodera, M., 33-ABPSI-4 Leary, B., 133-SR-4, 195-SR-9, 223-SR-11 Hofer, R., 206-EP-14 Jackson, D., 95-ECS-1 Kau, H., 13-GTE-1 Koeck, J., 203-EDU-4 Lee, B., 101-HSABP-6 Hoke, J., 25-PC-3, 39-GTE-7, 40-GTE-8, 53-PC-10, Jacob, E., 156-LP-18, 185-LP-26 Kaur, P., 203-EDU-4 Koehler, H., 126-LP-12 Lee, C., 24-PC-1 153-ITAR-3 Jaekle, D., 68-LP-5 Kawabata, S., 215-LP-33 Köglmeier, S., 77-PC-16 Lee, D., 127-LP-13 Holen, S., 153-ITAR-3 Jaffe, R., 150-HR-6 Kawabata, Y., 183-LP-23 Kontogiannis, G., 214-LP-31 Lee, G., 107-LP-11 Holicker, C., 126-LP-12 Jansen, H., 153-ITAR-3 Kawai, H., 211-HR-11 Koo, H., 24-PC-1 Lee, H., 55-PC-12, 95-ECS-1, 146-ECS-2 Hoopes, K., 32-ABPSI-3 Jaramillo, M., 112-SR-2 Kawashima, H., 157-LP-19 Koo, J., 28-SCP-1, 107-LP-11, 112-SR-2 Lee, I., 107-LP-11 Hopkins, M., 209-EP-17 Jarman, J., 139-TM-4 Kawatsu, K., 105-LP-9 Korkut, B., 98-EP-2 Lee, J., 55-PC-12, 193-SR-7 Hori, K., 124-HR-4, 181-HR-9 JasperLal, C., 112-SR-2, 163-SR-5 Kees, D., 203-EDU-4 Kotine, A., 203-EDU-4 Lee, P., 41-GTE-9 Hornung, M., 8-APC-1 Javeed, A., 176-EC-7 Keidar, M., 148-EP-8, 207-EP-15, Kouwa, J., 188-LP-29 Lee, S., 52-PC-9, 80-PC-19, 186-LP-27, 221-SCP-7 Hosangadi, A., 132-SCP-4, 185-LP-26 Jensen, D., 167-LP-22 209-EP-17, 218-NFF-8 Koyuncuoglu, A., 176-EC-7 Lee, Y., 143-ABPSI-9, 162-SCP-6 Hosoi, J., 80-PC-19 Jézéquel, P., 168-SR-6 Kelbassa, I., 14-GTE-2 Kreiner, K., 45-LP-2, 105-LP-9 Lefkowitz, J., 53-PC-10 Hou, Z., 51-PC-8 Jin, P., 186-LP-27 Kestner, B., 161-SCP-5 Krishna, S., 196-TFES-1 Leitgeb, T., 33-ABPSI-4 Hourani, M., 96-EERE-5 Jin, Z., 44-HSABP-3 Keutelian, P., 99-EP-3 Krishnamoorthy, S., 203-EDU-4 Lekeux, A., 184-LP-24 Houts, M., 190-NFF-7 Jingyu, Z., 74-PC-13 Keyawa, N., 137-EC-6 Krishnamurthy, A., 99-EP-3 Lekzian, E., 35-EC-3 Howe, D., 38-GEPC-1 Johansson, M., 14-GTE-2 Keyser, S., 136-APS-3 Krishnan, G., 7-ABPSI-2 Lele, S., 19-HSABP-1 Howe, S., 134-ST-1 Johnson, J., 143-ABPSI-9 Khalil, E., 36-EERE-1, 37-EERE-2, 57-TM-2, 62-EERE-3, Krishnan, K., 197-TM-6 Lengyel-Kampmann, T., 90-ABPSI-7 Hrbud, I., 207-EP-15 Johnson, P., 64-GTE-14, 165-APC-6 63-EERE-4, 96-EERE-5, 136-APS-3, 139-TM-4, Krishnaraj, K., 112-SR-2 Leopold, L., 39-GTE-7 Hruby, V., 205-EP-12 Jones, D., 144-APC-5 140-TM-5, 197-TM-6 Kruhsel, G., 167-LP-22 Lepsch, R., 91-APC-3 Hsiao, R., 146-ECS-2 Jones, M., 13-GTE-1 Khalil Hasan, A., 138-TFES-2 Kubota, I., 184-LP-24 Levack, D., 91-APC-3, 214-LP-31 Hsu, K., 153-ITAR-3 Jones, S., 15-GTE-3 Khandelwal, B., 138-TFES-2, 196-TFES-1 Kuchana, V., 40-GTE-8 Leverone, F., 210-HR-10 Huang, C., 25-PC-3, 137-EC-6, 156-LP-18 Jorns, B., 206-EP-14 Khayms, V., 205-EP-12 Kuehl, H., 11-EC-2 Levin, D., 97-EP-1, 98-EP-2 Huang, J., 57-TM-2 Joubert, E., 117-ABPSI-8 Khoo, B., 27-PC-5 Külah, H., 176-EC-7 Lewandowski, E., 94-EC-5 Author/Session Chair Index Li, B., 137-EC-6 Malkin, P., 8-APC-1 Meier, W., 25-PC-3 Muralidharan, B., 27-PC-5 Ogedengbe, E., 63-EERE-4, 139-TM-4, 197-TM-6 Li, J., 27-PC-5, 43-HSABP-2 Mallick, L., 49-PC-6, 79-PC-18 Meiners, W., 14-GTE-2 Murayama, S., 110-SCP-2 Ogura, K., 127-LP-13 Li, P., 114-TM-3 Maltbie, L., 211-HR-11 Meiss, J., 144-APC-5 Murphy, J., 54-PC-11, 80-PC-19 Oguro, J., 211-HR-11 Li, X., 55-PC-12, 123-HR-3 Manente, M., 104-LP-8 Menon, S., 27-PC-5 Musielak, D., 43-HSABP-2, 101-HSABP-6 Ohe, K., 18-HR-1, 179-HR-7 Li, Z., 97-EP-1, 98-EP-2 Mankins, J., 36-EERE-1 Merkle, C., 156-LP-18 Muth, D., 36-EERE-1, 37-EERE-2, 62-EERE-3, 63- Ohira, T., 155-LP-17 Liang, J., 44-HSABP-3, 45-LP-2, 66-HSABP-5, Manoharan, S., 143-ABPSI-9 Merkley, D., 149-HR-5 EERE-4, 96-EERE-5 Okai, K., 92-APS-4 221-SCP-7 Marchandise, F., 205-EP-12 Mern, J., 43-HSABP-2 Muzyka, B., 29-TM-1 Okaya, S., 136-APS-3 Lienart, T., 68-LP-5 Marchionni, M., 127-LP-13 Messina, A., 10-EC-1 Nagata, H., 181-HR-9 Okita, K., 81-SR-1 Liffring, M., 92-APS-4 Marcu, B., 69-LP-6, 187-LP-28 Meyer, E., 97-EP-1 Nagata, T., 183-LP-23, 215-LP-33 Okutucu, T., 176-EC-7 Lilley, D., 138-TFES-2 Marcuccio, S., 177-EP-9 Meyer, K., 153-ITAR-3 Nakagawa, I., 211-HR-11 Oliphant, K., 69-LP-6 Lim, K., 27-PC-5 Marn, A., 33-ABPSI-4 Meyer, M., 213-LP-30 Nakano, M., 122-EP-7 Ombrello, T., 53-PC-10 Lin, B., 19-HSABP-1 Marshall, M., 15-GTE-3 Meyer, S., 41-GTE-9 Nakatsukasa, G., 137-EC-6 Onodaka, S., 181-HR-9 Lin, W., 17-GTE-6 Marshall, W., 54-PC-11 Michaels, D., 74-PC-13 Nakayama, H., 53-PC-10 Onodera, T., 184-LP-24 Lin, Y., 139-TM-4 Martellaro, P., 146-ECS-2 Miers, C., 28-SCP-1 Nalim, M., 50-PC-7 Onofri, M., 157-LP-19 Lin, Z., 221-SCP-7 Martin, H., 102-ITAR-1 Mikellides, I., 121-EP-6, 178-EP-10, 206-EP-14 nanda, J., 222-SR-10 Oravec, H., 102-ITAR-1 Lindemann, F., 181-HR-9 Martin, P., 221-SCP-7 Miklaszewski, E., 203-EDU-4 Naples, A., 153-ITAR-3 Oriti, S., 94-EC-5, 176-EC-7 Lineberry, D., 107-LP-11, 185-LP-26, 186-LP-27, Martinez-Sanchez, M., 121-EP-6 Milana, C., 223-SR-11 Naraghi, M., 45-LP-2, 63-EERE-4, 157-LP-19 Ortun, B., 90-ABPSI-7 203-EDU-4 Martins, A., 195-SR-9, 201-ECS-3 Miley, G., 99-EP-3 Nardi, R., 203-EDU-4 Oschwald, M., 78-PC-17 Liou, M., 13-GTE-1, 101-HSABP-6 Maruyama, N., 93-EC-4 Miller, J., 166-EDU-2 Nariyoshi, R., 221-SCP-7 Oshio, Y., 118-APC-4 Litke, P., 25-PC-3, 39-GTE-7 Massa, L., 75-PC-14, 125-HSABP-7 Miller, S., 106-LP-10, 155-LP-17 Nasuti, F., 18-HR-1, 157-LP-19 Ostlund, J., 20-LP-1 Litt, J., 15-GTE-3, 90-ABPSI-7 Masse, R., 68-LP-5, 155-LP-17 Minato, R., 117-ABPSI-8 Natali, M., 28-SCP-1 Otten, T., 90-ABPSI-7 Little, J., 208-EP-16, 209-EP-17 Massot, M., 194-SR-8 Ming-bo, S., 44-HSABP-3 Natan, B., 19-HSABP-1, 65-HSABP-4, 152-HSABP-9 Otting, W., 136-APS-3 Liu, J., 66-HSABP-5 Mastrangelo, G., 113-SR-3 Mingareev, I., 14-GTE-2 Natsui, G., 42-GTE-10 Overly, J., 68-LP-5 Liu, T., 99-EP-3 Masuda, I., 154-LP-16 Miranda, J., 50-PC-7 Naumann, K., 222-SR-10 Oyama, S., 18-HR-1, 179-HR-7

88 Liu, Y., 15-GTE-3 Masui, S., 207-EP-15 Mireles, O., 218-NFF-8 Naylor, R., 28-SCP-1 Ozcan, M., 161-SCP-5 Liu, Z., 45-LP-2 Masuoka, T., 154-LP-16, 183-LP-23 Miyazawa, T., 143-ABPSI-9 Neary, D., 208-EP-16 Ozyoruk, Y., 185-LP-26 Locke, J., 186-LP-27 Masuyama, K., 148-EP-8 Mizobata, K., 117-ABPSI-8 Negishi, H., 105-LP-9, 127-LP-13, 157-LP-19 Özyurt, O., 176-EC-7 Lohaus, A., 64-GTE-14 Matlock, T., 121-EP-6, 209-EP-17 Moeck, J., 27-PC-5 Negri, M., 51-PC-8 Pace, G., 67-LP-4, 69-LP-6, 187-LP-28, 195-SR-9 Longmier, B., 206-EP-14 Matsibeker, E., 152-HSABP-9 Moehlenkamp, R., 44-HSABP-3 Nesmith, B., 137-EC-6 Pack, S., 26-PC-4 Lorincz, I., 70-NFF-1 Matsuda, N., 67-LP-4, 214-LP-31 Mohan Das, P., 114-TM-3 Netter, G., 126-LP-12 Packard, T., 190-NFF-7 Loth, E., 32-ABPSI-3, 114-TM-3, 197-TM-6 Matsuno, S., 188-LP-29 Mon, K., 24-PC-1 Newman, R., 38-GEPC-1 Paik, J., 137-EC-6 Lotufo Lopes, M., 117-ABPSI-8 Matsuo, A., 143-ABPSI-9 Mongia, H., 26-PC-4, 41-GTE-9 Ng, W., 64-GTE-14 Palaszewski, B., 70-NFF-1 Loureda, O., 187-LP-28 Matsushita, T., 155-LP-17 Montgomery, S., 117-ABPSI-8 Nguyen, C., 93-EC-4 Palmer, P., 79-PC-18 Love, N., 196-TFES-1 Matsuura, Y., 215-LP-33 Moon, I., 80-PC-19, 186-LP-27 Nguyen, T., 74-PC-13 Pan, Y., 45-LP-2 Lozano, P., 97-EP-1, 118-APC-4, 119-EP-4, 148-EP-8, Matticari, G., 165-APC-6 Moretto, F., 180-HR-8, 211-HR-11 Nicke, E., 90-ABPSI-7 Pang, A., 121-EP-6 177-EP-9 Mavris, D., 7-ABPSI-2, 161-SCP-5 Morgan, C., 156-LP-18 Nie, W., 51-PC-8, 76-PC-15 Paradis, L., 113-SR-3 Lu, G., 111-SCP-3 Mayer, T., 221-SCP-7 Morgan, O., 183-LP-23 Niehuis, R., 39-GTE-7 Parfet, T., 175-APS-5 Lu, W., 74-PC-13 Maynes, D., 69-LP-6 Morgenweck, D., 77-PC-16 Nishida, H., 118-APC-4 Park, D., 187-LP-28 Lui, C., 38-GEPC-1 McCallum, P., 136-APS-3 Morii, Y., 105-LP-9, 185-LP-26 Nishikizawa, S., 155-LP-17 Park, J., 100-HR-2 Lundgreen, R., 69-LP-6 McCleskey, C., 91-APC-3 Morillon, T., 113-SR-3 Nocerino, J., 122-EP-7 Park, K., 194-SR-8, 216-LP-34 Lv, X., 19-HSABP-1 McCurdy, D., 190-NFF-7 Morita, T., 210-HR-10 Noda, J., 65-HSABP-4 Parthasarathy, R., 37-EERE-2 Lyons, J., 175-APS-5 McDonald, M., 206-EP-14 Morris, G., 110-SCP-2 Noguchi, R., 181-HR-9 Paschereit, C., 27-PC-5 Ma, M., 13-GTE-1 McGuirk, J., 7-ABPSI-2 Morton, C., 37-EERE-2 Nomura, H., 92-APS-4 Pasini, A., 67-LP-4, 69-LP-6, 187-LP-28, 195-SR-9 Ma, P., 188-LP-29 McKay, B., 33-ABPSI-4, 60-ABPSI-5, 84-ABPSI-6 Mostafa Ayoub, A., 140-TM-5 Nonaka, S., 126-LP-12 Pass, R., 35-EC-3 Mack, M., 111-SCP-3 Mckeever, C., 40-GTE-8 Motoe, M., 24-PC-1 Novara, C., 123-HR-3 Pastrone, D., 16-GTE-5, 123-HR-3, 149-HR-5, 1 Madavan, N., 8-APC-1 McKinney, R., 49-PC-6 Mourtos, N., 117-ABPSI-8 Nsofor, E., 92-APS-4, 139-TM-4 80-HR-8 Madhanabharatam, B., 100-HR-2, 123-HR-3, 181-HR-9 McLean, C., 106-LP-10 Munakata, T., 66-HSABP-5 Nunes Almeida, L., 179-HR-7, 195-SR-9, 201-ECS-3 Patel, A., 203-EDU-4 Maicke, B., 133-SR-4 McManus, K., 78-PC-17 Munday, D., 15-GTE-3, 26-PC-4, 53-PC-10 O’Brien, T., 151-HSABP-8 Patel, M., 175-APS-5 Majdalani, J., 113-SR-3, 123-HR-3, 133-SR-4, McNaul, E., 175-APS-5 Munenaga, T., 184-LP-24 O’Brien, W., 6-ABPSI-1, 32-ABPSI-3 Patterson, M., 122-EP-7, 204-EP-11, 205-EP-12 168-SR-6, 181-HR-9, 188-LP-29, 194-SR-8 McPherson, M., 222-SR-10 Munoz-Ramos, K., 38-GEPC-1 Odeshi, A., 197-TM-6 Pavacic, A., 166-EDU-2 Makarem, S., 63-EERE-4 McQuillen, J., 154-LP-16 Murakami, A., 33-ABPSI-4 Oefelein, J., 52-PC-9 Pavarin, D., 124-HR-4, 180-HR-8, 211-HR-11 Malak, M., 40-GTE-8 Medhat, A., 140-TM-5 Murakami, D., 70-NFF-1 Ogawara, A., 105-LP-9, 127-LP-13 Paxson, D., 15-GTE-3, 50-PC-7 Author/Session Chair Index Pech, G., 214-LP-31 Radhakrishna, D., 49-PC-6, 76-PC-15, 79-PC-18 Rosenfeld, J., 114-TM-3 Schnackel, J., 184-LP-24 Sinha, A., 76-PC-15 Pedersen, K., 67-LP-4 Radinsky, S., 211-HR-11 Roth, M., 94-EC-5 Schneider, D., 103-LP-7 Sir, M., 134-ST-1, 224-ST-2 Peltier, S., 44-HSABP-3, 65-HSABP-4 Raitses, Y., 121-EP-6 Rousseau, C., 24-PC-1, 80-PC-19, 81-SR-1, 113-SR-3, Schneider, G., 35-EC-3 Siri, K., 96-EERE-5 Pencil, E., 148-EP-8 Rajagopal, M., 50-PC-7 133-SR-4, 168-SR-6, 194-SR-8, 195-SR-9 Schnitzler, B., 159-NFF-5 Sirignano, W., 77-PC-16 Perdones-Diaz, D., 90-ABPSI-7 Ramakrishna, P., 222-SR-10 Rovey, J., 144-APC-5 Schreiber, J., 35-EC-3, 137-EC-6 Skoch, G., 17-GTE-6 Perez, V., 203-EDU-4 Rand, L., 178-EP-10 Roy, A., 64-GTE-14 Schuette, A., 126-LP-12 Slegers, N., 100-HR-2 Pergola, P., 177-EP-9 Randles, R., 175-APS-5 Ruf, J., 144-APC-5 Schulman, R., 126-LP-12 SMAOUI, H., 117-ABPSI-8 Perkins, H., 50-PC-7 Rangsten, P., 79-PC-18 Ruiz-Calavera, L., 90-ABPSI-7 Schulze, M., 77-PC-16 Smit, G., 24-PC-1, 80-PC-19, 81-SR-1, 133-SR-4, Perkins, J., 208-EP-16 Ransom, D., 69-LP-6, 102-ITAR-1, 187-LP-28 Russo, A., 179-HR-7 Schwendeman, C., 29-TM-1 195-SR-9 Perna, L., 119-EP-4 Rathakrishnan, E., 152-HSABP-9 Ryon, J., 26-PC-4 Scoccimarro, D., 113-SR-3 Smith, B., 121-EP-6, 122-EP-7 Perullo, C., 7-ABPSI-2, 42-GTE-10 Ravi, V., 137-EC-6 Sabouri, M., 35-EC-3 Scott, J., 129-NFF-4, 146-ECS-2 Smith, T., 218-NFF-8 Pestak, C., 36-EERE-1 Ravikrishna, R., 76-PC-15, 196-TFES-1 Sack, W., 214-LP-31 Sedwick, R., 99-EP-3, 120-EP-5, 129-NFF-4, 189-NFF-6 Snyder, P., 32-ABPSI-3 Peterleithner, J., 33-ABPSI-4 Ravlich, I., 203-EDU-4 Sackheim, R., 155-LP-17 Seitz, A., 8-APC-1 Sohn, C., 52-PC-9 Peters, C., 29-TM-1 Ray, M., 28-SCP-1 Safwat, H., 139-TM-4 Sekar, B., 43-HSABP-2 Son, S., 149-HR-5, 167-LP-22 Petkow, D., 221-SCP-7 Rayman, M., 205-EP-12 Sahara, H., 155-LP-17 Sekerak, M., 206-EP-14 Song, K., 49-PC-6 Petronio, D., 211-HR-11 Read, S., 16-GTE-5 Sahu, A., 196-TFES-1 Selim, H., 62-EERE-3 Song, M., 143-ABPSI-9 Pfaab, K., 68-LP-5 Reed, B., 106-LP-10 Saito, M., 93-EC-4 Sell, J., 203-EDU-4, 215-LP-33 Song, Z., 93-EC-4 Pfeiffer, J., 11-EC-2 Reisz, A., 110-SCP-2 Saito, T., 33-ABPSI-4 Semenov, S., 212-ITAR-5 Sordyl, J., 15-GTE-3 Pinero, D., 112-SR-2 Retief, F., 24-PC-1, 80-PC-19 Saitoh, Y., 183-LP-23 Sen, B., 49-PC-6 Soulas, G., 122-EP-7, 206-EP-14 Pinto, R., 201-ECS-3 Reyes, J., 176-EC-7 Sakaue, K., 181-HR-9 Seo, S., 80-PC-19 Souverein, L., 221-SCP-7 Pitot, J., 210-HR-10 Reynolds, K., 8-APC-1 Sakuranaka, N., 65-HSABP-4 Serraglia, F., 163-SR-5, 223-SR-11 Spadavecchia, U., 165-APC-6 Pizzarelli, M., 157-LP-19 Reza Ahrabi, B., 6-ABPSI-1 Salvatore, V., 213-LP-30 Sezaki, C., 127-LP-13 Spencer, A., 7-ABPSI-2 Planquart, P., 113-SR-3 Rhodes, R., 91-APC-3 Samarawickrama, K., 181-HR-9 Shafer, D., 102-ITAR-1, 153-ITAR-3, 212-ITAR-5 Spencer, S., 29-TM-1, 57-TM-2, 114-TM-3, Plasek, M., 178-EP-10 Riccius, J., 105-LP-9 Sanchez, L., 107-LP-11, 215-LP-33 Shahat, M., 197-TM-6 197-TM-6, 198-TM-7

89 Polanka, M., 25-PC-3, 50-PC-7 Rich, S., 134-ST-1 Sankaran, V., 25-PC-3, 156-LP-18, 216-LP-34 Shankar, V., 138-TFES-2 Spores, R., 106-LP-10 Polansky, J., 209-EP-17 Richard, S., 34-APC-2 Santavicca, D., 55-PC-12 Sharaf ELDin, A., 140-TM-5 Spotts, N., 60-ABPSI-5 Polk, J., 204-EP-11, 206-EP-14 Richardson, M., 14-GTE-2 Sarawate, N., 111-SCP-3 Shark, S., 149-HR-5 Spurling, J., 168-SR-6 Pollard, J., 209-EP-17 Ricklick, M., 14-GTE-2, 42-GTE-10, 64-GTE-14 Sardeshmukh, S., 216-LP-34 Shashurin, A., 148-EP-8 Sreenivas, K., 6-ABPSI-1, 14-GTE-2, 17-GTE-6 Ponti, F., 123-HR-3, 223-SR-11 Rideout, J., 203-EDU-4 Sargent, D., 104-LP-8, 154-LP-16 Shastry, R., 206-EP-14 Sridharan, P., 112-SR-2, 163-SR-5 Popov, P., 77-PC-16 Riehl, R., 29-TM-1 Saripalli, P., 120-EP-5 Shaw, K., 57-TM-2 Srinivasan, B., 40-GTE-8 Pourmousa, A., 114-TM-3 Riel, J., 203-EDU-4 Sarker, M., 196-TFES-1 Shaw, R., 12-ES-1 Srinivasan, V., 112-SR-2, 163-SR-5 Pourpoint, T., 75-PC-14, 106-LP-10, 149-HR-5, Rimoli, J., 209-EP-17 Sarmiento, C., 159-NFF-5 Sherburn, M., 150-HR-6 Srivastava, S., 152-HSABP-9 167-LP-22, 183-LP-23, 203-EDU-4, 215-LP-33 Risha, G., 150-HR-6, 203-EDU-4, 215-LP-33 Sasaki, T., 165-APC-6, 176-EC-7 Shi, L., 19-HSABP-1 St. George, A., 15-GTE-3, 53-PC-10 Powell, S., 181-HR-9 Rittenhouse, J., 25-PC-3 Sato, J., 215-LP-33 Shibamoto, H., 181-HR-9 St. John, C., 38-GEPC-1 Prabhakaran, R., 46-LP-3 Robert, E., 223-SR-11 Sato, S., 66-HSABP-5 Shigeizumi, M., 166-EDU-2 Starin, S., 153-ITAR-3 Prakash, A., 41-GTE-9 Roberts, L., 210-HR-10 Sato, Y., 215-LP-33 Shimada, T., 18-HR-1, 24-PC-1, 179-HR-7, 210-HR-10 Stark, R., 103-LP-7 Pranav, S., 189-NFF-6 Roberts, R., 92-APS-4 Sattelmayer, T., 77-PC-16, 78-PC-17 Shimizu, T., 12-ES-1, 105-LP-9, 185-LP-26 Starkey, R., 66-HSABP-5, 143-ABPSI-9, 162-SCP-6 Pratt, J., 38-GEPC-1 Robertson, P., 92-APS-4 Sauer, J., 184-LP-24 Shimoda, M., 193-SR-7 Steenkamp, A., 24-PC-1, 133-SR-4, 195-SR-9 Preclik, D., 216-LP-34 Robin, M., 206-EP-14 Saunders, G., 46-LP-3 Shindo, T., 215-LP-33 Steffan, S., 162-SCP-6 Prévost, M., 168-SR-6 Robinson, J., 34-APC-2, 91-APC-3, 144-APC-5, Sawka, W., 222-SR-10 Shinohara, I., 118-APC-4 Steinberg, A., 25-PC-3 Prévot, P., 168-SR-6 165-APC-6, 174-APC-7 Scaramuzzino, F., 179-HR-7 Shinozaki, N., 110-SCP-2 Steinetz, B., 111-SCP-3, 132-SCP-4 Prince, E., 203-EDU-4 Robinson, N., 166-EDU-2 Schaefer, B., 67-LP-4 Shipley, K., 156-LP-18 Stern, T., 29-TM-1, 175-APS-5 Pugmire, K., 128-LP-15, 158-LP-20 Rocco, J., 179-HR-7, 195-SR-9 Scharnhorst, R., 84-ABPSI-6 Shito, M., 45-LP-2 Stevens, C., 53-PC-10 Puleo, B., 132-SCP-4 Rocco, L., 179-HR-7 Schauer, F., 40-GTE-8, 53-PC-10, 153-ITAR-3 Shitta, M., 63-EERE-4 Stevens, J., 203-EDU-4 Purohit, A., 34-APC-2 Rockel, D., 13-GTE-1 Schenkman, B., 38-GEPC-1 Shoukath A, M., 165-APC-6 Stewart, M., 159-NFF-5 Qi, L., 43-HSABP-2 Rockstroh, U., 39-GTE-7 Schinder, A., 209-EP-17 Shulman, V., 143-ABPSI-9 Steyn, F., 81-SR-1 Qiao, L., 75-PC-14 Roeser, H., 221-SCP-7 Schlechtriem, S., 123-HR-3 Sibra, A., 194-SR-8 Stretz, H., 112-SR-2 Qin, C., 114-TM-3 Roh, T., 221-SCP-7 Schlieben, G., 213-LP-30 Sideris, A., 77-PC-16 Stuermer, A., 90-ABPSI-7 Qin, F., 19-HSABP-1 Rojo, B., 14-GTE-2 Schmid, M., 77-PC-16 Sievers, R., 136-APS-3 Su, D., 13-GTE-1 Qiu, S., 114-TM-3 Roncioni, P., 157-LP-19, 213-LP-30, 216-LP-34 Schmitz, B., 126-LP-12 Simeoni, F., 16-GTE-5, 180-HR-8 Su, L., 51-PC-8 Quay, B., 55-PC-12 Rose, L., 209-EP-17 Schmitz, P., 57-TM-2 Simon, T., 114-TM-3 Subramanian, S., 14-GTE-2 Quinlan, J., 167-LP-22 Rosenband, V., 12-ES-1 Schmuland, D., 68-LP-5 Simurda, L., 18-HR-1 Sudhof, S., 211-HR-11 Author/Session Chair Index Sugimori, K., 67-LP-4 Thorpe, D., 91-APC-3 Wang, H., 216-LP-34 Woods, E., 28-SCP-1 Zhang, S., 20-LP-1 Sullivan, J., 100-HR-2 Tian, H., 123-HR-3, 188-LP-29 Wang, J., 43-HSABP-2, 121-EP-6, 209-EP-17 Wordingham, C., 178-EP-10 Zhang, T., 43-HSABP-2 Sullwald, W., 195-SR-9 Tomioka, S., 33-ABPSI-4, 53-PC-10, 65-HSABP-4, Wang, L., 151-HSABP-8 Wrosch, M., 175-APS-5 Zhang, W., 13-GTE-1 Summers, M., 100-HR-2 143-ABPSI-9 Wang, P., 97-EP-1, 98-EP-2 Wu, J., 24-PC-1 Zhang, Z., 137-EC-6 Sun, M., 45-LP-2 Tomita, T., 143-ABPSI-9, 184-LP-24 Wang, T., 20-LP-1 Wucherer, E., 183-LP-23 Zhao, X., 20-LP-1 Sunakawa, H., 105-LP-9, 127-LP-13 Tong, M., 16-GTE-5 Warren, J., 159-NFF-5, 190-NFF-7 Wyczalek, F., 96-EERE-5 Zhao, Y., 66-HSABP-5 Sung, H., 125-HSABP-7 Topal, E., 111-SCP-3 Watanabe, D., 105-LP-9 Wyczalek, M., 96-EERE-5 Zheng, X., 111-SCP-3 Sung, M., 67-LP-4 Torre, L., 67-LP-4, 69-LP-6, 187-LP-28, 195-SR-9 Watanabe, H., 122-EP-7 Wyczalek, T., 96-EERE-5 Zhou, C., 93-EC-4 Supie’, P., 113-SR-3 Totani, T., 181-HR-9 Watanabe, S., 155-LP-17 Xiaomin, H., 74-PC-13 Zhuang, F., 46-LP-3, 51-PC-8, 76-PC-15, 221-SCP-7 Sutliff, T., 136-APS-3 Trammell, M., 218-NFF-8 Watanabe, T., 46-LP-3, 66-HSABP-5, 104-LP-8, Xie, J., 97-EP-1 Zhuang, T., 148-EP-8, 207-EP-15 Suzuki, N., 222-SR-10 Tran, V., 37-EERE-2 126-LP-12, 188-LP-29 Xu, J., 75-PC-14 Zilliac, G., 18-HR-1, 150-HR-6, 180-HR-8 Syphers, J., 166-EDU-2 Tran, Y., 154-LP-16 Waxman, B., 18-HR-1, 179-HR-7, 180-HR-8, Yabuhara, E., 110-SCP-2 Zimmerman, J., 18-HR-1, 180-HR-8 Syring, C., 174-APC-7 Traum, M., 10-EC-1 210-HR-10 Yada, K., 45-LP-2 Zink, G., 26-PC-4 Szabo, J., 178-EP-10, 206-EP-14 Trejo, A., 213-LP-30 Webster, R., 6-ABPSI-1, 14-GTE-2, 17-GTE-6, Yamada, K., 154-LP-16 Zinn, B., 167-LP-22 Tachibana, T., 155-LP-17, 193-SR-7, 207-EP-15 Trivedi, D., 111-SCP-3 201-ECS-3 Yamagiwa, Y., 118-APC-4 Zorlu, O., 176-EC-7 Tagashira, T., 92-APS-4 Tsai, J., 57-TM-2 Wegeng, R., 36-EERE-1 Yamaguchi, S., 210-HR-10 Zulkefli, Z., 134-ST-1 Tai, J., 16-GTE-5, 161-SCP-5 Tsuchiya, T., 93-EC-4 Wei, X., 19-HSABP-1 Yamakawa, H., 118-APC-4 Zuniga, H., 64-GTE-14 Taits, A., 129-NFF-4, 221-SCP-7 Turkoz, E., 204-EP-11 Wei, Z., 43-HSABP-2, 152-HSABP-9 Yamamura, H., 118-APC-4 Zurbach, S., 205-EP-12 Tajmar, M., 70-NFF-1, 129-NFF-4, 177-EP-9 Tyson, R., 166-EDU-2, 203-EDU-4 Welch, G., 17-GTE-6 Yamanaka, M., 155-LP-17 Takahashi, H., 143-ABPSI-9 Ubogu, E., 138-TFES-2 Weldy, K., 198-TM-7 Yamanishi, N., 105-LP-9, 127-LP-13, 157-LP-19 Takahashi, K., 80-PC-19 Uchida, M., 80-PC-19 Wen, C., 27-PC-5 Yanagi, R., 92-APS-4 Takaki, R., 122-EP-7 Ueda, S., 184-LP-24 Werner, R., 181-HR-9 Yang, J., 186-LP-27 Takata, S., 67-LP-4, 214-LP-31 Uematsu, T., 181-HR-9 Weston, D., 15-GTE-3 Yang, L., 46-LP-3, 95-ECS-1 Takayanagi, S., 176-EC-7 Ueno, K., 118-APC-4 Whitlock, C., 118-APC-4 Yang, Q., 152-HSABP-9

90 Takegahara, H., 215-LP-33 Uhl, D., 137-EC-6 Whitmore, S., 124-HR-4, 149-HR-5, 179-HR-7 Yang, V., 43-HSABP-2, 125-HSABP-7 Takegoshi, M., 33-ABPSI-4 Ulas, A., 95-ECS-1 Wiegand, B., 138-TFES-2 Ye, Z., 13-GTE-1 Takiguchi, K., 93-EC-4 Ulmen, B., 99-EP-3 Wiegerink, R., 79-PC-18 Yee, C., 28-SCP-1 Talley, D., 156-LP-18 Um, D., 10-EC-1 Wierman, M., 77-PC-16 Yendler, B., 221-SCP-7 Tam, J., 153-ITAR-3 Umemura, Y., 104-LP-8, 126-LP-12 Wiest, H., 41-GTE-9 Yentsch, R., 66-HSABP-5 Tanaka, S., 80-PC-19 Underwood, C., 12-ES-1 Wilfing, G., 201-ECS-3 Yetter, R., 150-HR-6 Tanatsugu, N., 117-ABPSI-8 Uzawa, S., 46-LP-3 Wilhite, A., 125-HSABP-7, 224-ST-2 Yi, J., 74-PC-13 Tang, F., 28-SCP-1 Valentini, D., 67-LP-4, 69-LP-6, 187-LP-28, 195-SR-9 Williams, G., 29-TM-1, 118-APC-4 Yilmaz, M., 95-ECS-1 Tang, X., 19-HSABP-1 Van De Ven, J., 114-TM-3 Williams, J., 178-EP-10 Yim, J., 106-LP-10, 205-EP-12 Tangirala, V., 152-HSABP-9, 182-ITAR-4 Vanherweg, J., 211-HR-11 Williams, S., 207-EP-15 Yonezawa, R., 166-EDU-2 Tani, K., 33-ABPSI-4 Veale, K., 210-HR-10 Wilson, C., 138-TFES-2 Yoon, C., 25-PC-3 Tani, N., 105-LP-9, 127-LP-13 Verma, S., 157-LP-19 Wilson, D., 198-TM-7 Young, G., 150-HR-6 Tani, Y., 18-HR-1, 179-HR-7 Villalva Gomez, R., 26-PC-4 Wilson, J., 50-PC-7 Young, J., 122-EP-7, 204-EP-11 Tanvir, S., 75-PC-14 Villarreal, J., 100-HR-2 Wilson, M., 68-LP-5 Young, K., 13-GTE-1 Tao, H., 152-HSABP-9 Vireira, W., 187-LP-28 Wilson, S., 35-EC-3 Yu, G., 43-HSABP-2 Taraschi, P., 166-EDU-2 Vitucci, J., 99-EP-3, 207-EP-15 Wingborg, N., 54-PC-11 Yu, N., 123-HR-3, 188-LP-29 Tarau, C., 29-TM-1, 114-TM-3, 197-TM-6, 212-ITAR-5 Vivek, B., 165-APC-6 Wink, J., 181-HR-9 Yu, S., 74-PC-13 Tarditi, A., 129-NFF-4 Viviani, A., 179-HR-7 Winkler, C., 60-ABPSI-5, 84-ABPSI-6 Yu, X., 181-HR-9 Tashiro, Y., 67-LP-4, 214-LP-31, 215-LP-33 Votta, R., 157-LP-19, 213-LP-30 Winters, B., 102-ITAR-1, 104-LP-8 Yuan, Y., 43-HSABP-2 Teel, G., 148-EP-8, 218-NFF-8 Wacker, C., 39-GTE-7 Wirz, R., 120-EP-5, 148-EP-8, 209-EP-17 Yuasa, S., 210-HR-10 Telitschkin, D., 79-PC-18 Wada, Y., 181-HR-9 Wise, B., 126-LP-12 Yumusak, M., 195-SR-9 Teo, C., 27-PC-5 Wakita, M., 181-HR-9 Witcher, J., 61-APS-2 Yungster, S., 50-PC-7 Terhune, K., 97-EP-1 Walker, A., 7-ABPSI-2 Witty, W., 183-LP-23 Zakrajsek, J., 136-APS-3 Thakur, S., 188-LP-29 Walker, K., 29-TM-1 Woisetschläger, J., 33-ABPSI-4 Zametaev, E., 105-LP-9 Thalamy, M., 184-LP-24 Walker, M., 99-EP-3, 209-EP-17 Wolfe, C., 111-SCP-3 Zandbergen, B., 181-HR-9 Thatte, A., 132-SCP-4 Wan, J., 28-SCP-1 Wolford, D., 10-EC-1 Zaseck, C., 149-HR-5 Thayer, J., 114-TM-3 Wang, B., 57-TM-2 Wong, D., 112-SR-2 Zeng, P., 188-LP-29 Thornock, R., 60-ABPSI-5 Wang, C., 57-TM-2 Woodason, R., 17-GTE-6 Zhang, L., 125-HSABP-7 SAN JOSE LL21A LL20A CONVENTION LL21B LL20B LL21C PREFUNCTION CENTER LL20C LL21D VENUE MAP – SAN JOSE CONVENTIONLL20D CENTERLL21E

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CONCOURSE (Upper Level) www.aiaa.org/jpc2013 • www.iecec.org 91 #aiaaPropEnergy 28–30 JULY 2014 CLEVELAND, OHIO CALL FOR PAPERS OPENS: SEPTEMBER 2013

FEATURING • 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference • 12th International Energy Conversion Engineering Conference

www.aiaa.org/propulsionenergy2014 #aiaaPropEnergy