2O15 27–29 JULY 2015 ORLANDO, FL

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NO DOWNLOADING REQUIRED! Executive Steering Committee AIAA Propulsion and Energy 2015

Welcome The members of the Executive Steering Committee welcome you to the AIAA Propulsion and Energy Forum and Exposition 2015 (AIAA Propulsion and Energy 2015) with excitement and anticipation. Our community has made great strides over the past several years in alternative fuels, renewable energy, and sustainable energy Phil Burkholder Michael Heil programs. As we move forward in our exploration of the world and the universe, Rolls-Royce Ohio Aerospace discussions about continually increasing the efficiency, reliability, and sustainability Institute of energy systems are critical.

While here in Orlando for AIAA Propulsion and Energy 2015, we encourage you to engage with your colleagues from government, industry, and academia, and discuss the national and international outlook for energy and propulsion systems, global economic interdependence, the cost and affordability of future systems, technology development trends, workforce development, and much more. All of these conversations will rest on the foundation of our theme for the week: “Energize Innovation. Boost Value. Propel The Future.” Bob Hwang John Kinney Sandia National GE Aviation You will find the plenary themes woven into our panel and technical discussions, Laboratories allowing deeper examination of all aspects of energy and propulsion systems, including: electric propulsion, ground test capability, in-space propulsion, the need for effective communication with the media, and how STEM professionals can achieve a healthy work/life balance. In three intense days, AIAA Propulsion and Energy 2015 will help you gain knowledge in these important areas, while also allowing you to build contacts and do the networking necessary for future innovative collaborations and partnerships.

Thank you for making the choice to attend this year’s event, and for your continued Christian Mari Charles Precourt enthusiasm to advance the boundaries of the known in energy and propulsion SAFRAN Group Orbital ATK systems. We trust that the conversations and information shared this week will continue to drive cost savings, efficiency, and responsiveness of energy systems ever forward. And, more importantly, remember that the forum is a testament to how your work fuels the collective human drive to better humanity’s technological capabilities and to be part of something bigger than ourselves. This is your forum, and we hope that you will enjoy it and take full advantage of its offerings.

Sincerely,

Woodrow Whitlow Jr. Executive Steering Committee Cleveland State University AIAA Propulsion and Energy 2015

51st AIAA/SAE/ASEE Joint AIAA Propulsion and Energy Propulsion Conference 2015 is proud to feature the following conferences: 13th International Energy Conversion Engineering Conference www.aiaa-propulsionenergy.org 3 #aiaaPropEnergy IntroOrganizing Committee

Forum Organizing Committee Air Breathing Propulsion Systems Integration Propellants and Combustion Neal Herring, United Technologies M. Anand, Rolls-Royce Corporation Forum General Chair Research Center Charles Precourt, Orbital ATK Propulsion and Power Systems of Aircraft Electric Propulsion Unmanned Systems Forum 360 Chair Charles Beard, The Boeing Company Lea-Der Chen, University of Iowa Christine Pastor-Barsi, HX5 Sierra Electricity Delivery and Grid Reliability Propulsion Education and ASEE Forum Technical Chair Technologies and Energy Conversion Representative Gerard Welch, NASA Glenn Research Device Technology Robert Frederick, University of Alabama in Center Scott Duncan, Georgia Institute of Huntsville Technology Education Chair SAE Representative Steve Gorrell, Brigham Young University Electric Propulsion Richard Millar, Naval Postgraduate School John Dankanich, NASA Marshall Space International Chair Flight Center Solid Rockets Claudio Bruno, United Technologies David Poe, Aerojet Rocketdyne Corporation Energetic Components and Systems Brian Smith, Pacific Scientific Energetic Space and Earth-to-Orbit Vehicles Systems Member Engagement Chair Materials Company Miroslav Sir, The Aerospace Corporation G. Alan Lowrey, Lockheed Martin Corporation Energy Storage Technology System Concepts and Supporting Joe Troutman, EnerSys/ABSL Space Propulsion Technologies Young Professional Chair Products Corinne Gatto, Jet Propulsion Laboratory Tim Hinerman, Blue Origin Energy Conversion Device Technology Jeff McGivern, Jetboil Edward Lewandowski, NASA Glenn Special Advisor Research Center Don Sauvgeau, Orbital ATK Fossil-Fuel Power Technologies Bhupendra Khandelwal, University of Technical Program Committee Sheffield Forum Technical Program Chair Gas Turbine Engines Gerard Welch, NASA Glenn Research Jay Kapat, University of Central Florida Center Robert Thacker-Dey, Naval Air Systems Deputy Technical Chair – Energy and Command (NAVAIR) Thermal Management Technology Green Engineering/Green Energy Michael Choi, NASA Goddard Space Flight Valerie Lyons, NASA Glenn Research Center Center (retired) Deputy Technical Chair – Aviation High Speed Air Breathing Propulsion Jason Smith, GE Aviation Faure “Joel” Malo-Molina, Air Force ITAR Chair Research Laboratory Paul Smith, Boeing Commercial Airplanes Hybrid Rockets Advanced Engine Control & Intelligent Bala (Han) Madhan, SPG Liquid Systems Propulsion Alireza Behbahani, U.S. Air Force Liquid Propulsion Advanced Propulsion Concepts and ASME TC David Ransom, Southwest Research Representative Institute John Robinson (retired) Nuclear and Future Flight Propulsion Advanced Vehicle Systems Greg Meholic, The Aerospace Corporation Frank Chandler, The Boeing Company Nuclear Power Technologies Aerospace Power Systems Pavel Tsvetkov, Texas A&M University Abbas Salim, Lockheed Martin Corporation (retired) www.aiaa-propulsionenergy.org 4 #aiaaPropEnergy IntroContents

Welcome 3

Organizing Committee 4

Forum Overview 6

Sponsors 8 www.twitter.com/aiaa Keynote Speakers and Plenary Sessions 9 www.facebook.com/AIAAfan Forum 360 11

www.youtube.com/AIAATV Special Events 14

www.linkedin.com/companies/aiaa Networking Events 15

www.flickr.com/aiaaevents Continuing Education 16 www.instagram.com/aiaaerospace Recognition Events 17 livestream.com/AIAAvideo/PropEnergy2015 Exposition Hall 19 Join the conversation! Join the Q&A! Exhibitors 21 #aiaaPropEnergy aiaa.cnf.io

General Information 26 On-Site Wi Fi Information Network Name: PE2015 Author and Session Chair Information 28 Password: propenergy

ITAR Information 29 Photography or the video or audio recording of sessions or exhibits, as well as the Committee Meetings 30 unauthorized sale of AIAA-copyrighted material, is prohibited. Sessions at a Glance 31 AIAA is the world’s largest aerospace professional society, serving a diverse range of more than 30,000 Session Detail Matrix 36 individual members from 88 countries, and 95 corporate members. AIAA members help make the world safer, more connected, more accessible, and more prosperous. Author/Session Chair Index 83 For more information, visit www.aiaa.org, or follow us on Twitter @AIAA. Venue Map 90 www.aiaa-propulsionenergy.org 5 #aiaaPropEnergy IntroForum Overview

MONDAY TUESDAY WEDNESDAY 27 July 28 July 29 July Speakers’ Briefing in Technical Session Rooms Speakers’ Briefing in Technical Session Rooms Speakers’ Briefing in Technical Session Rooms 0730hrs (both am & pm sessions) (both am & pm sessions) (both am & pm sessions)

0800 hrs Opening Plenary Keynote Plenary Panel Plenary Panel 0830 hrs

0900 hrs Networking Coffee Break in Exposition Hall Networking Coffee Break in Exposition Hall Networking Coffee Break in Exposition Hall

0930 hrs

1000 hrs Technical Technical Exposition Technical Sessions Exposition Sessions Hall Open Sessions Exposition 1030 hrs Forum 360 Forum 360 Forum 360 Hall Open Hall Open 1100 hrs

1130 hrs

1200 hrs Box Lunch in Exposition Hall (ticket required) 1230 hrs Luncheon on Own Forum Recognition Luncheon

1300 hrs Exposition 1330 hrs Plenary Panel Hall Open Exposition 1400 hrs Plenary Panel Closing Plenary Keynote Hall Open 1430 hrs Networking Ice Cream Break in Exposition Hall

1500 hrs Networking Popcorn Break in Exposition Hall Exposition Hall Open 1530 hrs Exposition Hall Open Technical 1600 hrs Rising Leaders Forum 360 Technical Technical Sessions Forum 360 in Aerospace Leadership Sessions 1630 hrs Sessions Forum 360 Exchange/ Speed 1700 hrs Mentoring

1730 hrs

1800 hrs Reception in Exposition Hall Propulsion and Energy Lecture 1830 hrs (ticket required) 1900 hrs

1930 hrs

2000 hrs Rising Leaders in Aerospace Lecture

2030 hrs

www.aiaa-propulsionenergy.org 6 #aiaaPropEnergy Get Your Conference Info on the Go!

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AIAA would like to thank the following organizations for their support of AIAA Propulsion and Energy 2015 Executive Sponsor

Rising Leaders in Aerospace Sponsors

Twitter Board Sponsor Lanyard Sponsor

Valves for Propulsion Flight Ground

Supporting Sponsors

Media Sponsors

www.aiaa-propulsionenergy.org 8 #aiaaPropEnergy IntroKeynote Speakers and Plenary Sessions

Get the big picture on propulsion and energy from the thought leaders in the field during these high-level discussions and presentations.

Michael Hawes, Vice President, Orion Program Manager, Monday, 27 July Lockheed Martin Corporation Lee Monson, The Boeing Company (retired) 0800–0900 hrs Orange Ballroom D Mark Sirangelo, Corporate Vice President, Space Systems, Keynote Address Sierra Nevada Corporation Aviation Innovation 1300–1430 hrs Orange Ballroom D Christopher (Chris) Lorence, General Manager, Engineering Technologies, GE Aviation Technology Development and Trends in Propulsion and Energy Panel 1330–1500 hrs Orange Ballroom D Panelists will discuss the major technology challenges and opportunities that will shape the future of propulsion and Global Cooperation and Economic Development Panel energy, and how those challenges and opportunities should be addressed. The current international environment has introduced significant challenges to global cooperation, particularly Moderator: Graham Warwick, Managing Editor, Technology, in the propulsion community. This panel will examine the Aviation Week & Space Technology implications of the changing geopolitical landscape and the Panelists: importance of international cooperation in our industry. How do partners cooperate without becoming overly dependent on Jean Botti, Chief Technical Officer, Airbus any one player? Neil Garrigan, Executive Manager, Energy Systems and Technology, GE Aviation Moderator: James Maser, Vice President, Strategy, Marketing, & Business Development, Pratt & Whitney Doug Juul, Manager, Systems Technology, Lockheed Martin Corporation Panelists: Tom Williams, Director, Propulsion Systems Department, NASA Marshall Space Flight Center Jean-Paul Ebanga, President and CEO, CFM International Les Kovacs, Director, Washington Ops, United Launch Alliance (ULA) 1800–1900 hrs Orange Ballroom D Richard “Ric” Parker, Director of Research & Technology, Rolls-Royce plc Propulsion and Energy Lecture Marc Vales, Head of Future Programs, Airbus Safran e Transformation of the Kennedy Space Center Launchers An informational presentation on the transformation of the Bernard Zimmerman, Vice President, Group Strategy and Kennedy Space Center from a single, program-dependent Development, Pratt & Whitney launch complex, to a diverse, multi-user spaceport of the future enabling both government and commercial Tuesday, 28 July operations to and from low Earth orbit and beyond. The presentation will discuss the planning and execution of the Center’s transition from the 30-year Shuttle program; 0800–0900 hrs Orange Ballroom D the modernization of launch and ground processing Cost and Affordability of Future Systems Panel infrastructure to support NASA’s evolving Space Launch System and Orion multi-purpose crew vehicle; and the Panelists will discuss the key issues and approaches associated turnover of facilities and assets left underutilized by the with making future systems less costly and more affordable, retirement of the space shuttles to private industry and other and how to manage the balance between customer and seller government agencies. Challenges related to downsizing of needs. workforce, budget constraints, and contract and agreement Moderator: Michael Griffin, Chairman and CEO, Schafer strategies will be discussed, as well as overcoming barriers to Corporation change. In addition, the presentation will describe NASA’s journey to Mars and the critical work taking place at Kennedy Panelists: Space Center to enable it. Frank Culbertson, President, Space Systems Group, Robert Cabana, Center Director, NASA Kennedy Space Orbital ATK Center (continued) www.aiaa-propulsionenergy.org 9 #aiaaPropEnergy Keynote Speakers and Plenary Sessions

Wednesday, 29 July

0800–0900 hrs Orange Ballroom D Workforce Development Panel Discover how the makeup of the workforce will change over the next decade, how we need to adapt, and how to attract the necessary talent. Moderator: Mark Lewis, Director, IDA Science and Technology Policy Institute Panelists: Steve Gorrell, Associate Professor, Brigham Young University Michael Hawes, Vice President, Orion Program Manager, Lockheed Martin Corporation Carole Hedden, Executive Editorial Director, Aviation Week Executive Intelligence Yvette Weber, Engineering Manager, Air Force Material Command, U.S. Air Force

1330–1500 hrs Orange Ballroom D Keynote Developing Creative Storytelling Using Model- Based Design Michael Tschanz, Director, Technology & Analysis, Design and Engineering, Walt Disney World

www.aiaa-propulsionenergy.org 10 #aiaaPropEnergy IntroForum 360

1530–1800 hrs Orlando IV Government Investments Enabling Advancement of In-Space Propulsion The competition in the global space propulsion market continues to increase as nontraditional entities develop and demonstrate space propulsion devices. In this environment, U.S. industry continues to invest in strategy, concepts, and technology to maintain a healthy share of the market beyond the delivery of government assets. Simultaneously, U.S. government agencies These conversations will cover a spectrum of continue to infuse multiple programs to push the boundary timely topics including programs, systems, policy, of technical capabilities. The challenge is to align the focus of government-funded technology with the needs, requirements, operations, applications, platforms and more! and commercial opportunities of industry. These issues are critical for the commercial infusion and eventual sustainability of technology developed under government funding. Panelists will Monday, 27 July discuss the leverage of advanced in-space propulsion technology, examples of the successful infusion of government-funded 0930–1200 hrs Orlando IV technology development, and opportunities for government in-space propulsion investments that will enable emerging Aircraft Electric Propulsion – Bridging the Gap markets. A panel composed of leaders within government and industry, including spacecraft operators, will discuss the New aircraft electric and hybrid electric propulsion (EP/ leverage of advanced in-space propulsion technology, examples HEP) systems are of increasing excitement in the industry and of the successful infusion of government-funded technology represent an area of worldwide growth. This panel will focus development, and opportunities for government investments in- on the EP/HEP evolutionary path and the challenge to bridge space propulsion to enable emerging markets. between emerging small aircraft concepts and future commercial aircraft all-electric and hybrid gas-electric concepts. Moderator: Mitchell Walker II, Georgia Institute of Technology Moderator: Ruben Del Rosario, NASA Glenn Research Center Panelists: Panelists: Jonny Dyer, Google+Skybox Imaging Frank Anton, Siemens Mark Lewis, IDA Science and Technology Institute Michael Armstrong, Rolls-Royce Corporation Peter Lord, Space Systems Loral Marty Bradley, The Boeing Company Roger Myers, Aerojet Rocketdyne Andrew Gibson, ESAero Jeff Sheehy, Space Technology Mission Directorate, NASA Charles Lents, United Technologies Research Center Johannes Stuhlberger, Airbus

(continued)

www.aiaa-propulsionenergy.org 11 #aiaaPropEnergy ForumIntro 360

Tuesday, 28 July (continued) Wednesday, 29 July

0930–1200 hrs Orlando IV 0930–1200 hrs Orlando IV Evolution of Our National Ground Test Capability Work/Life Balance Challenges for the 21st As budgets continue to tighten, ground test infrastructure is a Century common area to look for savings. This session aims to explore The costs for educating and training a worker in the aerospace how organizations balance operation and maintenance of test profession are extremely high. In today’s environment, a good facilities against budget reality to accomplish their missions. number of households are dual income, and the incoming Key questions that will be explored include: What are the workforce of millennials value family, personal connection, and primary factors and metrics influencing sustainability of ground loyalty. Panelists will explore policies and methods for creating test infrastructure? Is there a general tendency for programs an environment that will enable individuals to balance work and to treat facilities as commodities, and how does this impact life needs to maintain a reliable, diverse, and effective workforce. our ability to retain national assets? How is our maturing computational capability influencing testing? It has long been Moderator: Barbara Esker, NASA the expectation that computational analysis might replace test; are we on the verge of seeing this goal realized or are we reaching Panelists: a codependent steady state between test and computations? Elizabeth Bierman, Honeywell Aerospace Has the industry’s technical risk posture changed as a result Amanda Billot, Pratt & Whitney of flat to shrinking budgets and the present balance between Jim Free, NASA Glenn Research Center computations and test? Klod Kokini, Purdue University Moderator: David Schuster, NASA Langley Research Center Panelists: 1500–1800 hrs Orlando IV Doug Garrard, Arnold Air Force Base Michael Horton, CUBRC Advancing Engineering Through Effective Michael Mastaler, NASA Communication with the Media Michael McWithey, Lockheed Martin Corporation Sooner or later, most engineers will end up talking to a reporter. Roger Simpson, NASA Stennis Space Flight Center Learn how to interact more effectively with and through the media, how to make engineering more relevant to the general public, how public perception through the media affects the 1500–1630 hrs Orlando IV aerospace industry and why interacting with the media matters. Learn how to make the most of this opportunity to help yourself Integrated Roles of Experimental Fluid Dynamics and your profession. Bring your hardest-hitting questions to this and Computational Fluid Dynamics panel of media experts as they discuss their trade. For years, the computational and experimental fluid dynamics Moderator: Vic Beck, Northrop Grumman Corporation communities have had separate advocacies with mixed results. Panelists: Many stakeholders and decision makers may not understand the integrated roles of experimental and computational fluid William Allen, Florida Southern College dynamics (EFD/CFD) in the RDT&E process for new aero Michael Curie, NASA Kennedy Space Center products. Do we need an integrated RDT&E map going forward Marcia Dunn, Associated Press for capability needs in terms of ground testing, computational William Harwood, CBS News methods, and flight testing? Scott Powers, Orlando Sentinel Moderator: James Heidmann, NASA Glenn Research Center Panelists: Keith Blodgett, GE Aviation Michael Mastaler, NASA Richard Scharnhorst, The Boeing Company Roy Schulz, Mira Facilities, 2 Inc. Paul Van Slooten, United Technologies Research Center

www.aiaa-propulsionenergy.org 12 #aiaaPropEnergy ForumIntro 360

The multidimensional program features a leadership exchange/speed mentoring, panel session, Q&A with top industry leaders, and multiple RISING opportunities for networking. These exciting and energetic activities will inLEADERS provide access to top aerospace leaders and their perspectives with subject AEROSPACE matter relevant to your career.

Sponsored by:

Sunday, 26 July Tuesday, 28 July

1800–1900 hrs Mizell A 1600–1730 hrs Orange G Reception Leadership Exchange/Speed Mentoring The reception will kick off the Rising Leaders in Aerospace The Leadership Exchange is an event for students and young events and is a perfect opportunity for young leaders to mingle professionals to meet and interact with established professionals. with others who will be participating in AIAA Propulsion and The Leadership Exchange is organized akin to a Speed Energy 2015 as attendee, presenter, or veteran professional. Networking event. Come meet other participants in a casual environment. You’re The attendees (mentees) will sit down at tables. The established bound to see them again at the Speaker, Networking, or Young professionals (mentors) will then go to a table. After 8–10 Professional Panel event. minutes of interaction, we ask the mentors to move to the next table. This allows for about 8 or 9 interactions during the event. Get your questions answered! Monday, 27 July Mentors include: Joe Anselmo, Editor-in-Chief, Aviation Week Network 1930–2100 hrs Orlando IV Jean Botti, Chief Technical Officer, Airbus How to Avoid a Career Catastrophe: Historic Juliett Davitian, Engineering Specialist, The Aerospace Corporation Aerospace Safety Lessons Lecture Jean-Paul Ebanga, President and CEO, CFM International This session is intended for students and early career aerospace Jeff Hakes, Manager - Fort Worth Aero, Acoustic, Propulsion, engineers. It is intended to be a dialogue, illustrated with recent and Airframe Integration, Advanced Development Programs, space flight safety issues, that explores the role that safety plays Skunk Works in the development and operation of space systems, and also to Bhupendra Khandelwal, Lecturer—Low Carbon Combustion show how proper attention to safety can be beneficial to a career Center, University of Sheffield in aerospace. Mark Lewis, Director, IDA Science and Technology Policy We invite all forum attendees to attend this session. Institute Sandy Magnus, Executive Director, AIAA Guy Norris, Technology Editor, Aviation Week Network Richard “Ric” Parker, Director of Research & Technology, Rolls- Royce plc Rosemary Robles-Culbreth, Propulsion Branch Manager, White Sands Test Facility Abbas Salim, Lockheed Martin Space Systems Company (retired) Graham Warwick, Managing Editor, Technology, Aviation Week Network

www.aiaa-propulsionenergy.org 13 #aiaaPropEnergy IntroSpecial Events

Monday, 27 July

1200-1230 hrs Orlando IV Special Lunchtime Information Session: The Air Force Turbine Prize The Air Force has just announced a $2 million technology prize designed to motivate independent development of a small, lightweight, fuel-efficient engine. The turbine power plant will be highly efficient over a range of power settings, have a high power density, and use a logistically available battlefield fuel (Jet A). The first engine to meet specific performance criteria in a verification test in the Air Force Research Laboratory will receive the prize. Full details are available at www.airforceprize.com. Please join us to learn specifics about the Air Force Turbine Prize, what it is, how to get involved, timelines, ask questions, etc.

Exposition Hall A $2 MILLION COMPETITION TO AIAA Region II ACCELERATE TURBINE ENGINE RESEARCH While you are at AIAA Propulsion and Energy 2015, don’t forget to stop by the AIAA Central Florida Section booth in the Exposition Hall. The booth will display activities going on in the Section. We hope you stop by to check it out.

Wednesday, 29 July

1500–1800 hrs Lake Highland B BENDING THE COST AIAA Undergraduate Engine Design Competition CURVE OF TECHNOLOGY DEVELOPMENT The AIAA Foundation and the Gas Turbine Engine Technical AND SPARKING AMERICAN CREATIVITY Committee have teamed up again to sponsor a design AND INNOVATION competition. Undergraduate students from universities all over the world were asked to prepare a design report to respond to a Request for Proposal (RFP). This RFP asked students to design an ultra-high bypass turbofan engine. All of the responses have been reviewed and ranked by technical Competition Details Presented By: experts, and the authors of the top three proposals have been Lt Col Aaron Tucker invited to AIAA Propulsion and Energy 2015 to make an oral Monday 7/27/2015 ● 12:00pm - 12:30pm presentation to a panel of judges. These judges will assess the Room: Orlando IV design, presentation, and responses to questions. They will add their scores to those provided by the technical judges to come up with a final 1st–3rd place ranking. The final rankings will be announced at the conclusion of the session. D O YOU HAVE WHAT IT TAKES? Learn more at:

www.aiaa-propulsionenergy.org 14 #aiaaPropEnergy IntroNetworking Events

As the old adage says, “It’s not just what you know, it’s who you know.” Connect with those who may become your future colleagues and collaborators, employers or employees. Exchange ideas with the companies you want to partner with, and interact with the leaders who are shaping the future of aerospace. Networking Coffee Breaks Welcome Reception Networking coffee breaks allow even more time for making A welcome reception will be held on Monday, 27 July, new contacts, continuing discussions from sessions, visiting 1800–1930 hrs, in the Exposition Hall. Take this opportunity the Exposition Hall, or checking emails and voicemails to keep to engage new contacts and refresh old ones. A ticket for the in touch with the office. Networking coffee breaks will be at reception is required, and is included in the registration fee the following times and locations: where indicated. Additional tickets may be purchased on site, as space is available. Monday, 27 July 0730–0800 hrs Orange Ballroom Foyer 0900–0930 hrs Exposition Hall 1500–1530 hrs Exposition Hall

Tuesday, 28 July 0730–0800 hrs Orange Ballroom Foyer 0900–0930 hrs Exposition Hall 1430–1500 hrs Exposition Hall Wednesday, 29 July 0730–0800 hrs Orange Ballroom Foyer 0900–0930 hrs Exposition Hall

www.aiaa-propulsionenergy.org 15 #aiaaPropEnergy IntroContinuing Education

AIAA is committed to keeping aerospace professionals at their technical best, and provides an ongoing source of learning, community, professional connections, and career development. Gain the knowledge you need to excel in your field or to move confidently into a new one. Learn how to interact with students and teachers, and help inspire the next generation of aerospace leaders.

Saturday–Sunday, 25–26 July Thursday–Friday, 30–31 July

0800–1700 hrs Clear Lake 0800–1700 hrs Spring Lake Advanced High Speed Air Breathing Propulsion Hybrid Rocket Propulsion This course will introduce students to the design and This course reviews the fundamentals of hybrid rocket development processes of high speed propulsion, including propulsion with special emphasis on application-based design ramjet/scramjets and TBCC concepts. Receive a comprehensive and system integration, propellant selection, flow field and overview of the state of the art, including highlights of current regression rate modeling, solid fuel pyrolysis, scaling effects, high speed propulsion programs in the world. Topics will transient behavior, and combustion instability. Advantages and include: disadvantages of both conventional and unconventional vortex • Mission Requirements hybrid configurations are examined and discussed. Topics will include: • Combined Cycle Propulsion Concepts • Introduction, Classification, Challenges, and Advantages of • Ramjet/Scramjet Inlet Design Hybrids • Ram/Scramjet Combustion Structural Design • Similarity and Scaling Effects in Hybrid Rocket Motors • Fuels and Thermal Management Engine/Airframe • Flowfield Modeling of Classical and Nonclassical Hybrid Integration, TBCC Integration Rockets • Advanced Materials • Solid Fuel Pyrolysis Phenomena and Regression Rate: • CFD Modeling and Simulation of High Speed Reacting Flow Mechanisms & Measurement Techniques • Propulsion Multidisciplinary Design Optimization (MDO) • Combustion Instability and Transient Behavior in Hybrid Rocket Motors • High Speed Propulsion Ground Testing • Metals, Other Energetic Additives, and Special Binders Used • High Speed Flight Testing in Solid Fuels for Hybrid Rocket Applications

New Editor-in-Chief Sought for Journal of Propulsion and Power (JPP)

AIAA is seeking an outstanding candidate with an international The full position description and Editor-in-Chief search reputation to assume the responsibilities of Editor-in-Chief of announcement can be found on the JPP landing page in the Journal of Propulsion and Power. JPP is devoted to the Aerospace Research Central: http://arc.aiaa.org/loi/jpp advancement of the science and technology of aerospace propulsion and power through the dissemination of original To receive full consideration, applications and all required archival papers contributing to advancements in airbreathing, materials must submitted by 1 Oct. 2015, but applications electric, and advanced propulsion; solid and liquid rockets; will be accepted until the position is filled. fuels and propellants; power generation and conversion for aerospace vehicles; and the application of aerospace science and technology to terrestrial energy devices and systems. The chosen candidate will assume the editorship at an exciting time as new features and functionality intended to enhance journal content are added to Aerospace Research Central, AIAA’s platform for electronic publications.

www.aiaa-propulsionenergy.org 16 #aiaaPropEnergy Recognition Events

AIAA celebrates our industry’s discoveries and achievements from the small but brilliantly simple innovations that affect everyday lives to the major discoveries and missions that fuel our collective human drive to explore and accomplish amazing things. Join AIAA in celebrating achievements in propulsion and energy at the AIAA Recognition Luncheon on Wednesday, 29 July, 1200–1330 hrs, in the Florida Ballroom. A ticket for the luncheon is required, and is included in the registration fee where indicated. Additional tickets may be purchased on site, as space is available.

The following awards will be presented: Aerospace Power Systems Award Propellants and Combustion Award Theodore G. Stern Mitchell Smooke Director, Solar Power Solutions Strathcona Professor of Mechanical Engineering Alliance Spacesystems, LLC & Materials Science & Applied Physics El Cajon, California Yale University New Haven, Connecticut “For over 30 years of developing advanced photovoltaic power systems for spacecraft; for providing exceptional leadership and “For fundamental and substantive contributions to combustion innovation in the aerospace power system community; and and propellant science and the advancement of numerical for significant contributions to AIAA and AIAA professional combustion.” education.” Wyld Propulsion Award Air Breathing Propulsion Award R. Carl Stechman Jan C. Schilling Consultant Advanced Products Chief Engineer (retired) Formally Chief Engineer and Technical Principal GE Aviation Aerojet (Redmond, WA)/The Marquardt Company (Van Nuys, Cincinnati, Ohio CA) “For innovation in gas turbine engine design and safety, “For over 50 years of development and integration of storable especially in composite fan blading, low NOx combustion, and rocket engines into space systems from Apollo, to the Space high pressure ratio compressor airfoils.” Shuttle, to Orion.”

Engineer of the Year Award Certificates of Merit: William J. Emrich Aerospace Power Systems Best Paper Senior Engineer AIAA 2014-3640, “High Power Density Modular Electric NASA Marshall Space Flight Center Huntsville, Alabama Power System for Aerospace Applications,” Scott Steffan and Gregory Semrau, Moog Inc. “For conceiving of, designing, and bringing to operational status the megawatt-class Nuclear Thermal Rocket Element Aerospace Power Systems Best Student Paper Environment Simulator.” AIAA 2014-3459, “Non-Cooled Power System for Venus Lander,” Denise Salazar, The University of Texas at Austin; Geoffrey Landis, NASA Glenn Research Center; and Anthony Energy Systems Award Colozza, Vantage Partners, LLC. Tom I-Ping Shih Professor, School of Aeronautics and Astronautics Purdue University West Lafayette, Indiana “For outstanding contributions to computational tool development and improvement for use in design, analysis and examination of complex engineering problems involving aerodynamics, propulsion, and energy.”

(continued) www.aiaa-propulsionenergy.org 17 #aiaaPropEnergy IntroRecognition Events

Certificates of Merit (continued) Hybrid Rockets Best Paper Air Breathing Propulsion Systems Integration Best Papers AIAA 2014-3646, “Evaluation of Para-n-based Fuels for Hybrid Rocket Engines,” Mario Kobald, C. Schmierer, Helmet AIAA-2014-0722, “Numerical and Experimental Investigations Ciezki, and Stefan Schlechtriem, German Aerospace Center on Highly Integrated Subsonic Air Intakes,” Thomas Berens, (DLR); and Elena Toson and Luigi De Luca, Politecnico di Luis Ruiz-Calavera, and David Funes-Sebastian, AIRBUS Milano. Defence and Space; Anne-Laure Delot, ONERA; Magnus Tormalm, Swedish Defense Research Agency (FOI); Martin Rein, German Aerospace Center (DLR); Michael Säterskog, Hybrid Rockets Best Student Paper Saab; Nicola Ceresola, Alenia Aermacchi, and Ludovic Zurawski, MBDA. AIAA 2014-3868, “Effects of Injector Design on Combustion Stability in Hybrid Rockets Using Self-Pressurizing Oxidizers,” Benjamin S. Waxman, Jonah E. Zimmerman, Brian J. Cantwell, AIAA-2014-3684, “Propulsion System Dynamic Stanford University; and Gregory G. Zilliac, NASA Ames Modeling of the NASA Supersonic Concept Vehicle for Research Center. AeroPropulsoServoElasticity,” George Kopasakis, Joseph W. Connolly, and Jonathan A. Seidel, NASA Glenn Research Center. Liquid Propulsion Best Paper AIAA 2014-3681 “Combustion Stability Characteristics of Electric Propulsion Best Paper the Project Morpheus Liquid Oxygen / Liquid Methane Main Engine,” John C. Melcher and Robert L. Morehead, NASA AIAA 2014-3710, “The Effect of Background Pressure on Johnson Space Center. SPT-100 Hall Thruster Performance,” Kevin D. Diamant, The Aerospace Corporation; and Raymond Liang and Ron L. Corey, Space Systems/Loral, LLC. Nuclear and Future Flight Propulsion Best Paper AIAA 2014-3520, “Developing the Pulsed Fission-Fusion (PuFF) Engine,” Robert Adams, NASA Marshall Space Flight High Speed Air Breathing Propulsion Best Paper Center; Jason Cassibry, University of Alabama-Huntsville; AIAA Paper 2014-3743, “A Priori Analysis of Flamelet-Based David Bradley, Yetispace, Inc.; Leo Fabisinski, International Modeling for a Dual-Mode Scramjet Combustor,” Jesse R. Space Systems Inc.; and Geoffrey Statham, ERC Inc. Quinlan and James McDaniel, University of Virginia; Tomasz Drozda, NASA Langley Research Center; and Guilhem Lacaze and Joseph Oefelein, Sandia National Laboratories. Propellants and Combustion Best Paper AIAA 2014-0647, “Microspheres Composite of Nano-Al and Nanothermite: An Approach to Better Utilization of Nanomaterials,” Haiyang Wang, Guoqiang Jian, Jeffery Delisio, and Michael Zachariah, University of Maryland.

www.aiaa-propulsionenergy.org 18 #aiaaPropEnergy IntroExposition Hall

Charging Station dSPACE Poco Lounge 216 315 Marotta SEDS PCB Mu Controls Aero Piezotronics 214 313 316 415 416 515 516

Metal Industries 314 413 414 513 514

Turbo AIAA Central Machined Florida Products, LLC Section 409 VACCO 509 5 609 T 208 308 407 408 507 508 607 AIAA Pavilion

P

Aviation 202 302 402 502

Exhibitors by Booth Number (êindicates AIAA Corporate Members) ê 302 Aerojet Rocketdyne ê ENTRANCE413 National Technical Systems (NTS) 610 AIAA Central Florida Section 614 North Star Imaging Inc. ê 214 BETA CAE Systems 502 Orbital ATK 415 Cambridge University Press 516 PCB Piezotronics 308 Cobham 315 Poco Graphite 416 Desktop Aeronautics 507 Pointwise, Inc. ê 216 dSPACE, Inc. ê 604 Price Induction Inc. 510 EKK Eagle Industry, Co. Ltd 409 Rolls-Royce Corporation ê 402 GE Aviation ê 313 Stanford Mu Corporation 407 General Dynamics - OTS 515 Students for the Exploration and Development of Space (SEDS)—UC San Diego 509 Intelligent Light ê 508 Tecplot, Inc. 514 JASC-CONTROLS 609 Turbo Machined Products LLC 607 Keystone Engineering Company 602 University of Cincinnati Research Institute (UCRI) 316 Marotta Controls, Inc. 408 VACCO Industries 314 Metal Technology 414 Valcor Engineering Corporation 202 Moog, Inc. 513 Worthington Industries (SCI) 608 MT Aerospace AG 208 NASA www.aiaa-propulsionenergy.org 19 #aiaaPropEnergy IntroExposition Hall

The Exposition Hall is the hub of activity during this event. Networking coffee breaks, luncheons, receptions, poster sessions, poster presentation sessions, and exhibitor presentations are all held in the Exposition Hall to give attendees and exhibitors an opportunity to connect with partners, industry thought leaders, and collaborators who can help move your business forward. Exposition Hall Hours AIAA Pavilion Monday, 27 July 0900–1200 hrs Stop by the AIAA Pavilion, located in the Exposition Hall, 1330–1600 hrs to browse publications and merchandise, learn about your Reception* 1800–1930 hrs membership benefits, and meet AIAA staff. Tuesday, 28 July 0900–1200 hrs Networking Luncheon* 1200–1300 hrs 1300–1600 hrs 30% Off All Books at Propulsion and Energy 2015 Wednesday, 29 July 0900–1200 hrs AIAA Publications is offering a special discount on all titles featured at AIAA Propulsion and Energy 2015. Attendees can *A ticket is required to attend the reception and the networking take advantage of a 30% discount off the list price of all books luncheon for sale at the AIAA Bookstore located in the AIAA Pavilion. This special offer will only be available during the forum! Take advantage of these super savings and visit the AIAA Bookstore! New this year! Charging Stations Stay connected at Propulsion and Energy: charge your laptop, Special Events tablet or phone at our complimentary charging stations. Conveniently located in the Exposition Hall at the end of Monday, 27 July 1500–1530 hrs the 600 aisle. Popcorn Break Tuesday, 28 July 1430–1500 hrs Ice Cream Break

www.aiaa-propulsionenergy.org 20 #aiaaPropEnergy Exhibitors Aerojet Rocketdyne 302 Cobham 308 2001 Aerojet Road 10 Cobham Drive Rancho Cordova, CA 95742 Orchard Park, NY 14127 www.aerojet.com www.cobham.com [email protected] [email protected] Aerojet Rocketdyne, is a world-recognized aerospace and Cobham builds on extensive space flight heritage with defense leader providing propulsion and energetics to innovative propulsion solutions that support chemical, electric the space, missile defense, strategic, tactical missile, and and cold gas systems. Leveraging decades of component armaments areas in support of domestic and international design, Cobham has developed a variety of integrated pressure markets. Additional information about Aerojet Rocketdyne is control assemblies for propulsion applications for the launch available online at www.Rocket.com. vehicle and satellite market. Cobham has expanded beyond our standard propulsion offerings for the dynamic small sat market with integrated propulsion modules optimized for AIAA Central Florida Section 610 individual customer requirements. 1082 West Riviera Blvd Oviedo, FL 32765 info.aiaa.org/Regions/SE/CF/default.aspx Desktop Aeronautics 416 The Central Florida Section of the American Institute of 1900 Embarcadero Way Aeronautics and Astronautics is dedicated to furthering Palo Alto, CA 94303 the interested, activities, and technical programs of local www.desktop.aero professional, students and educators within the Central Florida [email protected] aerospace community. Founded in 1994, Desktop Aeronautics has grown into a well-established consulting firm dedicated to advancing the state of the art in aerodynamics and aircraft design. We BETA CAE Systems 214 have significant experience and recognized expertise in 29800 Middlebelt Road, Suite 100 aerodynamics, aircraft design, computational fluid dynamics, Farmington Hills, MI 48334 and multidisciplinary optimization. We have worked with www.ansa-usa.com leading aerospace organizations on some of the most difficult [email protected] challenges in aerospace industry. BETA CAE Systems is an engineering services company that distributes and supports the industry leading ANSA and dSPACE 216 META software. ANSA is a CAE pre-processing tool for FE and CFD analysis, for full-model build, from CAD to solver 50131 Pontiac Trail input file, in one integrated environment. META is a post- Wixom, MI 48393 processor for analyzing results from ANSYS, NASTRAN, www.dspaceinc.com ABAQUS, LS-DYNA, PAMCRASH, RADIOSS, MADYMO, [email protected] and other solvers. dSPACE is the world’s leading provider of hardware and software tools for developing and testing sophisticated electronic control systems. dSPACE systems support numerous Cambridge University Press 415 aerospace, defense, UAV and space flight technology 32 Avenue of the Americas applications in areas such as: engine development, navigation New York, NY 10013-2473 systems, propulsion, real-time flight maneuver simulation, and www.cambridge.org/us testing of on-board systems. www.dspaceinc.com [email protected] Cambridge’s publishing in books and journals combines state- EKK Eagle Industry, Co. LTD. 510 of-the-art content with the highest standards of scholarship, writing and production. Visit our stand to browse new titles, 1731 Technology Dr., Ste. 760 available at a 20% discount, and to pick up sample issues of San Jose, CA 95132 www.ekk.co.jp our journals. Visit our website to see everything we do: www. [email protected] cambridge.org/engineering EKK Eagle is a comprehensive mechanical seals MFG. For the aerospace and optical engineering industries, we research, develop and produce mechanical seals for use principally in aircraft and space rocket jet engines, and various sensors and sensor modules used in optical equipment.

www.aiaa-propulsionenergy.org 21 #aiaaPropEnergy Exhibitors GE Aviation 402 Keystone Engineering Company 607 One Neumann Way, MD G414 4401 Donald Douglas Drive Cincinnati, OH 45215 Long Beach, CA 90808 www.ge.com/aviation www.keyengco.com [email protected] [email protected] GE Aviation, an operating unit of GE (NYSE: GE), is a world- Keystone is a world leader in the design and fabrication of leading provider of jet, turboprop, and turboshaft engines, engineered products used in critical flightweight aerospace and components, and integrated systems for commercial, military, defense applications. Keystone core competencies include the business, and general aviation aircraft. GE Aviation has a design, analysis, and production of lightweight propellant and global service network to support these offerings. For more pressure storage tanks, spun domes for satellites and launch information, visit us at www.ge.com/aviation. Follow GE vehicles, large diameter aircraft bearing systems (see “AWACS” Aviation on Twitter at http://twitter.com/GEAviation and section for details) and other specialized engineered products YouTube at http://www.youtube.com/user/GEAviation. for various defense and aerospace applications.

General Dynamics —OTS 407 Marotta Controls, Inc 316 4300 Industrial Avenue 78 Boonton Avenue Lincoln, NE 68504 Montville, NJ 07045 www.gd-ots.com www.marotta.com [email protected] [email protected] General Dynamics Ordnance and Tactical Systems provides Marotta Controls, Inc. has 50+ years of experience in designing reliable and affordable composite products to the defense and control systems for spacecraft. Our engineered propulsion commercial aerospace markets. With more than 50 years of controls are compact, lightweight, use minimal power and are expertise, General Dynamics designs, develops, manufactures ready for integration into your system. Let our experienced and tests a full range of composite missile and space structures, engineering team work with you to overcome your control including rocket motors, pressure vessels, launch tubes and system challenges. Visit us at booth 316. fuel tanks. Metal Technology 314 Intelligent Light 509 173 Queen Avenue SE 301 Rt. 17 North, 7th Floor Albandy, OR 97322 Ruthorford, NJ 07070 www.mtialbany.com www.ilight.com [email protected] [email protected] With more than forty years of experience, Metal Technology Intelligent Light provides post-processing, data management (MTI) leads the way in additive manufacturing, precision and big data visualization capability for CFD. Thousands of machining, forming and forging of exotic metals. MTI users rely on the industry leading FieldView software and our works with materials such as Tantalum, Niobium, Titanium, custom engineering services to maximize their productivity Molybdenum, Tungsten and their alloys. MTI is ISO9001 and effectiveness. Let us help you eliminate bottlenecks and registered and ITAR compliant. achieve breakthrough results. Moog 202 JASC-Controls 514 500 Jamison Rd. 2303 W. Alameda Drive East Aurora, NY 14052 Tempe, AZ 85282 www.moog.com/space www.jasc-controls.com [email protected] [email protected] Moog designs and manufactures payload, spacecraft, and The JASC Corporation specializes in the design and launch vehicle components and systems including: spacecraft production of high-reliability components for pneumatic, attitude control and mechanisms, propulsion systems and fluid hydraulic, and fuel systems. Since its inception in 1990, JASC control components, software and avionics, ground systems, has been providing fluid control solutions and advanced thrust vector and steering controls, electric and hydraulic products for the aircraft, spacecraft, and power generation actuation, spacecraft vibration and shock isolation systems, industries. payload adapters, ground test equipment and shock testing services.

www.aiaa-propulsionenergy.org 22 #aiaaPropEnergy ExhibitorsIntro

MT Aerospace AG 608 Orbital ATK 502 Franz Josef Straub-Str. 5 PO Box 707 86153 Augsburg Germany Brigham City, UT 84302 www.mt-aerospace.de www.atk.com [email protected] [email protected] MT Aerospace is an internationally well-respected aerospace ATK is on the forefront of R&D and manufacture of solid company. With over 700 employees and almost 50 years of rocket propulsion, aircraft structures, missile components, project experience we are the technology leader in light weight small sats, solar arrays, satellite components, and flares and construction using metal and composite materials for ARIANE decoys. ATK provides affordable solutions to meet emerging 5, for satellites, spacecrafts, the Airbus fleet as well as radio needs. telescope constructions. PCB Piezotronics 516 NASA 208 3425 Walden Ave Depew 300 E Street Southwest NY 14043 Washington, DC 20546 www.pcb.com www.nasa.gov [email protected] PCB Piezotronics is a global leader in the design and manufacture of microphones, vibration, force, torque, load, Since its inception in 1958, the National Aeronautics and Space strain, and pressure sensors, as well as the pioneer of ICP® Administration (NASA) has sought to reach for new heights technology. PCB® proudly stands behind their products and reveal the unknown so that what we do and learn will with the industry’s only commitment to Total Customer benefit all humankind. NASA’s priorities are: Earth Right Now Satisfaction. Visit us at www.pcb.com – Your Planet is Changing. We’re on It; Aeronautics– We’re with You When You Fly; International Space Station – Off the Earth, For the Earth; Journey to Mars; Solar System and Poco Graphite 315 Beyond; and Technology Powering Exploration. For more 300 Old Greenwood Road information, visit us at: www.nasa.gov. Decatur, TX 76234 www.poco.com NTS – National Technical Systems 413 [email protected] Poco Graphite is a leading manufacturer of Graphite, SiC, 24007 Ventura Boulevard Carbon Foam, and Coating Materials for use in Propulsion Calabasas, CA 91302 www.nts.com and Turbine applications. POCO materials are used in extreme [email protected] environments, including systems that require precision & high performance. Typical applications are bushings, thrust NTS provides a wide range of test, inspection and certification washers, rings, seals, and thermal management systems. solutions. Our clients see us as an extension of their own teams, providing the expertise required to build better, stronger, safer, more reliable products. With the largest Pointwise 507 network of test laboratories and engineering service centers in 213 South Jennings Avenue North America and over 50 years of experience to draw from, Fort Worth, TX 76104 NTS is prepared to meet any challenge. www.pointwise.com [email protected] North Star Imaging 614 Pointwise, Inc. is solving the top problem facing engineering analysts today: mesh generation for computational fluid 19875 South Diamond Lake Road dynamics. Manufacturing firms and research organizations use Rogers, MN 55374 www.xrayinspectionservice.com Pointwise’s mesh generation software to seamlessly bridge the [email protected] gap between CAD and computational fluid dynamics analysis. NSI is a leading manufacturer of Industrial 2D Digital X-ray and 3D X-ray CT systems. Industrial X-ray scanning allows users to inspect both the internal and external structures of an object without opening it up or otherwise destroying the item. NSI’s Inspection Services Group offers need based consulting services for anyone needing X-ray/CT scanning.

www.aiaa-propulsionenergy.org 23 #aiaaPropEnergy IntroExhibitors

Price Induction, Inc. 604 216 14th Street NW, Suite 8 Atlanta, GA 30318 www.price-induction.com [email protected] Price Induction is a turbine engine manufacturer, designer of the world’s smallest turbofan. Price Induction is also involved in innovation programs for major aerospace groups Engine Manufacturer Experience. Its design office is fully conversant in all the aspects that make up the development cycle of an aeronautical turbine engine, as well as those of similar complex mechanical systems.

Rolls-Royce Corporation 409 450 S. Meridian Street, MC-N1-02 Indianapolis, IN 46225 www.Rolls-Royce.com At Rolls-Royce LibertyWorks, we develop solutions for everything from advanced VTOL technology to high-speed flight. We provide technology the US warfighter needs to perform the mission. We value our relationshipsTM with airframers, Army Advanced Technology Division, DARPA, NASA, AFRL, Naval Research Laboratory and advanced technology consortiums.

Stanford Mu Corporation 313 20725 Annalee Avenue Carson, CA 90746-3503 www.stanfordmu.com [email protected] An internationally recognized leader in the design, development and production of propulsion systems and other fluid control components for satellites, spacecrafts and space vehicles. Space Components is ISO9001:2008 and AS9100:0029 Reve. C Certified and has delivered over 800 regulators of which 312 have successfully flown; the balance are awaiting launch.

Students for the Exploration and Development of SpaceThe Contents (SEDS) of this Package UC are Stanford San Mu DiegoCorporation Confidential. 515 9500 Gilman Dr. La Jolla, CA 92092 seds.ucsd.edu [email protected] Students for the Exploration and Development of Space (SEDS) at the UC San Diego is a team of undergraduate students with the vision of advancing space technologies by researching 3D-printed metal rocket engines. Following their success in 2013 with the Tri-D engine, SEDS UCSD intends to be one of the first people to successfully recover a rocket powered by their latest 3D-printed engine, Vulcan-I, in early August.

www.aiaa-propulsionenergy.org 24 #aiaaPropEnergy ExhibitorsIntro

Tecplot, Inc. 508 VACCO Industries 408 3535 Factoria Blvd SE, Ste 550 10350 Vacco Street Bellevue, WA 98006 South El Monte, CA 91733 www.tecplot.com www.vacco.com [email protected] [email protected] Tecplot software empowers engineers and scientists working VACCO is a leading designer and manufacturer of specialty with computational fluid dynamics (CFD) to discover, analyze, valves, filters and advanced fluid control products—offering and understand information in complex data, and to effectively innovative engineered solutions to critical missions for defense, communicate their results to others via brilliant images and space, and commercial markets for 60 years. Reliable heritage. compelling animations. Tecplot products are used by more Intelligent solutions. than 45,000 technical professionals around the world. Valcor Engineering Corporation 414 Turbo Machined Products LLC 609 2 Lawrence Road ® 102 Industrial Drive Springfield, NJ 07081 VALCOR Frankfort, NY 13340 www.valcor.com www.turbomp.com [email protected] Turbo Machined Products in Frankfort, NY, has specialized in Valcor Aerospace specializes in the design and manufacture 5-axis machining since 1994. Our customer base includes UTC of custom valves and control components (solenoid, relief, P&W, GE Aviation, Blue Origin & SPACEX. We manufacture check, fill and drain valves, pressure regulators, actuators) for components for defense, aerospace and power generation liquids (propellants, fuel, hydraulic fluid) and gases in critical industries. Please contact us for new engine development & aerospace (aircraft, launch vehicle, missile, spacecraft, etc.) production machining of components such as Rocket engine applications. fuel inducers, LOX impellers, Oxidizer impellers, gas swirlers, fans, BLISKS, OGV’s, compressor blades and contour milling of airfoil components. Worthington Industries 513 336 Enterprise Place Pomona, CA 91768 Univ. of Cincinnati Research Institute (UCRI) 602 www.worthingtoncylinders.com 260 Stetson Street Suite 5300 [email protected] Cincinnati, OH 45219 UNIVERSITY of CINCINNATI Manufacturer of Composite Overwrapped Pressure Vessels and www.ucri.org/ [email protected] RESEARCH INSTITUTE Structures. In our rapid-fire, knowledge-driven economy, smarts rule. That’s why UCRI helps businesses tap into the world–class expertise and resources found in virtually every hallway on the UC campus. We’re a separate organization from UC, but closely affiliated and well connected. We’re business people who offer a “one stop shop” for accessing UC smarts in all its many varieties, including some that may surprise you. Let us show you just how easy we make it.

www.aiaa-propulsionenergy.org 25 #aiaaPropEnergy IntroGeneral Information

AIAA Registration and Information Center Hours Conference Proceedings The AIAA Registration and Information Center will be located Proceedings for the forum will be available online. The cost on the ballroom level of the Convention Center. is included in the registration fee where indicated. Online proceedings will be available on 27 July 2015. Attendees who Sunday, 26 July 1500–1900 hrs register in advance for the online proceedings will be provided Monday, 27 July 0700–1800 hrs with instructions on how to access them. Those registering on site will be provided with instructions at that time. Tuesday, 28 July 0700–1700 hrs Proceedings: Wednesday, 29 July 0700–1700 hrs 1. To view proceedings, visit www.aiaa.org >ARC>Meeting Papers. Wi-Fi Internet Access On Site a. Log in with the link at the top right of the page. Wi-Fi service for attendees is available in the foyer space of b. Select the appropriate conference from the list. the hotel outside session rooms and the Exposition Hall (see page 5). To keep this service available and optimized for all c. Search for individual papers with the Quick Search toolbar attendees, please do not download files larger than 2MB, in the upper-right corner of the page: create multiple sessions across multiple devices, or download i. By paper number: Click the Paper Number link, select multiple files in one session. If you receive an error message the conference year, and enter the paper number. that an AIAA server is blocking your current IP address, please ii. Use the Search textbox to find papers by author, title, or inform the AIAA Registration and Information Center. keyword. The Advanced Search link provides additional search information and options. 2. All manuscript files submitted by four days prior to the conference are currently in the proceedings. Files submitted after that date, both original and revised manuscripts, will not be available until the final proceedings update, which may take up to 15 business days after the last day of the conference. 3. Direct any questions concerning access to proceedings and/ or ARC to [email protected].

Manuscript Revisions 1. Manuscript revision is open for all presenting authors from 0900 hrs Eastern Time, 28 July, through 2000 hrs Eastern Time, 7 August 2015. 2. Revisions submitted for manuscripts already online will not refresh until after the proceedings have been updated, which may take up to 15 business days after the last day of the conference.

www.aiaa-propulsionenergy.org 26 #aiaaPropEnergy IntroGeneral Information

Certificate of Attendance Young Professional Guide for Gaining Certificates of Attendance are available for attendees who Management Support request documentation at the forum itself. The Certificates Young professionals have the unique opportunity to meet and of Attendance will be available for attendees to print at a learn from some of the most important people in the business self-service station at the registration desk starting Monday by attending conferences and participating in AIAA activities. afternoon, 27 July 2015. AIAA offers this service to better serve A detailed online guide, published by the AIAA Young the needs of the professional community. Claims of hours or Professional Committee, is available to help you gain support applicability toward professional education requirements are and financial backing from your company. The guide explains the responsibility of the participant. the benefits of participation, offers recommendations and provides an example letter for seeking management support and funding, and shows you how to get the most out of your Employment Opportunities participation. The online guide can be found on the AIAA website at www.aiaa.org/YPGuide. AIAA assists members who are searching for employment by providing a bulletin board at forums. This bulletin board is solely for “open position” and “available for employment” postings. Employers are encouraged to have personnel who Nondiscriminatory Practices are attending an AIAA forum bring “open position” job AIAA accepts registrations irrespective of race, creed, gender, postings. Individual AIAA members may post “available for color, sexual orientation, physical handicap, and national or employment” notices. AIAA cannot assume responsibility for ethnic origin. notices forwarded to AIAA Headquarters. AIAA reserves the right to remove inappropriate notices. AIAA members can post and browse resumes, browse job listings, and access other online employment resources by visiting the AIAA Career Restrictions Center at http://careercenter.aiaa.org. Photography or the video or audio recording of sessions or exhibits, as well as the unauthorized sale of AIAA-copyrighted material, is prohibited. Membership AIAA is your vital lifelong link to the collective creativity International Traffic in Arms Regulations (ITAR) and brainpower of the aerospace profession and a champion for its achievements – and nonmembers who pay the full AIAA speakers and attendees are reminded that some topics nonmember registration fee will receive their first year’s AIAA discussed at the forum could be controlled by the International membership at no additional cost! Students who are not yet Traffic in Arms Regulations (ITAR). U.S. nationals (U.S. members may apply their registration fee toward their first citizens and permanent residents) are responsible for ensuring year’s student member dues. (Free membership is not included that technical data they present in open sessions to non-U.S. in discounted group-rate registration.) nationals in attendance or in conference proceedings are not export restricted by the ITAR. U.S. nationals are likewise responsible for ensuring that they do not discuss ITAR export- restricted information with non-U.S. nationals in attendance.

AIAA Foundation Since 1996 the AIAA Foundation has provided programs and support for educators and students. Through classroom grants, scholarships, awards, design competitions, and student conferences, the AIAA Foundation has encouraged students in grades K–12 and at the university level to discover the aerospace industry and become the next generation of scientists and engineers. Please consider making a donation so that the Foundation can continue to provide the resources needed to support aerospace education and to recognize innovation at all levels. For more information and to donate online, please visit www.aiaafoundation.org.

www.aiaa-propulsionenergy.org 27 #aiaaPropEnergy GeneralIntro Information

Author and Session Chair Information

Speakers’ Briefings in Session Rooms Audiovisual Authors who are presenting papers will meet with session Each session room will be preset with the following: one chairs and co-chairs in their session rooms for a short LCD projector, one screen, one microphone and sound 30-minute briefing on the day of their sessions to exchange system (if necessitated by room size), and one laser pointer. bios and review final details prior to the session. Please attend Laptop computers will also be provided. You may also use on the day of your session(s). Laptops preloaded with the your own computer. Any additional audiovisual equipment Speaker Briefing preparation slides will be provided in each requested onsite will be at cost to the presenter. Please note session room. Speakers’ Briefing schedule is as follows: that AIAA does not provide security in the session rooms and Monday, 27 July 0730–0800 hrs recommends that items of value not be left unattended. Tuesday, 28 July 0730–0800 hrs “No Paper, No Podium” and “No Podium, No Wednesday, 29 July 0730–0800 hrs Paper” Policy Speakers’ Practice Room If a written paper is not submitted by the final manuscript deadline, authors will not be permitted to present the paper at Speakers who wish to practice their presentations may do so the forum. Also, if the paper is not presented at the forum, it in Spring Lake. A sign-up sheet will be posted on the door. In will be withdrawn from the proceedings. It is the responsibility consideration of others, please limit practice time to 30-minute of those authors whose papers or presentations are accepted to increments. ensure that a representative attends the conference to present the paper. These policies are intended to improve the quality Session Chair Reports of the program for attendees. All session chairs are asked to complete a session chair report to evaluate their session for future planning. AIAA Journal Publication has partnered with Canvas Solutions to provide an electronic AIAA has prior publication rights to any paper presented at Session Chair Report form. You can download the FREE its conferences. Authors who are seeking the opportunity for mobile app in your App Store, AppWorld, or Marketplace peer-reviewed publication are encouraged to submit their by searching for “Canvas Solutions, Inc.” The mobile app is papers for consideration by one of the Institute’s archival free, so please be sure to download it. Detailed instructions journals: AIAA Journal; Journal of Aircraft; Journal of will be provided in the session rooms. If you do not have Guidance, Control, and Dynamics; Journal of Propulsion a tablet or a smartphone, simply use the report form as a and Power; Journal of Spacecraft and Rockets; Journal of guide and enter your session chair report information at the Thermophysics and Heat Transfer; or Journal of Aerospace session chair reporting computer station located on site near Information Systems. Journal scopes and author guidelines the AIAA registration area. Report data will be collected and and instructions can be found in Aerospace Research Central used for future planning purposes, including session topics at http://arc.aiaa.org/page/authorresources. You may now and room allocations. Please submit your session chair report submit your paper to a journal for review before electronically by 30 July 2015. the conference presentation date: http://mc.manuscriptcentral.com/aiaa.

AIAA is the world’s largest aerospace professional society, serving a diverse range of more than 30,000 individual members from 88 countries, and 95 corporate members. AIAA members help make the world safer, more connected, more accessible, and more prosperous. For more information, visit www.aiaa.org, or follow us on Twitter @AIAA. American Institute of Aeronautics and Astronautics 1801 Alexander Bell Drive, Suite 500 Reston, VA 20191-4344 703.264.7500 or 800.639.AIAA (2422) Fax: 703.264.7657 [email protected] www.aiaa.org www.aiaa-propulsionenergy.org 28 #aiaaPropEnergy IntroITAR Information ITAR-Restricted Sessions Availability of Manuscripts from ITAR-Restricted Sessions On Tuesday, a limited number of papers will be presented A DVD containing the manuscripts from the ITAR sessions in “U.S.-Only” technical sessions. In addition to your forum will be available for purchase on site at the forum, by those registration, a separate registration process is required to who are registered to attend the ITAR sessions, for $25. There attend these restricted sessions. Please see the detailed will be no sale or distribution of these papers after the event. information on the ITAR Registration Grid to determine your individual requirements. ITAR Electronics Policy Access to ITAR Sessions: Presenting a Paper, Chairing a Session, or Attending an ITAR-Restricted Presentation No phones, computers (other than the presenter), iPads, cameras, and other electronic devices with cameras or Admittance to the restricted technical papers is controlled by recording capabilities will be permitted into the ITAR the U.S. International Traffic in Arms Regulations (ITAR). All session room. There will be a check-in desk in front of the attendees, presenters, and session chairs will need to register room where you can check these devices during the time for the conference and then visit the ITAR Registration Desk to you are in the sessions. complete additional registration procedures. Anyone wishing to enter the restricted session room MUST abide by the procedures and submittal of verification documents mandated by the DoD. No Exceptions! Important session information for all attendees wishing to present or attend ITAR papers

AIAA Restricted Papers – ITAR Regulations Session Admittance Policy (Revised 10/19/2012) Several papers scheduled to be presented at this conference will DD Form 2345 individual certication credentials (required for be restricted papers governed by ITAR (U.S. International Tra c U.S. & Resident Aliens) MUST be from one of the following: in Arms Regulations). If you plan to attend any presentations 1. Copy of an approved and active DD2345 for the restricted by ITAR, you must bring proof of citizenship PLUS individual, OR the other verication documents as shown below. Please note that only U.S. Citizens and U.S. Resident Aliens can be 2. Copy of an approved and active DD2345 for the considered for attendance at these restricted presentations. individual’s employer PLUS evidence of current Admittance to restricted sessions and access to restricted employment status with that employer (corporate ID, technical papers is implemented and controlled by ITAR . business card, etc.), OR All restricted session attendees (including speakers and session 3. A listing of the individual’s employer in the most recent chairs for these sessions) MUST abide by the procedures and DoD quarterly Qualied U.S. Contractor Access List PLUS submittal of verication documents as noted below – NO evidence of current employment status with that employer EXCEPTIONS: (corporate ID, business card, etc.). DD Form 2345 may be downloaded and completed online in ATTENDEE CLASSIFICATION IDENTIFICATION & PROOF OF EMPLOYMENT order to apply for approval to be listed on the Qualied U.S. REQUIREMENTS Contractor List, www.dlis.dla.mil/jcp. Allow at least 4–6 weeks (or longer) prior to the AIAA technical conference dates for U.S. Government Employees 1. Proof of U.S. Citizenship (for example, passport, you to receive the approval and be listed on the Qualied U.S. birth certificate, voters registration card, Contractor List. NOTE: CAC Cards naturalization papers), AND are NOT proof of 2. Personal photographic identification: U.S. How to get your ITAR Clearance: citizenship. Government/Military Photo ID badge, such as CAC card Bring all of the above listed identication, proof of employment and certication credentials to the AIAA ITAR U.S. Citizens 1. Proof of U.S. Citizenship (for example, passport, Registration Desk in the AIAA Registration area. birth certificate, voters registration card, naturalization papers), AND Your documents will be veried and you will be provided with 2. Personal photographic identification (passport, a stamp indicating your ITAR clearance. Photo ID will be driver’s license, etc.), AND checked against your ITAR badge before admittance is granted 3. Certification credentials based on DD Form 2345 to any ITAR presentation. (see below for details) Please be advised that all policies and procedures MUST be followed or admittance to restricted sessions will not be Resident Aliens (U.S.) 1. Resident Alien Card, AND permitted. 2. Personal photographic identification (passport, driver’s license, etc.), AND 3. Certification credentials based on DD Form 2345 (see below for details) www.aiaa-propulsionenergy.org 29 #aiaaPropEnergy IntroCommittee Meetings Time Title Location Sunday, 26 July 2015 1500-1700 hrs SRTC Awards and Communications Subcommittee Sand Lake 1500-1700 hrs SRTC Education and History Subcommittee Pocket Lake 1530-1630 hrs TAC P&E Rocket, Space & Advanced Propulsion Group Ruby Lake 1700-2000 hrs Propulsion and Energy Group Meeting Lake Eola 1900-2100 hrs LPTC Steering Committee Pocket Lake Monday, 27 July 2015 0800-0900 hrs HSABPTC Steering Committee Ruby Lake 0900-1000 hrs ABPTCs Steering Committee Clear Lake 1000-1030 hrs ABPTCs New Member Orientation Ruby Lake 1030-1100 hrs GTETC Membership Upgrade Clear Lake 1100-1200 hrs ABPSI TC Meeting Ruby Lake 1100-1200 hrs GTE TC Meeting Pocket Lake 1100-1200 hrs HSABP TC Meeting Conway Lake 1100-1200 hrs 2016 P&E Forum Technical Program Committee Clear Lake 1200-1500 hrs Nuclear and Future Flight Propulsion TC Turkey Lake 1300-1400 hrs ABPTCs Conference Subcommittee Pocket Lake 1400-1500 hrs Aircraft Electric Propulsion Path Forward Ruby Lake 1400-1500 hrs ABPTCs Honors and Awards Subcommittee Pocket Lake 1500-1600 hrs TAC P&E Operations Group Pocket Lake 1500-1600 hrs ABPTCs Education Subcommittee Ruby Lake 1600-1700 hrs ABPTCs Communications Subcommittee Conway Lake 1700-1800 hrs PAW Committee Ruby Lake 1700-1800 hrs ABP Working Groups Pocket Lake 1700-1900 hrs GEPC Leadership & Conference Team Conway Lake 1900-2200 hrs Terrestrial Energy Systems TC Sand Lake 1900-2130 hrs Propellants and Combustion TC Lake George A 1900-2200 hrs Energetic Components and Systems TC Clear Lake 1900-2200 hrs Solid Rockets TC Lake George B 1900-2200 hrs ABPTCs Committee Meeting Lake Mizell B Tuesday, 28 July 2015 1500-1600 hrs TAC P&E Products Group Pocket Lake 1700-1930 hrs Green Engineering PC Turkey Lake 1800-2200 hrs Moog Reception Ruby Lake 1800-2000 hrs Pressure Gain Combustion PC Clear Lake 1830-2100 hrs Electric Propulsion TC Pocket Lake 1900-2300 hrs Liquid Propulsion TC Orlando V 1900-2200 hrs Aerospace Power Systems TC Conway Lake 1900-2200 hrs Hybrid Rockets TC Lake Florence Wednesday, 29 July 2015 1400-1500 hrs TAC P&E Energy Group Pocket Lake

All meetings held on the lobby level at the Hilton Orlando, unless otherwise specified. www.aiaa-propulsionenergy.org 30 #aiaaPropEnergy IntroSessions at a Glance

Sessions at a Glance Overview

Energy-Focused Topic Areas Propulsion-Focused Topic Areas Advanced Engine Controls (AEC) Advanced Engine Controls (AEC) Electricity Delivery and Grid Reliability (ED) Advanced Propulsion Systems (APS) Energy Conversion Device Technology (ECD) Air Breathing Propulsion Systems Integration (ABPSI) Energy Efficiency (EE) Electric Propulsion (EP) Fossil-Fuel Power (FFP) Energetic Components and Systems (ECS) Green Engineering/Green Energy (GE) Gas Turbine Engines (GTE) ITAR (ITAR) Green Engineering/Green Energy (GE) Propulsion and Power Systems of Unmanned Systems (PP) High Speed Air Breathing Propulsion (HSABP) Thermal Management Technology (TM) Hybrid Rockets (HR) ITAR (ITAR) Liquid Propulsion (LP) Nuclear and Future Flight Propulsion (NFF) Pressure Gain Combustion (PGC) Propellants and Combustion (PC) Propulsion Aerodynamics Workshop Report Out (PAW) Propulsion Education (EDU) Solid Rocket (SR) Space Transportation (ST) System Concepts and Supporting Propulsion Technology (SC) Vehicle Systems (VS)

Abbreviation Title Date Start Time Location Advanced Engine Controls (AEC) 86-AEC-1 Advanced Engine Controls & Intelligent Systems 28-Jul 1430 hrs Lake Concord B Aircraft Electric Propulsion (AEP) 59-AEP-1 Aircraft Electric/Hybrid Propulsion 28-Jul 0900 hrs Orange E 115-ABPSI-4/AEP-2 Emerging Propulsion System Technologies 29-Jul 0900 hrs Orange E Advanced Propulsion Concepts (APC) 60-APC-1 Advanced Space Transportation Concepts 28-Jul 0900 hrs Lake Highland A 87-APC-2 Advanced Propulsion Concepts 28-Jul 1430 hrs Lake Nona B Advanced Propulsion Systems (APS) 5-APS-1 The Next Step in Human Exploration - Orion & Space Launch Systems 27-Jul 0900 hrs Lake Eola 61-APS-2 Space Solar Power System Architectures and Concepts / Solar Electric 28-Jul 0900 hrs Lake Highland B Propulsion Power Management and Distribution 116-APS-3 Power Generation for Planetary Missions 29-Jul 0900 hrs Lake Highland B Air Breathing Propulsion Systems Integration (ABPSI) 4-ABPSI-1 Inlets 27-Jul 0900 hrs Lake Sheen A 32-ABPSI-2 Integrated Propulsion 27-Jul 1500 hrs Lake Sheen A 58-ABPSI-3 Nozzles 28-Jul 0900 hrs Lake Sheen A 115-ABPSI-4/AEP-2 Emerging Propulsion System Technologies 29-Jul 0900 hrs Orange E Electricity Delivery and Grid Reliability (ED) 34-ED-1 Gulf Coast Energy Future 27-Jul 1500 hrs Lake Eola 89-ED-2/EE-4 Systems-Level Analysis for Energy Efficiency and Renewable Energy / 28-Jul 1430 hrs Lake Down B Electrical Components www.aiaa-propulsionenergy.org 31 #aiaaPropEnergy IntroSessions at a Glance

Abbreviation Title Date Start Time Location Energetic Components and Systems (ECS) 6-ECS-1 Energetic Components & System Analysis 27-Jul 0900 hrs Lake Nona B 63-ECS-2 Energetic Applications, Technology & Education 28-Jul 0900 hrs Lake Nona B 141-ECS-3 Energetic Components & Systems Educational Series 29-Jul 1500 hrs Lake Eola Energy Conversion Device Technology (ECD) 33-ECD-1 Stirling Engines and Systems 27-Jul 1500 hrs Lake Highland B 62-ECD-2 Stirling Components 28-Jul 0900 hrs Lake Lucerne 88-ECD-3 Dual Use Technology: Challenges and Opportunities 28-Jul 1430 hrs Lake Eola 140-ECD-4 Magnetohydrodynamic, Brayton, AMTEC, and Other Advanced 29-Jul 1500 hrs Lake Nona B Concepts Energy Efficiency (EE) 7-EE-1 Solar and Wind Energy for Terrestrial Applications 27-Jul 0900 hrs Lake Down B 36-EE-2 Efficient Ventilation and Moisture Control 27-Jul 1500 hrs Lake Down B 64-EE-3 Fuel Cells, Energy Storage, and Combustion 28-Jul 0900 hrs Lake Down B 89-ED-2/EE-4 Systems-Level Analysis for Energy Efficiency and Renewable Energy / 28-Jul 1430 hrs Lake Down B Electrical Components 118-EE-5 Renewable and Sustainable Energy in Florida 29-Jul 0900 hrs Lake Eola Electric Propulsion (EP) 8-EP-1 Flight Operations and Annular Ion Development 27-Jul 0900 hrs Lake Mizell A 9-EP-2 Technology Maturation and Innovative Concepts 27-Jul 0900 hrs Lake Mizell B 37-EP-3 SmallSat Systems and Thruster Diagnostics 27-Jul 1500 hrs Lake Mizell A 65-EP-5 Near-Term Higher Power Systems and Application 28-Jul 0900 hrs Lake Mizell A 66-EP-6 Resistojets and Arcjets 28-Jul 0900 hrs Lake Mizell B 90-EP-7 Hall Modeling and Cathodes 28-Jul 1430 hrs Lake Mizell A 142-EP-10 Pulsed and Micro Thrusters 29-Jul 1500 hrs Lake Mizell A Fossil-Fuel Power (FFP) 10-FFP-1 Fossil-Fuel Power Technologies I 27-Jul 0900 hrs Lake Highland B 92-FFP-2 Fossil-Fuel Power Technologies II 28-Jul 1430 hrs Lake Down A Gas Turbine Engines (GTE) 11-GTE-1 Turbine I 27-Jul 0900 hrs Lake Monroe 12-GTE-2 Compressors I 27-Jul 0900 hrs Lake Florence 67-GTE-4 Turbine II 28-Jul 0900 hrs Lake Monroe 68-GTE-5 Compressors II 28-Jul 0900 hrs Lake Florence 93-GTE-6 Combustors 28-Jul 1430 hrs Lake George B 94-GTE-7 Engine Design I 28-Jul 1430 hrs Lake Monroe 95-GTE-8 Engine Design II 28-Jul 1430 hrs Lake Florence 121-GTE-9 Turbine III 29-Jul 0900 hrs Lake Monroe 125-HSABP-5/GTE-10 High-Speed Pressurized Systems 29-Jul 0900 hrs Lake George A 143-GTE-11/HSABP-6 Detonation Engines 29-Jul 1500 hrs Lake Florence 144-GTE-12 Turbine Durability 29-Jul 1500 hrs Lake Monroe 145-GTE-13 AIAA Undergraduate Engine Design Competition 29-Jul 1500 hrs Lake Highland B Green Engineering/Green Energy (GE) 120-GE-1 Green Engineering 29-Jul 0900 hrs Lake Florence www.aiaa-propulsionenergy.org 32 #aiaaPropEnergy IntroSessions at a Glance

Abbreviation Title Date Start Time Location High Speed Air Breathing Propulsion (HSABP) 14-HSABP-1 Advances in Hypersonic Air-Breathers 27-Jul 0900 hrs Lake George A 41-HSABP-2 Computational Analysis of Supersonic Combustors 27-Jul 1500 hrs Lake George A 70-HSABP-3 Design and Development of Innovative High-Speed Air Breathing 28-Jul 0900 hrs Lake George A System 124-HSABP-4 Experimental and Computational Research in Supersonic Injection 29-Jul 0900 hrs Lake Mizell B Including Predictive Capability 125-HSABP-5/GTE- High-Speed Pressurized Systems 29-Jul 0900 hrs Lake George A 10 156-SR-6/HSABP-8 Solid Propellant Ducted Rockets 29-Jul 1500 hrs Lake Mizell B 147-HSABP-7 High Fidelity Simulations of High-Speed Air Breathing System 29-Jul 1500 hrs Lake George A Hybrid Rockets (HR) 13-HR-1 Internal Ballistics Analysis and Modeling I 27-Jul 0900 hrs Lake Sheen B 39-HR-2 Combustion Dynamics and Mixing Efficiencies I 27-Jul 1500 hrs Lake Sheen B 40-HR-3 Internal Ballistics Analysis and Modeling II 27-Jul 1500 hrs Lake Florence 69-HR-4 Design Studies Including Cost and Feasibility Analysis I 28-Jul 0900 hrs Lake Sheen B 96-HR-5 Design and Development of Novel Hybrid Rocket Concepts 28-Jul 1430 hrs Lake Sheen B 97-HR-6 Development and Evaluation of Novel Oxidizer and Fuel Formulations 28-Jul 1430 hrs Lake Highland B 98-HR-7 Hybrid Rockets – Current Programs Objectives and Updates 28-Jul 1430 hrs Lake Sheen A 122-HR-8 Combustion Stability, Motor Performance, and Related Issues 29-Jul 0900 hrs Lake Sheen B 123-HR-9 Combustion Dynamics and Mixing Efficiencies II 29-Jul 0900 hrs Lake Sheen A 146-HR-10 Design Studies Including Cost and Feasibility Analysis II 29-Jul 1500 hrs Lake Sheen B ITAR Restricted Sessions * see page 29 for more details 71-ITAR-1 Air Breathing Propulsion Systems: Nozzles and Diffusers 28-Jul 0900 hrs Orlando VI 99-ITAR-2 Advanced Rocket and Space Technology: Propellants, Docking and 28-Jul 1430 hrs Orlando VI Additive Manufacturing Liquid Propulsion (LP) 15-LP-1 Green Propellant Infusion Mission (GPIM) and Green Propulsion 27-Jul 0900 hrs Orange E 16-LP-2 Combustion Chamber Heat Transfer 27-Jul 0900 hrs Orange F 17-LP-3 Injectors I 27-Jul 0900 hrs Lake Lucerne 18-LP-4 Modelling and Simulation of Engines and Propulsion Systems I 27-Jul 0900 hrs Lake Highland A 42-LP-5 Combustion Dynamics I 27-Jul 1500 hrs Orange E 43-LP-6 Injectors II 27-Jul 1500 hrs Orange F 44-LP-7 Modelling and Simulation of Engines and Propulsion Systems II 27-Jul 1500 hrs Lake Lucerne 45-LP-8 Propellant Storage & Management I 27-Jul 1500 hrs Lake Nona B 72-LP-10 Spacecraft Propulsion Systems I 28-Jul 0900 hrs Orange F 73-LP-11 Liquid Propulsion History: Lessons Learned from Canceled Programs 28-Jul 0900 hrs Lake Eola 100-LP-12 Green Propulsion 28-Jul 1430 hrs Orange E 101-LP-13 Liquid Rocket Engines 28-Jul 1430 hrs Orange F 102-LP-14 Materials & Manufacturing 28-Jul 1430 hrs Lake Lucerne 103-LP-15 Propellant Slosh 28-Jul 1430 hrs Lake Highland A 126-LP-16 Propellant Storage & Management II 29-Jul 0900 hrs Orange F 127-LP-17 Rocket Nozzles I 29-Jul 0900 hrs Lake Lucerne

continued www.aiaa-propulsionenergy.org 33 #aiaaPropEnergy IntroSessions at a Glance

Abbreviation Title Date Start Time Location Liquid Propulsion (LP) (continued) 128-LP-18 Spacecraft Propulsion Systems II 29-Jul 0900 hrs Lake Nona B 148-LP-19 Combustion Dynamics II 29-Jul 1500 hrs Lake Lucerne 149-LP-20 Propellant Feed Systems & Fluid Machinery 29-Jul 1500 hrs Lake Highland A 150-LP-21 Rocket Nozzles II 29-Jul 1500 hrs Orange E 151-LP-22/ PGC-1/ Pressure Gain Combustion for Liquid Propulsion 29-Jul 1500 hrs Orange F PC-12 Nuclear and Future Flight Propulsion (NFF) 19-NFF-1 Nuclear Thermal Propulsion: Technology Development and 27-Jul 0900 hrs Lake Nona A Programmatics 46-NFF-2 Fusion and Alternative Nuclear Concepts 27-Jul 1500 hrs Lake Nona A 74-NFF-3 Nuclear Thermal Propulsion: Missions, Vehicles and Architectures 28-Jul 0900 hrs Lake Nona A 104-NFF-4 Future Flight Propulsion Systems 28-Jul 1430 hrs Lake Nona A 129-NFF-5 Conversations in Breakthrough Propulsion Physics: Gravity 29-Jul 0900 hrs Lake Nona A Pressure Gain Combustion (PGC) 151-LP-22/ PGC-1/ Pressure Gain Combustion for Liquid Propulsion 29-Jul 1500 hrs Orange F PC-12 Propellants and Combustion (PC) 22-PC-1 Advanced and Novel Concepts 27-Jul 0900 hrs Lake Louise 23-PC-2 Combustion Modeling and Simulation I 27-Jul 0900 hrs Lake Virginia 48-PC-3 Spray Injection and Combustion 27-Jul 1500 hrs Lake Louise 49-PC-4 Propellants and Fuels I 27-Jul 1500 hrs Lake Virginia 77-PC-5 Modeling of Combustion Dynamics, Instabilities and Noise I 28-Jul 0900 hrs Lake Louise 78-PC-6 Propellants and Fuels II 28-Jul 0900 hrs Lake Virginia 105-PC-7 Combustion Diagnostics and Experiments 28-Jul 1430 hrs Lake George A 106-PC-8 Combustion Modeling and Simulation II 28-Jul 1430 hrs Lake Louise 107-PC-9 Deflagrations and Detonations 28-Jul 1430 hrs Lake Virginia 131-PC-10 Modeling of Combustion Dynamics, Instabilities and Noise II 29-Jul 0900 hrs Lake Louise 132-PC-11 Scramjets, Supersonic Combustion 29-Jul 0900 hrs Lake Virginia 151-LP-22/ PGC-1/ Pressure Gain Combustion for Liquid Propulsion 29-Jul 1500 hrs Orange F PC-12 152-PC-13 Propellants and Fuels III 29-Jul 1500 hrs Lake Louise 153-PC-14 Rocket Motor Studies 29-Jul 1500 hrs Lake Concord B 154-PC-15 Combustion Dynamics Experiments and Control 29-Jul 1500 hrs Lake Virginia Propulsion Aerodynamics Workshop Report Out (PAW) 21-PAW-1 Nozzle Section I 27-Jul 0900 hrs Lake Concord B 47-PAW-2 Nozzle Section II 27-Jul 1500 hrs Lake Concord B 76-PAW-3 S-Duct Inlet Section 28-Jul 0900 hrs Lake Concord B Propulsion Education (EDU) 35-EDU-1 Propulsion Education I 27-Jul 1500 hrs Lake George B 117-EDU-2 Propulsion Education II 29-Jul 0900 hrs Lake George B Propulsion and Power Systems of Unmanned Systems (PP) 133-PP-1 Propulsion and Power Systems of Unmanned Systems 29-Jul 0900 hrs Lake Highland A www.aiaa-propulsionenergy.org 34 #aiaaPropEnergy IntroSessions at a Glance

Abbreviation Title Date Start Time Location Solid Rocket (SR) 24-SR-1 Solid Rocket Motor Combustion Flow Fields and Instability I 27-Jul 0900 hrs Lake Concord A 50-SR-2 Solid Rocket Motor Historical and Current Developments 27-Jul 1500 hrs Lake Concord A 79-SR-3 Solid Rocket Motor Combustion Flow Fields and Instability II 28-Jul 0900 hrs Lake Concord A 108-SR-4 Solid Rocket Motor Propellant Characteristics Analysis 28-Jul 1430 hrs Lake Concord A 135-SR-5 Solid Rocket Motor Nozzles, Thrust Management, and Ignition 29-Jul 0900 hrs Lake Concord A 156-SR-6/HSABP-8 Solid Propellant Ducted Rockets 29-Jul 1500 hrs Lake Mizell B 157-SR-7 Solid Rocket Motor Propellant Modeling and Simulation 29-Jul 1500 hrs Lake Concord A Space Transportation (ST) 25-ST-1 Space Transportation I 27-Jul 0900 hrs Lake George B 80-ST-2 Space Transportation II 28-Jul 0900 hrs Lake George B System Concepts and Supporting Propulsion Technology (SC) 134-SC-1 Engineering and Analysis for Propulsion System Design 29-Jul 0900 hrs Lake Down B 155-SC-2 Seal Material Advancements and Advanced Seal Technology 29-Jul 1500 hrs Lake George B Thermal Management Technology (TM) 51-TM-2 Heat Transfer and Transport Modeling and Analysis II 27-Jul 1500 hrs Lake Down A 81-TM-3 Thermal System Applications and Unique Environments I 28-Jul 0900 hrs Lake Down A 136-TM-4 Future Demands for Thermal Management: Opportunities and 29-Jul 0900 hrs Lake Down A Challenges 158-TM-5 Thermal System Applications and Unique Environment II 29-Jul 1500 hrs Lake Down A Vehicle Systems (VS) 159-VS-1 Advanced Vehicle System Concepts 29-Jul 1500 hrs Lake Down B

www.aiaa-propulsionenergy.org 35 #aiaaPropEnergy PARKING BOARDROOMS

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MAIN HOTEL LAYOUT LOBBY DAVID’S CLUB BAR & GRILL LOBBY BAR HILTON ORLANDO GIFT SHOP SPENCER’SFOR BUSINESS THE STEAKS & Walkway to Orange County Convention Center CENTER MARKETPLACE CHOPS MAIN ENTRANCE/PORTE COCHERE

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MAIN HOTEL LAYOUT LOBBY DAVID’S CLUB BAR &LOBBY GRILL BAR HILTON ORLANDO GIFT SPENCER’S SHOP FOR BUSINESS THE STEAKS & Walkway to Orange County Convention Center CENTER MARKETPLACE CHOPS MAIN ENTRANCE/PORTE COCHERE

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www.aiaa-propulsionenergy.org 9138 #aiaaPropEnergy Monday Monday, 27 July 2015 1-NW-1 Networking Coffee Break Ballroom Foyer 0730 - 0800 hrs Monday, 27 July 2015 2-SB-1 Monday Speakers’ Briefing In Session Room 0730 - 0800 hrs Speakers, presenters and session chairs for both the morning and afternoon technical sessions, please meet in your session room to load presentations and discuss the flow of your session. Monday, 27 July 2015 3-PLNRY-1 Opening Keynote Orange D 0800 - 0900 hrs Aviation Innovation Christopher (Chris) Lorence General Manager, Engineering Technologies GE Aviation Monday, 27 July 2015 4-ABPSI-1 Inlets Lake Sheen A Chaired by: L. LEAVITT, NASA 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3700 AIAA-2015-3701 AIAA-2015-3702 AIAA-2015-3703 36 Inward-Turning Streamline-Traced Experimental Study of Flow Field in Numerical Calibration of Mass Flow Effects of Distortion on Mass Flow Supersonic Inlet Design Method for Rectangular Sectioned 90 Degree Plug for Inlet Testing Plug Calibration Low-Boom, Low-Drag Applications Bend of an APU Style Inlet J. Sasson, Case Western Reserve J. Sasson, Case Western Reserve S. Otto, C. Trefny, J. Slater, NASA Glenn F. Lou, F. John, N. Key, Purdue University, University, Cleveland, OH; D. Davis, University, Cleveland, OH; D. Davis, Research Center, Cleveland, OH West Lafayette, IN NASA Glenn Research Center, Cleveland, NASA Glenn Research Center, Cleveland, OH; P. Barnhart, Case Western Reserve OH; P. Barnhart, Case Western Reserve University, Cleveland, OH University, Cleveland, OH Monday, 27 July 2015 5-APS-1 The Next Step in Human Exploration - Orion & Space Launch Systems Lake Eola 0900 - 1200 hrs It will be a panel where the panel members will talk about the overall space exploration program strategy and progress, and most importantly, highlight the very successful EFT-1 flight on 5 December 2014. Each panel member will also make a short presentation where they will highlight the scope of their involvement, accomplishments and milestone progress. The panel will also highlight the performance of propulsion and power subsystems on the very first, highly successful and history making Orion Flight.

Moderator: Paul Anderson, Lockheed Martin Space Systems Panelists: Joe Mayer Larry Price / Roger McNamara Brent Hughes Keith Reiley Philip Weber Donald Sauvageau Tom Martin Lockheed Martin Space Systems Lockheed Martin Space Systems Lockheed Martin Space Systems The Boeing Company NASA Kennedy Orbital ATK Aerojet Rocketdyne Monday, 27 July 2015 6-ECS-1 Energetic Components & System Analysis Lake Nona B Chaired by: K. GONTHIER, Louisiana State University and J. BAGLINI, Exodynamics Technology Incorporated 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3704 AIAA-2015-3705 AIAA-2015-3706 AIAA-2015-3707 AIAA-2015-3708 AIAA-2015-3709 Correlation between Ignition Time A Heuristic Model for Estimating A Detailed Numerical Calibration Shock Source Assessment of a Analysis of Dissipation Induced by Analysis of Linear Shaped Charge and Thermal Time Constant in Ignition Delays for Pressure Of Shock Pressure In The Gap Test Separation Nut Successive Planar Shock Loading of Igniting Rapid Deflagration Cord 1W-1A HBW EED’s Cartridges with Loosely Packed Configuration For Characterizing J. Kozmic, H. Lee, Chemring Energetic Granular Explosive using Explicit Dynamics Method L. Yang, Self, La Canada Flintridge, CA Energetic Materials Non-Ideal Energetic Materials Devices, Downers Grove, IL K. Gonthier, P. Rao, Louisiana State R. Hsiao, Pacific Scientific EMC, Hollister, H. Lee, Chemring Energetic Devices, B. Kim, J. Yoh, Seoul National University, University, Baton Rouge, LA CA Downers Grove, IL Seoul, Korea (the Republic of) Monday, 27 July 2015 7-EE-1 Solar and Wind Energy for Terrestrial Applications Lake Down B Chaired by: E. OGEDENGBE, ENERGHX Consulting/University of Lagos and S. AYAD 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3710 AIAA-2015-3711 AIAA-2015-3712 AIAA-2015-3713 AIAA-2015-3714 AIAA-2015-3715 An Introduction to the University Design of a CSP-Based Heat Heat-Pipe PV-T System with Optimization via “De - Turbulating” An Experimental Study of the Near In-Cloud Ice Accretion Modeling of KwaZulu-Natal’s Solar Energy Tracking System for Combustion Phase Change Thermal Storage to Spoked Wheels of a Solar Car Wake of Horizontal Axis Wind on Wind Turbine Blades Using an Research Amplified Flux Facility of Food Waste in a Downdraft Enhance the Energy Efficiency K. Veale, C. Bemont, C. Lawrence, Turbines Extended Messinger Model - SERAFF Bio-digester N. Ghaddar, A. Sweidan, K. Ghali, University of KwaZulu-Natal, Durban, M. Mourad, S. Ayad, O. Abd Elatif, Benha L. Sankar, M. Ali, Georgia Institute of P. Perumall, M. Brooks, J. Pitot, University A. Oshilalu, E. Ogedengbe, University of American University of Beirut, Beirut, South Africa University, Cairo, Egypt Technology, Atlanta, GA of KwaZulu-Natal, Durban, South Africa Lagos, Akoka-Yaba, Nigeria Lebanon

37 Monday, 27 July 2015 8-EP-1 Flight Operations and Annular Ion Development Lake Mizell A Chaired by: J. WILLIAMS, Colorado State University and N. ARTHUR 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3716 AIAA-2015-3717 AIAA-2015-3718 AIAA-2015-3719 AIAA-2015-3721 AIAA-2015-3720 Electric Propulsion Electronics In-Flight Operation of the Dawn Ion In-Flight Operation of the High Thrust-to-Power Annular Characterization Of Discharge Low-Power Operation and Plasma Activities in Europe - 2015 Propulsion System Through Early Hayabusa2 Ion Engine System in Engine Technology Uniformity And Performance Via Characterization of a Qualification M. Gollor, A. Franke, ESA, Noordwijk, The Orbit Operations at Ceres the EDVEGA Phase M. Patterson, R. Thomas, NASA Glenn Stimulated Beam Extraction Of A Model SPT-140 Hall Thruster Netherlands; W. Dechent, U. Schwab, C. Garner, M. Rayman, Jet Propulsion K. Nishiyama, S. Hosoda, R. Tsukizaki, H. Research Center, Cleveland, OH; M. 65 Cm Annular Ion Engine C. Garner, B. Jorns, R. Hofer, Jet Advance Space Power Equipment GmbH, Laboratory, California Institute of Kuninaka, Japan Aerospace Exploration Crofton, J. Young, The Aerospace J. Foster, N. Arthur, University of Michigan, Propulsion Laboratory, California Institute Salem, Germany; G. Glorieux, Airbus, Technology, Pasadena, CA Agency (JAXA), Sagamihara, Japan Corporation, El Segundo, CA; J. Foster, Ann Arbor, Ann Arbor, MI; M. Patterson, of Technology, Pasadena, CA; R. Liang, Elancourt, France; M. Boss, Airbus, University of Michigan, Ann Arbor, Ann NASA Glenn Research Center, Cleveland, J. Delgado, Space Systems/Loral, Palo Immenstaad, Germany; et al. Arbor, MI OH; J. Young, M. Crofton, The Aerospace Alto, CA Corporation, El Segundo, CA Monday, 27 July 2015 9-EP-2 Technology Maturation and Innovative Concepts Lake Mizell B Chaired by: R. SHASTRY, NASA Glenn Research Center and C. WORDINGHAM, Princeton University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3722 AIAA-2015-3723 AIAA-2015-3724 AIAA-2015-3725 AIAA-2015-3726 AIAA-2015-3727 Downstream Plasma Velocity Initial Thrust Measurements of Status of the Development and High-Density Electron Cyclotron Experimental Measurements of MHD and Thermal Coupled Measurement and Scaling Law of Marshall’s Ion-ioN Thruster Measurement of a Microwave Resonance Electric Propulsion Momentum Transfer in a Direct Simulation of an MPD Thruster High-Power Helicon Double Gun N. Schloeder, T. Scogin, T. Liu, M. Walker, Microplasma Source for A. Reisz, Reisz Engineers, Huntsville, AL Wave-Drive Thruster A. Kawasaki, Tokyo Institute of Thruster Georgia Institute of Technology, Atlanta, Micropropulsion M. Feldman, E. Choueiri, Princeton Technology, Yokohama, Japan; K. Kubota, N. Murakami, R. Winglee, University of GA; K. Polzin, J. Dankanich, NASA R. Dextre, University of Alabama, University, Princeton, NJ Japan Aerospace Exploration Agency Washington, Seattle, Seattle, WA Marshall Space Flight Center, Huntsville, Huntsville, Huntsville, AL (JAXA), Chofu, Japan; I. Funaki, Japan AL; et al. Aerospace Exploration Agency (JAXA), Sagamihara, Japan; Y. Okuno, Tokyo Institute of Technology, Yokohama, Japan Monday, 27 July 2015 10-FFP-1 Fossil-Fuel Power Technologies I Lake Highland B Chaired by: B. KHANDELWAL, The University of Sheffield 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3728 AIAA-2015-3729 AIAA-2015-3730 Numerical Study on the Effects Influence Of Production Pathways The Use of LNG as Aviation Fuel: of Fuel Injector Cone-Angle on And Sources Of Different Fuels On Combustion and Emission Soot Nano-Particles, CO, and Combustion Instabilities Of A Gas M. Yahyaoui, Airbus, Suresnes, France

CO2 Pollutions in a Combustion Turbine Engine

38 Chamber Burning Kerosene S. Roy, B. Khandelwal, C. Lord, University M. Darbandi, M. Ghafourizadeh, Sharif of Sheffield, Sheffield, United Kingdom University of Technology, Tehran, Iran (the Islamic Republic of); G. Schneider, University of Waterloo, Waterloo, Canada Monday, 27 July 2015 11-GTE-1 Turbine I Lake Monroe Chaired by: M. RICKLICK, Embry Riddle Aeronautical University and G. PANIAGUA 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3731 AIAA-2015-3732 AIAA-2015-3733 AIAA-2015-3734 AIAA-2015-3735 AIAA-2015-3736 Computational studies on End-wall Numerical Simulations of a Time Resolved Stereo-PIV CFD Benchmarking of Heat Combination of Ribs and Pins for CFD Benchmarking of Heat Film Cooling from a Single Row Rectangular Channel with Measurements of the Horseshoe Transfer Predictions in Internal Internal Cooling Transfer and Pressure Drop of Holes at Different Stream-wise Symmetric and Non-symmetric Vortex System in a Low Aspect Channel with Rib Turbulators M. Otto, J. Hodges, University of Central Predictions in a Pin Fin Channel Locations in a Gas Turbine Cascade Wedge-shaped Turbulators Ratio Pin-Fin Array Y. Mehta, M. Ricklick, Embry-Riddle Florida, Orlando, FL; M. Ricklick, Embry- R. Fernandes, M. Ricklick, Embry-Riddle K. Parammasivam, D. Ravi, Anna L. Tran, Z. Little, P. Tran, J. Kapat, C. Anderson, S. Lynch, Pennsylvania State Aeronautical University, Daytona Beach, FL Riddle Aeronautical University, Altamonte Aeronautical University, Daytona Beach, FL University, Chennai, India University of Central Florida, Orlando, FL University, State College, PA Springs, FL; J. Kapat, University of Central Florida, Orlando, FL Monday, 27 July 2015 12-GTE-2 Compressors I Lake Florence Chaired by: N. KEY, Purdue University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3737 AIAA-2015-3738 AIAA-2015-3739 AIAA-2015-3740 AIAA-2015-3741 Numerical Study on the Application Numerical Investigation of Near- Influence Of Rain Droplets On The Simulations of the Effect of Velocity A Parametric Shape Optimization of Circumferential Groove Casing stall Behavior of a Transonic Stage Characteristics Of An Axial Ratios on an Effusion Cooled Strategy for Compressor Vane Treatment to a Heavy Duty Gas Compressor Stage under 80% Multistage Compressor Combustor Wall with Adaptive Mesh Design Turbine Compressor at Multi- Nominal Speed Condition V. Tasdelen, University of Stuttgart, Refinement CFD and Conjugate Z. Grey, G. Modgil, Rolls-Royce Group plc, Operational Conditions R. Liu, A. Hou, S. Li, X. Song, Q. Ni, Stuttgart, Germany Heat Transfer Indianapolis, IN H. Chen, W. Song, Tsinghua University, Beihang University, Beijing, China G. Kumar, S. Drennan, Convergent Beijing, China Science, Inc., New Braunfels, TX Monday, 27 July 2015 13-HR-1 Internal Ballistics Analysis and Modeling I Lake Sheen B Chaired by: A. KARP, Jet Propulsion Laboratory and S. WHITMORE, Utah State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3742 AIAA-2015-3743 AIAA-2015-3744 AIAA-2015-3745 Modeling of Saturated and On the Quadrupole Vortex Motion Effect of Outflow Boundary Engineering Model for Hybrid Superheated N2O Heat Transfer in a Right-Cylindrical Hybrid Rocket Conditions on the Stability of Rocket Regression Rate Rates, with Experimental Engine Cylindrically-Shaped Hybrid Amplification by Helical Fuel Ports Verification T. Marquardt, J. Majdalani, O. Cecil, Rockets S. Whitmore, S. Walker, D. Merkley, Utah P. Lemieux, California Polytechnic State Auburn University, Auburn, AL T. Elliott, University of Tennessee, State University, Logan, UT University, San Luis Obispo, CA; D. Chattanooga, Chattanooga, TN; J. 39 Pastrone, P. Sanchez Arribas, Technical Majdalani, Auburn University, Auburn, AL University of Turin, Turin, Italy Monday, 27 July 2015 14-HSABP-1 Advances in Hypersonic Air-Breathers Lake George A Chaired by: J. WHITE, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3746 AIAA-2015-3747 AIAA-2015-3748 AIAA-2015-3749 AIAA-2015-3750 Analysis of Hypersonic Nozzles Mechanism and Prediction for Investigation of the Self-Starting A Method to Compute Flameout Simulations of Ethylene and with Newton and Preconditioned Occurrence of Shock Train Sharp ability of An Internal WaveRider Limits of Scramjet-Powered Hydrogen Combustions in Scramjet Newton-GMRES Methods Forward Movement Inlet for Ramjet Hypersonic Vehicles Combustor Y. Muslubas, S. Eyi, Middle East Technical K. Xu, J. Chang, W. Zhou, D. Yu, Harbin F. Zuo, G. Huang, Z. Yu, W. Tang, Nanjing C. Mbagwu, J. Driscoll, University of R. Rouzbar, S. Eyi, Middle East Technical University, Ankara, Turkey Institute of Technology, Harbin, China University of Aeronautics and Astronautics, Michigan, Ann Arbor, Ann Arbor, MI University, Ankara, Turkey Nanjing, China Monday, 27 July 2015 15-LP-1 Green Propellant Infusion Mission (GPIM) and Green Propulsion Orange E Chaired by: T. POURPOINT, Purdue University and D. SARGENT, Federal Aviation Administration 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3751 AIAA-2015-3752 AIAA-2015-3753 AIAA-2015-3754 AIAA-2015-3755 AIAA-2015-3756 Green Propellant Infusion Mission Adiabatic Compression Testing of GPIM AF-M315E Propulsion System Plume Characterization of a FTIR Analysis of Triethylamine Fracture Mechanics Testing of Program Overview, Status, and AF-M315E R. Spores, Aerojet Rocketdyne, Redmond, Laboratory Model 22 N GPIM Borane and White Fuming Nitric Titanium 6Al-4V in AF-M315E Flight Operations P. Quach, ERC, Inc., Edwards AFB, CA; WA Thruster via High-Frequency Acid Gaseous Combustion Products J. Sampson, J. Martinez, NASA Kennedy C. McLean, Ball Aerospace & Technologies A. Brand, Air Force Research Laboratory, Raman Spectroscopy A. Mugenda, O. Busari, A. Benhidjeb- Space Center, Cape Canaveral, FL Corporation, Boulder, CO Edwards AFB, CA; G. Warmoth, ERC, Inc., G. Williams, J. Kojima, Ohio Aerospace Carayon, T. Pourpoint, Purdue University, Edwards AFB, CA Institute, Cleveland, OH; L. Arrington, M. West Lafayette, IN Deans, D. Fischer, B. Reed, NASA Glenn Research Center, Cleveland, OH; et al. Monday, 27 July 2015 16-LP-2 Combustion Chamber Heat Transfer Orange F Chaired by: M. PIZZARELLI, University of Rome and M. NARAGHI, Manhattan College 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3757 AIAA-2015-3758 AIAA-2015-3759 AIAA-2015-3760 AIAA-2015-3761 AIAA-2015-3762 Convective and Radiative Numerical Analysis of Chamber Comparison of Heat Transfer Regenerative Cooling Performance Extension of the Laminar Flamelet Potential Benefits of Pressure Gain Contributions to Wall Heat Transfer Wall Heat Fluxes in a LOX/CH4 Characteristic of Rectangular Analysis of the LE-X Engine Model to Account for Wall Heat Combustion in Liquid Rocket Engine in Liquid Rocket Engine Thrust Single Injector Rocket and Oval Cooling Channels of Combustion Chamber Losses in Rocket Engine Combustor Pre-Burners Chambers A. French, P. Natale, Italian Aerospace Regeneratively Cooled Rocket H. Negishi, Y. Daimon, N. Negoro, A. Simulations S. Coogan, Southwest Research Institute, B. Betti, D. Bianchi, G. Leccese, D. Research Center (CIRA), Capua, Italy Engines Kurosu, Japan Aerospace Exploration A. Zambon, A. Hosangadi, W. Calhoon, San Antonio, TX 40 Lentini, F. Nasuti, University of Rome “La R. Cavillon, Alstom, Villeurbanne, France; Agency (JAXA), Tsukuba, Japan Combustion Research and Flow Sapienza”, Rome, Italy M. Naraghi, Manhattan College, Riverdale, Technology, Inc., Pipersville, PA NY; G. Chen, University of Maryland, College Park, College Park, MD Monday, 27 July 2015 17-LP-3 Injectors I Lake Lucerne Chaired by: I. LEYVA and S. CHIANESE, SpaceX 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3763 AIAA-2015-3764 AIAA-2015-3765 AIAA-2015-3766 AIAA-2015-3767 Impinging Fuel Injector Atomization Dynamic Characteristics of Open- A Cold-flow Experimental Characterization of Injector Transient Response of a Liquid and Combustion Modeling type Swirl Injector with Varying Observation of the Two-stage Response in a Hypergolic Pulse Injector to a Transverse Pressure K. Brinckman, G. Feldman, A. Hosangadi, Geometry Impinging Type Injector for Rocket Detonation Rocket Engine Wave Combustion Research and Flow Y. Chung, H. Kim, S. Jeong, Y. Yoon, Propulsion B. Kan, S. Heister, Purdue University, West D. Lim, S. Heister, D. Stechmann, B. Technology, Inc., Pipersville, PA Seoul National University, Seoul, Korea B. Huang, T. Yuan, Y. Chen, Y. Su, Lafayette, IN Kan, B. Justice, Purdue University, West (the Republic of) National Cheng Kung University, Tainan, Lafayette, IN Taiwan Monday, 27 July 2015 18-LP-4 Modelling and Simulation of Engines and Propulsion Systems I Lake Highland A Chaired by: T. GIEL, Jacobs Technology and A. LEKEUX, CNES 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3768 AIAA-2015-3769 AIAA-2015-3770 AIAA-2015-3771 Cavitating Venturi Model Using CFD Modeling of the Multipurpose Application of Multidisciplinary Characterization of Cryogenic Standard Element and Options in Hydrogen Test Bed (MHTB) Analysis and Optimization on AR1 Liquid Propellants flashing Commercially Available Lumped- Self-Pressurization and Spray Using ModelCenter® phenomena under vacuum Parameter Software Bar Mixing Experiments in M. Long, J. Horton, Aerojet Rocketdyne, conditions G. Beck, Southwest Research Institute, Normal Gravity: Effect of the West Palm Beach, FL M. Luo, B. Vasques, O. Haidn, Technical San Antonio, TX Accommodation Coefficient on the University of Munich, Munich, Germany Tank Pressure O. Kartuzova, M. Kassemi, NASA Glenn Research Center, Cleveland, OH Monday, 27 July 2015 19-NFF-1 Nuclear Thermal Propulsion: Technology Development and Programmatics Lake Nona A Chaired by: J. WARREN, NASA Headquarters and C. JOYNER, Aerojet Rocketdyne 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3772 AIAA-2015-3773 AIAA-2015-3774 AIAA-2015-3775 AIAA-2015-3776 AIAA-2015-3777 The NASA Advanced Exploration Review of Nuclear Thermal Affordable Development and Subscale Validation of the Extrusion Development of Coating Development on Graphite- Systems Nuclear Thermal Propulsion Ground Test Options Demonstration of a Small NTR Subsurface Active Filtration of Graphite-Based Composite Fuel for Based Composite Fuel for Nuclear Propulsion Project D. Coote, K. Power, NASA Stennis Space Engine and Stage: A Preliminary Exhaust (SAFE) Approach to NTP Nuclear Thermal Propulsion Thermal Propulsion M. Houts, D. Mitchell, T. Kim, W. Emrich, Center, Stennis Space Center, MS; H. NASA, DOE and Industry Ground Testing M. Trammell, B. Jolly, A. Qualls, Oak Ridge B. Jolly, M. Trammell, A. Qualls, Oak Ridge 41 R. Hickman, H. Gerrish, NASA Marshall Gerrish, G. Doughty, NASA Marshall Space Assessment W. Marshall, S. Borowski, NASA Glenn National Laboratory, Oak Ridge, TN National Laboratory, Oak Ridge, TN Space Flight Center, Huntsville, AL; et al. Flight Center, Huntsville, AL S. Borowski, R. Sefcik, NASA Glenn Research Center, Cleveland, OH; C. Martin, Research Center, Cleveland, OH; J. Fittje, D. Kelly, National Security Technologies, Vantage Partners, LLC, Brook Park, OH; A. LLC, Las Vegas, NV; M. Bulman, Aerojet Qualls, B. Schnitzler, Oak Ridge National Rocketdyne, Sacramento, CA Laboratory, Oak Ridge, TN; A. Weitzberg, Self, Woodland Hills, CA; et al. Monday, 27 July 2015 20-NW-2 Networking Coffee Break Exposition Hall 0900 - 0930 hrs Monday, 27 July 2015 21-PAW-1 Nozzle Section I Lake Concord B Chaired by: C. CHUCK, Boeing Commercial Airplanes and A. DELOT, ONERA 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3778 AIAA-2015-3779 Oral Presentation Oral Presentation Perspectives on Propulsion CFD for NSAWET Results of the Dual Dsfr Nozzle Performance A Comparative Study on Nozzle Applications Relevant to Separate Flow Reference Nozzle Predictions And CFS Boxermesh Axisymmetric Dual Flow Reference the AIAA Propulsion Aerodynamics from AIAA PAW02 Evaluation Using Rolls-Royce In- Nozzle Workshop Z. Li, H. Chen, Y. Zhang, Tsinghua House Hydra CFD Tool N. Vijayakumar, D. Wilson, University of N. Domel, Lockheed Martin Aeronautics University, Beijing, China J. Sokhey, Rolls-Royce North America, Texas at Arlington, Arlington, TX Company, Fort Worth, TX Indianapolis, IN; N. Grech, M. Slaby, Rolls- Royce plc, Derby, United Kingdom Monday, 27 July 2015 22-PC-1 Advanced and Novel Concepts Lake Louise Chaired by: R. PITZ, Vanderbilt University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3780 AIAA-2015-3781 AIAA-2015-3782 AIAA-2015-3783 An Innovative Turbo Compound Radial Effects on Rotating Towards Non-premixed Injection Effects Of Thermites On Burning Internal Engine Concept for UAV Detonation Engine Swirl Modeling of Rotating Detonation And Radiation Performances Of and Other Applications C. Nordeen, University of Connecticut, Engines Foil-Typed Mtv Infrared Decoys J. Taylor, J. Mehta, J. Charneski, M. Storrs, Storrs, CT; D. Schwer, A. Corrigan, D. Schwer, K. Kailasanath, Naval Research J. Du, H. Guan, J. Li, Nanjing University of Lindstrom, K. Launglucknavalai, Belcan Naval Research Laboratory, Washington, Laboratory, Washington, DC Science and Technology, Nanjing, China Corporation, Cincinnati, OH DC; B. Cetegen, University of Connecticut, Storrs, Storrs, CT Monday, 27 July 2015 23-PC-2 Combustion Modeling and Simulation I Lake Virginia Chaired by: M. ANAND, Rolls-Royce Corp and F. DIMARE, DLR 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3784 AIAA-2015-3785 AIAA-2015-3786 AIAA-2015-3787 3D Computation For Torch Jet Parametric Design of Injectors for Parametric Study of Effect of Investigation Of The Effect Of Co/ Ignition Of Premixed Methane- LDI-3 Combustors Geometric Configurations of Counter Configurations Of A Double Hydrogen-Air Blends In A K. Ajmani, Vantage Partners, LLC, Microjets in an Axisymmetric Dump Swirler Airblast Atomizer In An Pre-Chamber Constant Volume Cleveland, OH; H. Mongia, Purdue Combustor Flow Annular Turbojet Combustor With Combustor At Variable Pre- University, West Lafayette, IN; P. Lee, M. Vellakal, A. Taha, University of Illinois, Computational Fluid Dynamics Chamber Pressure Woodward FST, Inc., Zeeland, MI Urbana-Champaign, Urbana, IL H. Bolat, TUBITAK-SAGE, Ankara, Turkey; 42 M. Khan, K. Paik, M. Nalim, Indiana S. Uslu, TOBB University of Economics and University-Purdue University Indianapolis, Technology, Ankara, Turkey Indianapolis, IN Monday, 27 July 2015 24-SR-1 Solid Rocket Motor Combustion Flow Fields and Instability I Lake Concord A Chaired by: J. MAJDALANI, Auburn University and J. HORNICK, Aerojet Rocketdyne 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3788 AIAA-2015-3789 AIAA-2015-3790 On Steady Trkalian High Speed Transverse Vortico-Acoustic Waves Study On The Effects Of Gas Flows: Swirling Compressible in the Presence of Strong Mean Temperature On Cold Flow Test Of Motions in Rockets with Headwall Flow Shear Layers Nozzle Damping Injection P. Kovacic, J. Batterson, J. Majdalani, B. Sun, J. Li, W. Su, N. Wang, Beijing O. Cecil, J. Majdalani, J. Batterson, Auburn Auburn University, Auburn, AL Institute of Technology, Beijing, China University, Auburn, AL Monday, 27 July 2015 25-ST-1 Space Transportation I Lake George B Chaired by: M. SIR, Aerospace Corp (COMP) 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3791 AIAA-2015-3792 AIAA-2015-3793 AIAA-2015-3794 Rho-Isp Revisited and Basic Stage Orion EFT-1 Propulsion Test Results Airbus Defence & Space Spacecraft Exploring NASA Human Spaceflight Mass Estimating for Launch Vehicle S. Norris, Lockheed Martin Corporation, Passivation Initiative and Pioneering Scenarios Conceptual Sizing Studies Denver, CO P. Fernando, R. Baldwin, D. Briot, Airbus, E. Zapata, NASA Kennedy Space Center, T. Kibbey, Jacobs, Huntsville, AL Stevenage, United Kingdom Cape Canaveral, FL Monday, 27 July 2015 26-TM-1 Heat Transfer and Transport Modeling and Analysis I Lake Down A Chaired by: C. TARAU, Advanced Cooling Technologies and M. CHOI, NASA-Goddard Space Flight Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3795 AIAA-2015-3796 AIAA-2015-3797 AIAA-2015-3798 AIAA-2015-3799 Validation Of The Thermo-Fluid CFD Analysis and Full Scale Wind Diffusion Effect on Hypersonic Flow Design of the Ventilation System Forced Convective Heat Transfer in Characteristics For Laminated Tunnel and Flight Testing of a Using Fick’s Law in an Underground Car Park:The AL2O3-air Nanoaerosol Screens Woven Copper Wire Mesh Complex Auxiliary Power Unit H. Gur, S. Eyi, Middle East Technical Effect of Jet Fans Configurations M. Trivedi, C. Johansen, University of Enhancing The Regenerative Intake System University, Ankara, Turkey E. Khalil, S. Gomaa, Cairo University, Calgary, Calgary, Canada Compact Heat Exchanger Heat J. Hernanz, Airbus, Getafe, Spain; B. Giza, Egypt Transfer Areas Bouldin, Honeywell International, Inc., F. Senda, Nuclear Energy Corporation Phoenix, AZ; M. Gallego, Airbus, Getafe, of South Africa, Brits, South Africa; R. Spain Dobson, University of Stellenbosch, Stellenbosch, South Africa Monday, 27 July 2015 27-F360-1 Aircraft Electric Propulsion: Bridging the Gap Orlando IV 0930 - 1200 hrs Aircraft electric and hybrid electric propulsion (EP/HEP) is of increasing excitement in the industry and represents an area of worldwide growth. The focus of this panel will be on the EP/HEP evolutionary path, and the challenge to bridge between emerging small aircraft concepts and future commercial aircraft all-electric and hybrid gas-electric concepts. In this session, content presented in recent forums, will be highlighted and tailored for P&E’s propulsion/energy-centric audience, helping to connect the topic between different national and international forums.

Moderator: Ruben Del Rosario, NASA Glenn Research Center 43 Panelists: Andrew Gibson Charles Lents Frank Anton Michael Armstrong Marty Bradley Johannes Stuhlberger ESAero United Technologies Research Center Siemens Rolls-Royce Corporation The Boeing Company Airbus

Monday, 27 July 2015 28-LECT-1 U.S. Air Force Prize Announcement Orlando IV 1200 - 1230 hrs The Air Force has just announced a $2 million technology prize designed to motivate independent development of a small, lightweight, fuel-efficient engine. The turbine power plant will be highly efficient over a range of power settings, have a high power density, and use a logistically available battlefield fuel (Jet A). The first engine to meet specific performance criteria in a verification test in the Air Force Research Laboratory will receive the prize. Full details are available at www.airforceprize.com. Please join us to learn specifics about the Air Force Turbine Prize, what it is, how to get involved, timelines, ask questions, etc. Monday, 27 July 2015 29-NW-3 Lunch Break 1200 - 1330 hrs Lunch on your own. Please see the information desk for a list of local restaurants. Monday, 27 July 2015 30-PLNRY-2 Global Cooperation & Economic Development Orange D 1330 - 1500 hrs The current international environment has introduced significant challenges to global cooperation, particularly in the propulsion community. This panel will examine the implications of the changing geopolitical landscape and the importance of international cooperation in our industry. How do partners cooperate without becoming overly dependent on any one player?

Moderator: Jim Maser, Vice President, Strategy, Marketing and Business Development, Pratt & Whitney Panelists: Jean-Paul Ebanga Richard “Ric” Parker Marc Vales Les Kovacs Bernard Zimmerman President and CEO, CFM International Director of Research and Technology, Rolls-Royce plc Head of Future Programmes, Airbus Safran Launches Director of Washington Operations, United Launch Vice-President Group Strategy & Development, Alliance (ULA) Pratt & Whitney

Monday, 27 July 2015 31-NW-4 Networking Coffee Break Exposition Hall 1430 - 1500 hrs Monday, 27 July 2015 32-ABPSI-2 Integrated Propulsion Lake Sheen A Chaired by: T. BERENS, AIRBUS Defence and Space and H. CHEN, Tsinghua University 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-3800 AIAA-2015-3801 AIAA-2015-3802 AIAA-2015-3803 AIAA-2015-3804 AIAA-2015-3805 CFD-based Analysis of Boundary Performance Analysis of a Design Point Analysis of an Hybrid Passive Flow Control in Boundary Fan Response to Inlet Swirl Mail-Slot Nacelle Shape Design Layer Ingesting Propulsion Distributed Propulsion System with Fuel Cell Gas Turbine Cycle for Layer Ingesting Semi Submerged Distortions Produced by for N3-X Hybrid Wing-Body 44 S. Ochs, G. Tillman, J. Joo, D. Voytovych, Boundary Layer Ingestion Advanced Distributed Propulsion Inlet Boundary Layer Ingesting Aircraft Configuration United Technologies Research Center, Inc., E. Valencia, National Technical University, Systems U. Küçük, TUBITAK-SAGE, Ankara, Turkey; Configurations H. Kim, SAIC, Brookpark, OH; M. Liou, East Hartford, CT Quito, Ecuador; C. Liu, L. Panagiotis, R. E. Valencia, National Technical University, Ö. Baran, TED University, Ankara, Turkey; D. Frohnapfel, W. O’Brien, Virginia M. Liou, NASA Glenn Research Center, Singh, D. Nalianda, Cranfield University, Quito, Ecuador; V. Hidalgo, Tsinghua O. Uzol, Middle East Technical University, Polytechnic Institute and State University, Cleveland, OH Cranfield, United Kingdom University, Beijing, China; L. Panagiotis, D. Ankara, Turkey Blacksburg, VA Nalianda, R. Singh, Cranfield University, Cranfield, United Kingdom; C. Liu, Shanghai Jiao Tong University, Shanghai, China Monday, 27 July 2015 33-ECD-1 Stirling Engines and Systems Lake Highland B Chaired by: D. HILL and S. WILSON, NASA Glenn Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3806 AIAA-2015-3807 AIAA-2015-3808 AIAA-2015-3809 Advanced Stirling Convertor (ASC) Advanced Stirling Convertor Dual Characterization of the Advanced Modular Stirling Radioisotope Technology Maturation Convertor Controller Testing at Stirling Radioisotope Generator Generator W. Wong, S. Wilson, NASA Glenn Research NASA Glenn Research Center in EU2 P. Schmitz, Power Computing Solutions, Center, Cleveland, OH; J. Collins, K. the Radioisotope Power System E. Lewandowski, S. Oriti, NASA Glenn Inc., North Ridgeville, OH; L. Mason, NASA Wilson, Sunpower, Inc., Athens, OH Systems Integration Laboratory Research Center, Cleveland, OH Glenn Research Center, Cleveland, OH; G. Dugala, L. Taylor, M. Bell, Vantage J. Schreiber, Ohio Aerospace Institute, Partners, LLC, Cleveland, OH; M. Fraeman, Brookpark, OH D. Frankford, Johns Hopkins University Applied Physics Laboratory, Laurel, MD Monday, 27 July 2015 34-ED-1 Gulf Coast Energy Future Lake Eola 1500 - 1730 hrs This is a discussion panel where the panel members will talk about the future of Gulf Coast Energy, with emphasis on challenges and opportunities. Each panel member will also make a short presentation to highlight his/her scope of involvement in Gulf Coast energy and view of the Gulf Coast Energy future. The panel consists of leaders from the Gulf Coast energy sectors.

Moderator: Dave Robau, Executive Director, Gulf Coast Energy Network. Panelists: Kelley Smith-Burk Ervan Hancock Dub Taylor Director, Florida Office of Energy, Executive Office of the Governor Manager, Renewable and Green Strategies, Georgia Power Director, Texas Energy Conservation Office

Monday, 27 July 2015 35-EDU-1 Propulsion Education I Lake George B Chaired by: R. TYSON, University of Alabama in Huntsville and M. HITT, The University of Alabama in Huntsville 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-3810 AIAA-2015-3811 AIAA-2015-3812 AIAA-2015-3813 AIAA-2015-3814 AIAA-2015-3815 Experiments with Pintle Injector Internal Ballistics Model for a Sweeping Jet Actuators for Active Development of a Turbine Engine Sky-Infra Project in Mongolia and Design of an RF Ion Thruster Design and Development Mixed Hybrid Rocket Motor Flow Control and Compressor Test Rigs for Aero-Space Engineering Education J. Botha, T. Jones, J. de Swardt, University R. Nardi, V. Perez, A. Pimenta, M. Mascaro, D. Jones, D. Lineberry, M. Zamora, B. Pafford, U.S. Military Graduate Level Education and Project of Stellenbosch, Stellenbosch, South Africa Technological Institute of Aeronautics R. Frederick, University of Alabama, Academy, West Point, NY Research Y. Obikane, Nagaoka University of (ITA), São José dos Campos, Brazil Huntsville, Huntsville, AL; M. Moser, K. S. Arnold, P. Anusonti-Inthra, J. Cox, J. Technology, Nagaoka, Japan; B. Choijil, Mahaffy, Exquadrum, Inc., Adelanto, CA Hartman, University of Tennessee Space Mongolia University of Science and Institute, Tullahoma, TN Technology, Ulaanbaatar, Mongolia 45 Monday, 27 July 2015 36-EE-2 Efficient Ventilation and Moisture Control Lake Down B Chaired by: N. GHADDAR, American University of Beirut and E. KHALIL, Cairo University 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-3816 AIAA-2015-3817 AIAA-2015-3818 AIAA-2015-3819 AIAA-2015-3820 AIAA-2015-3821 Optimized Operation of Moisture Buffering Capacity of The Energy Performance Of A On The Computations of Air Flow Numerical Investigations of Indoor Thermal Comfort Through Mixing Displacement Ventilation Combined Hygroscopic Curtains: Theoretical Building Air Conditioning System Regimes and Thermal Patterns Air Quality in Infection Isolation and Personalized Ventilation with a Novel Evaporative Cooled and Experimental Study Integrated With A Basement in an Air-Conditioned Open Sport Rooms Systems Ceiling for a Typical Office in the K. Ghali, S. Salloum, N. Ghaddar, Cooling Source Driven By Trombe Facility A. Eldegwy, E. Khalil, E. Bially, S. Mourad, H. Elmaghraby, E. Khalil, Cairo University, City of Beirut American University of Beirut, Beirut, Wall M. Sobhi, E. Khalil, Cairo University, Cairo University, Giza, Egypt Giza, Egypt K. Ghali, M. Itani, N. Ghaddar, American Lebanon N. Ghaddar, K. Ghali, M. Badawiyeh, Giza, Egypt University of Beirut, Beirut, Lebanon American University of Beirut, Beirut, Lebanon Monday, 27 July 2015 37-EP-3 SmallSat Systems and Thruster Diagnostics Lake Mizell A Chaired by: E. CARDIFF, NASA and M. GLASCOCK 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3822 AIAA-2015-3823 AIAA-2015-3824 AIAA-2015-3825 AIAA-2015-3826 Development of a Compact Hall Iodine Hall Thruster Feed System Computational Study of Mass- Characterization of Vacuum Study of the Discharge Chamber Thruster in the 50-150 Watt Range Design, Development and Testing Less Thruster for Nano-Satellite Facility Background Gas Through Magnetic Field Configuration M. Tajmar, Technical University of Dresden, J. Dankanich, K. Polzin, NASA Marshall Applications Simulation and Considerations for Effects on the Electron Cyclotron Dresden, Germany Space Flight Center, Huntsville, AL G. Font, U.S. Air Force Academy, Colorado Electric Propulsion Ground Testing Resonance (ECR) Microwave Ion Springs, CO J. Yim, NASA Glenn Research Center, Thruster Cleveland, OH; J. Burt, Air Force Research Y. Kamis, M. Celik, Bogazici University, Laboratory, Wright-Patterson AFB, OH Istanbul, Turkey Monday, 27 July 2015 39-HR-2 Combustion Dynamics and Mixing Efficiencies I Lake Sheen B Chaired by: S. CLAFLIN, Aerojet Rocketdyne and D. PASTRONE, Politecnico di Torino 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3827 AIAA-2015-3828 AIAA-2015-3829 AIAA-2015-3830 AIAA-2015-3831 Visualization of Flow Dynamics in Fuel-rich Combustion Characteristics Parametric Visualization Study of A Visual Study of the Combustion of Experimental Tests of Throttleable

the Post Chamber of Hybrid Rocket of Hybrid Rocket Engine Self-Pressurizing Propellant Tank High-Regression Rate and Classical H2O2/PE Hybrid Rocket Motors using Chemiluiminescence Images D. Lee, C. Lee, Konkuk University, Seoul, Dynamics Hybrid Rocket Fuels S. Zhao, P. Wang, H. Tian, N. Yu, G. Cai, G. Choi, Y. Moon, C. Lee, Konkuk Korea (the Republic of) J. Zimmerman, B. Cantwell, Stanford E. Jens, V. Miller, F. Mechentel, B. Beihang University, Beijing, China; P. University, Seoul, Korea (the Republic of) University, Stanford, CA; G. Zilliac, NASA Cantwell, S. Hubbard, Stanford University, Zeng, Beijing Institute of Electronic System Ames Research Center, Moffett Field, CA Stanford, CA Engineering, Beijing, China 46 Monday, 27 July 2015 40-HR-3 Internal Ballistics Analysis and Modeling II Lake Florence Chaired by: B. MADHANABHARATAM, Aerospace Consultant and B. EVANS, Stanford University 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3832 AIAA-2015-3833 AIAA-2015-3834 AIAA-2015-3835 Flight Performance Simulations of Scaling of Hybrid Rocket Motors Hybrid Rocket Engine Transient Numerical Analysis of Port Vertical Launched Sounding Rockets with Swirling Oxidizer Injection Internal Ballistic Simulation Diameter Effect on Hybrid Rocket Using Altering-Intensity Swirling- E. Paccagnella, University of Padua, D. Greatrix, Ryerson University, Toronto, Fuel Regression Rate with Axial Oxidizer-Flow-Type Hybrid Motors Padua, Italy; A. Karabeyoglu, Space Canada Injection K. Ozawa, K. Kitagawa, T. Shimada, Propulsion Group, Inc., Palo Alto, CA; F. D. Bianchi, F. Nasuti, University of Rome Institute of Space and Astronautical Barato, D. Pavarin, University of Padua, “La Sapienza”, Rome, Italy; C. Carmicino, Sciense, Japan Aerospace Exploration Padua, Italy University of Naples “Federico II”, Naples, Agency, Sagamihara, Japan Italy Monday, 27 July 2015 41-HSABP-2 Computational Analysis of Supersonic Combustors Lake George A Chaired by: D. MACINNIS, Raytheon Missile Systems and T. SMITH, Boeing Engineering Operations & Technology 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3836 AIAA-2015-3837 AIAA-2015-3838 AIAA-2015-3839 AIAA-2015-4251 4D Data Assimilation for Large Simulation of Kerosene Combustion Understanding Scramjet A Coupled Aerodynamic and An Investigation of Boundary- Eddy Simulation of High Speed Sustaining with Cavities in a Strut- Combustion Using LES of the Propulsive Performance Analysis of Layer Separation in the Scramjet Turbulent Combustion Based RBCC Engine HyShot II Combustor: Stable the Generic Hypersonic Vehicle Combustor H. Mirgolbabaei, C. Patton, T. Wignall, J. J. Ye, H. Pan, F. Qin, X. Wei, X. Tang, Combustion and Incipient Thermal F. Ferguson, N. Dasque, H. Mrema, N. Kubo, Tohoku University, Sendai, Japan; Edwards, T. Echekki, North Carolina State S. Zhang, Northwestern Polytechnical Choking J. Kizito, North Carolina A&T State S. Tomioka, Japan Aerospace Exploration University, Raleigh, NC University, Xi’an, China K. Nordin-Bates, C. Fureby, Swedish University, Greensboro, NC; F. Malo- Agency (JAXA), Kakuda, Japan Defense Research Agency (FOI), Molina, Air Force Research Laboratory, Stockholm, Sweden Wright-Patterson AFB, OH Monday, 27 July 2015 42-LP-5 Combustion Dynamics I Orange E Chaired by: D. LINEBERRY, UAH Propusion Research Center and S. SCHUMAKER, Air Force Reseach Laboratory 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3840 AIAA-2015-3841 AIAA-2015-3842 AIAA-2015-3843 AIAA-2015-3844 Response Function Modeling in the Determination of Heat Release Comparison of Laminar and Studies on Injection-Coupled Unsteady Energy Transport Applied Study of Longitudinal Combustion Response Function from 2D Hybrid Linear Eddy Model Closures for Instability for Liquid Propellant to Flame Transfer Functions and Instability by a Quasi-1D Eulerian RANS-LES Data for the CVRC Combustion Instability Simulations Rocket Engines Reduced Order Models Solver Combustor M. Harvazinski, D. Talley, V. Sankaran, K. Kobayashi, Japan Aerospace Exploration E. Jacob, GTL Company, Tullahoma, TN; J. M. Frezzotti, F. Nasuti, University of Rome M. Frezzotti, F. Nasuti, University of Rome Air Force Research Laboratory, Edwards Agency (JAXA), Kakuda, Japan; T. Batterson, Auburn University, Auburn, AL 47 “La Sapienza”, Rome, Italy; C. Huang, C. “La Sapienza”, Rome, Italy; C. Huang, C. AFB, CA Shimizu, Japan Aerospace Exploration Merkle, W. Anderson, Purdue University, Merkle, W. Anderson, Purdue University, Agency (JAXA), Sagamihara, Japan; Y. West Lafayette, IN West Lafayette, IN Daimon, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; Y. Nunome, T. Tomita, Japan Aerospace Exploration Agency (JAXA), Kakuda, Japan; A. Kurosu, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; et al. Monday, 27 July 2015 43-LP-6 Injectors II Orange F Chaired by: S. CHIANESE, SpaceX and I. LEYVA 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3845 AIAA-2015-3846 AIAA-2015-3847 Optical Measurements of Ethanol/ Experimental Study on the Effects Semi-Hypergolic Kerosene/ Liquid Oxygen Rocket Engine of Varying the Impingement Hydrogen Peroxide Fuel System Combustor with Planar Pintle Distance of Like-Doublet Injectors and Its Auto-Ignition Injector Injector B. Sweeney, R. Frederick, University of Design K. Sakaki, H. Kakudo, S. Nakaya, M. Alabama, Huntsville, Huntsville, AL T. Yuan, Y. Chen, B. Huang, National Tsue, University of Tokyo, Tokyo, Japan; Cheng Kung University, Tainan, Taiwan H. Isochi, Uematsu Electric Company, Ltd., Akabira, Japan; K. Suzuki, Intersteller Technologies, Inc., Taiki, Japan; et al. Monday, 27 July 2015 44-LP-7 Modelling and Simulation of Engines and Propulsion Systems II Lake Lucerne Chaired by: A. LEKEUX, CNES and M. MASQUELET, GE Global Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3848 AIAA-2015-3849 AIAA-2015-3850 AIAA-2015-3851 AIAA-2015-3852 Complex Lamellar Cyclonic Vortex Characterization of Particle Generalized Fluid System Chemical And CFD Modelling Of Assessment of a Conjugate in a Cylindrical Chamber with a Trajectories in the Bidirectional Simulation Program (GFSSP) - Sub-Scale Bread-Board Igniter Heat Transfer Model for Rocket Hollow Core Vortex Engine Version 6 Based On Experimental Data Engine Cooling Channels Fed with T. Barber, O. Cecil, J. Majdalani, Auburn B. Maicke, Pennsylvania State University, A. Majumdar, A. Leclair, R. Moore, NASA Assessment Supercritical Methane University, Auburn, AL Harrisburg, PA; J. Majdalani, Auburn Marshall Space Flight Center, Huntsville, P. Natale, Italian Aerospace Research M. Pizzarelli, F. Nasuti, University of Rome University, Auburn, AL AL; P. Schallhorn, NASA Kennedy Space Center (CIRA), Capua, Italy “La Sapienza”, Rome, Italy; R. Votta, F. Center, Cape Canaveral, FL Battista, Italian Aerospace Research Center (CIRA), Capua, Italy Monday, 27 July 2015 45-LP-8 Propellant Storage & Management I Lake Nona B Chaired by: V. AHUJA, CRAFT Tech and C. KIRCHBERGER, German Aerospace Center (DLR) 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3853 AIAA-2015-3854 AIAA-2015-3855 AIAA-2015-3856 Preliminary Simulations of Ullage Comparison of Computational Numerical Modeling of Boiling Flow CFD Extraction of Heat Transfer Dynamics in Microgravity during Results with a Low-g, Nitrogen in a Cryogenic Propulsion System Coefficient in Cryogenic Propellant Jet Mixing Portion of the Tank Slosh and Boiling Experiment Y. Umemura, Japan Aerospace Exploration Tanks Pressure Control Experiments M. Stewart, J. Moder, NASA Glenn Agency (JAXA), Ibaraki, Japan; T. Himeno, H. Yang, CFD Research Corporation, J. Moder, K. Breisacher, NASA Glenn Research Center, Cleveland, OH University of Tokyo, Tokyo, Japan; Huntsville, AL; J. West, NASA Marshall

48 Research Center, Cleveland, OH K. Kinefuchi, N. Tani, H. Negishi, H. Space Flight Center, Huntsville, AL Kobayashi, Japan Aerospace Exploration Agency (JAXA), Ibaraki, Japan; et al. Monday, 27 July 2015 46-NFF-2 Fusion and Alternative Nuclear Concepts Lake Nona A Chaired by: R. SEDWICK, University of Maryland and M. RODRIGUEZ 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3857 AIAA-2015-3858 AIAA-2015-3859 AIAA-2015-3860 AIAA-2015-3861 Simulation of Hemispherical From Laser Pulse Propulsion A Multiphysics Smoothed Particle Simulation of an Inertial Progress towards the Development Nozzles for Pulsed Plasma to Fusion Pulse Propulsion: An Hydrodynamics Model of Erosion Electrostatic Confinement Device of a Traveling Wave Direct Energy Propulsion Applications Evolutionary Approach in Space-Based Nuclear Fusion Using a Hermite N-body Individual Converter for Aneutronic Fusion K. Schillo, J. Cassibry, S. Thompson, B. Cassenti, University of Connecticut, Reactor Components Time-step Scheme Propulsion Applications University of Alabama, Huntsville, Storrs, Storrs, CT; R. Budica, Self, M. Rodriguez, J. Cassibry, University of A. Chap, R. Sedwick, University of A. Chap, University of Maryland, College Huntsville, AL Huntington Beach, CA; L. Johnson, NASA Alabama, Huntsville, Huntsville, AL Maryland, College Park, College Park, MD Park, College Park, MD; J. Scott, NASA Marshall Space Flight Center, Huntsville, Johnson Space Center, Houston, TX; A. AL; T. Kammash, University of Michigan, Tarditi, Electric Power Research Institute, Ann Arbor, Ann Arbor, MI Inc., Knoxville, TN; J. Wolinski, NASA Johnson Space Center, Houston, TX Monday, 27 July 2015 47-PAW-2 Nozzle Section II Lake Concord B Chaired by: J. SOKHEY, Rolls-Royce Corp and M. CHRISTIANSEN, Aero Systems Engineering 1500 hrs 1530 hrs 1600 hrs 1630 - 1730 hrs Oral Presentation AIAA-2015-3862 Oral Presentation Open Discussion Modeling Empirical Test Data with BCFD Analysis for the 2nd A Comparative CFD Study on the CFD++ on an Axisymmetric 25 AIAA Propulsion Aerodynamics Effect of Varying Nozzle Fan to Degree Conical Nozzle Workshop: Nozzle Results Core Total Pressure Ratio on the S. Podleski, Innovative Engineering C. Winkler, The Boeing Company, DSFR Nozzle Solutions, Mukilteo, WA; N. Woo, Hazelwood, MO M. Christiansen, K. Mikkelsen, Aero University Preparatory Academy, Seattle, Systems Engineering, St. Paul, MN WA; S. Tu, Ingraham High School, Seattle, WA Monday, 27 July 2015 48-PC-3 Spray Injection and Combustion Lake Louise Chaired by: K. MCMANUS, GE Global Research Center and J. GORE, Purdue University 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3863 AIAA-2015-3864 AIAA-2015-3865 AIAA-2015-3866 Impinging Jet Spray Formation Experimental Study of a Heated Effect of Orifice Shape on Effects of Droplets on an Using Viscoelastic Liquids Liquid Jet in a Crossflow Cavitation-Induced Injection Exothermic Reacting Supersonic N. Rodrigues, Purdue University, West H. Wiest, S. Heister, Purdue University, Characteristics of High-Temperature Shear Flow Lafayette, IN; J. Mallory, Western New West Lafayette, IN Aviation Fuel Z. Ren, Tsinghua University, Beijing, China England University, Springfield, MA; P. H. Lee, Y. Jin, H. Choi, K. Hwang, Agency

49 Sojka, Purdue University, West Lafayette, for Defense Development, Daejeon, Korea IN (the Republic of) Monday, 27 July 2015 49-PC-4 Propellants and Fuels I Lake Virginia Chaired by: T. JACKSON, University of Florida Gainesville and V. RAMAN, University of Michigan 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-3867 AIAA-2015-3868 AIAA-2015-3869 AIAA-2015-3870 AIAA-2015-3871 AIAA-2015-3872 Effect of Water and Humidity on Combustion Characteristics of Enhancement of Ammonium Burning Characteristics of AP/HTPB The Effect of Iron Metal Ions and Research on NEPE Propellant Life

Hypergolic Propellant Ignition Gaseous CH4/O2 Coaxial Jets in a Perchlorate/Hydroxyl-Terminated Propellants Supplemented with Low Chelating Agents of Iron on the Prediction Model Delay Model combustor Polybutadiene Combustion Kinetics Thermal Conductivity Powders Thermal Decomposition of HAN- Y. Xiong, X. Sui, N. Wang, Beijing Institute N. Zarbo, T. Pourpoint, Purdue University, S. Choi, T. Kim, O. Kwon, Sungkyunkwan Using Ethanol-Doped Air M. Kohga, S. Shioya, National Defense Based Liquid Monopropellant of Technology, Beijing, China West Lafayette, IN University, Suwon, Korea (the Republic of) R. Gonçalves, Federal University of Academy, Yokosuka, Japan R. Amrousse, K. Hori, K. Hatai, H. Pará, Belém, Brazil; K. Iha, J. Rocco, Kagawa, H. Ikeda, Japan Aerospace Technological Institute of Aeronautics Exploration Agency (JAXA), Sagamihara, (ITA), São José dos Campos, Brazil Japan Monday, 27 July 2015 50-SR-2 Solid Rocket Motor Historical and Current Developments Lake Concord A Chaired by: M. LANGHENRY, Raytheon Missile Systems and D. POE, Aerojet Rocketdyne 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3873 AIAA-2015-3874 AIAA-2015-3875 AIAA-2015-3876 AIAA-2015-3877 Solid Rocket Motor Reliability and SLS Booster Development Orion Launch Abort System The Solid Rocket Legacy of Zefiro 40 Solid Rocket Motor: From Historical Failure Modes Review J. Redden, Alliant Techsystems, Brigham JETTISON MOTOR Performance on Thiokol’s Huntsville Division 1949- a Technological Demonstrator to T. Sojourner, D. Richardson, B. Allen, S. City, UT Exploration Flight Test - 1 1996 Vega Evolution Flight Stage Hyde, S. McHenry, B. Goldberg, ATK, R. McCauley, NASA Marshall Space Flight T. Moore, Defense Systems Information A. Neri, ESA, Frascati, Italy Brigham City, UT; et al. Center, Huntsville, AL; J. Davidson, G. Analysis Center, Belcamp, MD Gonzalez, NASA Langley Research Center, Hampton, VA Monday, 27 July 2015 51-TM-2 Heat Transfer and Transport Modeling and Analysis II Lake Down A Chaired by: M. CHOI, NASA-Goddard Space Flight Center and C. TARAU, Advanced Cooling Technologies 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3878 AIAA-2015-3879 AIAA-2015-3880 AIAA-2015-3881 AIAA-2015-3882 Analyses of Thermal Comfort Numerical Study of the Heat Numerical Study of Convective Hypersonic Flow Analysis of Implicit Solution of One- and Indoor Air Quality under Transfer and Friction Performance Heat Transfer of Aviation Kerosene Re-entry Vehicles Using Three Dimensional Transient Ablation Stratum, Displacement and Mixing in Channels with a Supercritical with Consideration of Fuel Pyrolysis Dimensional Navier-Stokes O. Onay, S. Eyi, Middle East Technical Ventilation Systems Fluid and Coking at Supercritical Equations University, Ankara, Turkey A. ElHaroun, E. Khalil, A. Fahim, E. Bially, L. Tran, J. Kapat, University of Central Pressures M. Ozgun, S. Eyi, Middle East Technical Cairo University, Giza, Egypt Florida, Orlando, FL K. Xu, H. Meng, Zhejiang University, University, Ankara, Turkey

50 Hangzhou, China Monday, 27 July 2015 52-F360-2 Government Investments Enabling Advancement of In-Space Propulsion Orlando IV 1530 - 1800 hrs The competition in the global space propulsion market continues to increases as non-traditional entities develop and demonstrate space propulsion devices. In this environment, U.S. industry continues to invest in strategy, concepts, and technology to maintain a healthy share of the market beyond the delivery of government assets. Simultaneously, U.S. government agencies continue to infuse multiple programs to push the boundary of technical capabilities. The challenge is to align the focus of government-funded technology with the needs, requirements, and commercial opportunities of industry. These issues are critical for the commercial infusion and eventual sustainability of technology developed under government funding. A Panel composed of leaders within government and industry, including spacecraft operators, will discuss: The leverage of advanced in-space propulsion technology, examples of the successful infusion of government-funded technology development, and identify opportunities for government investments in-space propulsion to enable emerging markets.

Moderator: Mitchell Walker II, Georgia Institute of Technology Panelists: Roger Myers Jeff Sheehy Mark Lewis Peter Lord Jonny Dyer Aerojet-Rocketdyne NASA Headquarters IDA Science and Technology Policy Institute Space Systems Loral Google+Skybox Imaging

Monday, 27 July 2015 53-NW-5 Welcome Reception Exposition Hall 1800 - 1930 hrs Monday, 27 July 2015 54-RLA-1 How to Avoid a Career Catastrophe: Historic Aerospace Safety Lessons Orlando IV 1930 - 2100 hrs Wayne Hale Director of Human Spaceflight at Special Aerospace Services This session is intended for students and early career Aerospace Engineers. It is intended to be a dialog, illustrated with recent space flight safety issues, that explores the role that safety plays in the development and operation of space systems. And further, to show how proper attention to safety can be beneficial to a career in aerospace. Tuesday Tuesday, 28 July 2015 55-NW-6 Networking Coffee Break Ballroom Foyer 0730 - 0800 hrs Tuesday, 28 July 2015 56-SB-2 Tuesday Speakers’ Briefing In Session Room 0730 - 0800 hrs Speakers, presenters and session chairs for both the morning and afternoon technical sessions, please meet in your session room to load presentations and discuss the flow of your session. Tuesday, 28 July 2015 57-PLNRY-3 Cost and Affordability of Future Systems Panel Orange D 0800 - 0900 hrs Panelists will discuss the key issues and approaches associated with making future systems less costly and more affordable, and how to manage the balance between customer and seller needs.

51 Moderator: Michael Griffin, Chairman and CEO, Schafer Corporation Panelists: Michael Hawes Lee Monson Frank Culbertson Mark Sirangelo Vice President and Orion Program Manager, Lockheed Martin Vice President Sales - Middle East and Americas, The Boeing President Space Systems Group, Orbital ATK Corporate Vice President Space Systems, Sierra Nevada Space Systems Company Company (ret.) Corporation

Tuesday, 28 July 2015 58-ABPSI-3 Nozzles Lake Sheen A Chaired by: R. NICHOLS, The University of Alabama at Birmingham 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3883 AIAA-2015-3884 AIAA-2015-3885 AIAA-2015-3886 Initial Subscale Performance Three-dimensional Jet Acoustic Experiment-Based Modeling of An Experimental Study of Subsonic Measurements of the AIAA Dual Characterization and Geometry Flow Fields in Clustered External and Sonic Jets Controlled by Separate Flow Reference (DSFR) Optimization of Chevron Nozzles Nozzles Air-Tabs Nozzle S. Mani, D. Lee, Korea Advanced Institute T. Isono, Tohoku University, Sendai, A. Perumal, Amrita University, Coimbatore, K. Mikkelsen, D. Myren, D. Dahl, M. of Science and Technology, Yuseong-gu, Japan; S. Tomioka, N. Sakuranaka, Japan India; S. Verma, National Aerospace Christiansen, Aero Systems Engineering, Korea (the Republic of); V. Sanal Kumar, Aerospace Exploration Agency (JAXA), Laboratories, Bangalore, India; E. Inc., Plymouth, MN Kumaraguru College of Technology, Kakuda, Japan Rathakrishnan, Indian Institute of Coimbatore, India Technology Kanpur, Kanpur, India Tuesday, 28 July 2015 59-AEP-1 Aircraft Electric/Hybrid Propulsion Orange E Chaired by: R. SCHARNHORST, Boeing Defense, Space & Security 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3887 AIAA-2015-3888 AIAA-2015-3889 AIAA-2015-3890 AIAA-2015-3891 A Parametric Environment for Investigation of FC/GT Hybrid Core Electric-Powered Commercial Turboelectric Aircraft Drive Key Electric Motors for Non-Cryogenic Weight and Sizing Prediction in Electrical Propulsion for Fan Aircraft Feasibility Performance Parameters and Hybrid Electric Propulsion of Motor/Generator for Hybrid Aircraft D. Aktas, University of Tennessee Space Functional Requirements K. Duffy, University of Toledo, Toledo, OH Electric Propulsion K. Okai, T. Himeno, T. Watanabe, Institute, Tullahoma, TN R. Jansen, G. Brown, J. Felder, NASA Y. Miyairi, C. Perullo, D. Mavris, Georgia University of Tokyo, Tokyo, Japan; H. Glenn Research Center, Cleveland, OH; K. Institute of Technology, Atlanta, GA Nomura, Nihon University, Narashino, Duffy, University of Toledo, Toledo, OH Japan; T. Tagashira, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Tuesday, 28 July 2015 60-APC-1 Advanced Space Transportation Concepts Lake Highland A Chaired by: E. ZAPATA, NASA-Kennedy Space Center and J. ROBINSON, Retired f/Boeing 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3892 AIAA-2015-3893 AIAA-2015-3894 AIAA-2015-3895 Roadmap for Long Term Multi-purpose Space Tug Vehicle Sub-Orbital Passenger Aircraft for Solar Sail Propulsion for Sustainable Space Exploration J. Robinson, Propellant Supply Technology, Space Launch Operations Interplanetary Cubesats and Habitation - Defining the Seal Beach, CA; R. Rhodes, NASA Kennedy D. Thorpe, D. Escher, R. Rhodes, Space L. Johnson, A. Sobey, K. Sykes, NASA Functional Requirements for Early Space Center, Cape Canaveral, FL Propulsion Synergy Team, Washington, DC Marshall Space Flight Center, Huntsville, Phase of Space Habitation AL 52 R. Rhodes, NASA Kennedy Space Center, Cape Canaveral, FL; E. Henderson, NASA Johnson Space Center, Houston, TX; J. Robinson, Propellant Supply Technology, Huntington Beach, CA Tuesday, 28 July 2015 61-APS-2 Space Solar Power System Architectures and Concepts / Solar Electric Propulsion Power Management and Distribution Lake Highland B Chaired by: M. HUGHES, Lockheed Martin Corporation and A. BAISDEN, The Johns Hopkins University Applied Physics Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3896 AIAA-2015-3897 AIAA-2015-3898 AIAA-2015-3899 AIAA-2015-3900 AIAA-2015-3901 Lightweight Integrated Solar Array Utilizing a Solar Panel Array On Orbit Measurement of Next Advanced Concept of the Space High Input Voltage, Silicon Carbide Modular Power Systems for (LISA): Providing Higher Power to Architecture to Support Work on Generation Space Solar Cell Electric Power System Integrated (SiC) Power Processing Unit Aerospace Vehicles Small Spacecraft Space Solar Power Technology on the International with the Propulsion Performance Demonstration G. Semrau, S. Steffan, Moog, East C. Johnson, J. Carr, L. Fabisinski, T. B. Kading, J. Straub, University of North Space Station S. Okaya, Japan Aerospace Exploration K. Bozak, L. Pinero, R. Scheidegger, Aurora, NY Russell, L. Smith, NASA Marshall Space Dakota, Grand Forks, Grand Forks, ND D. Wolford, M. Myers, N. Prokop, M. Agency (JAXA), Sagamihara, Japan M. Aulisio, M. Gonzalez, NASA Glenn Flight Center, Huntsville, AL Krasowski, NASA Glenn Research Center, Research Center, Cleveland, OH; A. Cleveland, OH; D. Parker, J. Cassidy, Birchenough, Vantage Partners, LLC, Lockheed Martin Corporation, Greenbelt, Cleveland, OH MD; et al. Tuesday, 28 July 2015 62-ECD-2 Stirling Components Lake Lucerne Chaired by: L. MASON, NASA Glenn Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3902 AIAA-2015-3903 AIAA-2015-3904 AIAA-2015-3905 AIAA-2015-3906 Optimization of the Appendix Gap Design, Qualification and Evaluation and Validation of Overview of Stirling Technology Pressure Loss Predictions of the Design in Stirling Cycle Machines Integration Testing of the Organic Materials for Advanced Research at NASA Glenn Research Reactor Simulator Subsystem at J. Pfeiffer, H. Kuehl, Technical University of High-Temperature Resistance Stirling Convertors (ASCs): Center NASA GRC Dortmund, Dortmund, Germany Temperature Device for Stirling Overview S. Wilson, NASA Glenn Research Center, T. Reid, NASA Glenn Research Center, Power System E. Shin, Ohio Aerospace Institute, Cleveland, OH Cleveland, OH T. Chan, R. Elisii, D. Hill, J. White, Cleveland, OH Lockheed Martin Corporation, King of Prussia, PA; E. Lewandowski, S. Oriti, NASA Glenn Research Center, Cleveland, OH Tuesday, 28 July 2015 63-ECS-2 Energetic Applications, Technology & Education Lake Nona B Chaired by: S. GOLDSTEIN, The Aerospace Corporation and H. LEE, Chemring Energetic Devices 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3907 AIAA-2015-3908 AIAA-2015-3909 AIAA-2015-3910 AIAA-2015-3911 Comparison of BPN Igniter Gains Provided by Opto-pyro Combustion Performance 2015 CAD/PAD Technology Educational Preparation for Compositions Containing Micron- Technology in Terms of Safety on Improvement of Energetic Thin Roadmap Update a Career in CAD/PAD Related and Nano-Sized Boron Particles Launchers Films Using Carbon Nanotubes J. Burchett, T. Blachowski, Naval Surface Industries 53 S. Koc, ROKETSAN Missile Industries, B. Chamayou, Airbus, Les Mureaux, France K. Kappagantula, Ohio University, Athens, Warfare Center, Indian Head, MD J. Burchett, Naval Surface Warfare Center, Inc., Ankara, Turkey; A. Ulas, Middle East OH; J. Cano, M. Pantoya, Texas Tech Indian Head, MD; J. Baglini, Exodynamics Technical University, Ankara, Turkey University, Lubbock, TX Technology, Inc., Phoenix, AZ Tuesday, 28 July 2015 64-EE-3 Fuel Cells, Energy Storage, and Combustion Lake Down B Chaired by: J. MALLORY and F. ZHANG 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3912 AIAA-2015-3913 AIAA-2015-3914 AIAA-2015-3915 AIAA-2015-3916 AIAA-2015-3917 Effect of Polyelectrolyte Multilayer High-speed and Micro-scale Investigation of Titanium Felt Modeling of Interfacial Resistance Impact of Oxygen Enrichment Combustion Characteristics of Fabrication Method on Conductance Measurements of Flow and Transport Parameters for Energy Effects on the Performance and on the Performance of Heat- Ammonia as a Renewable Energy for Fuel Cell Applications Reaction Dynamics for Sustainable Storage and Hydrogen/Oxygen Efficiency for Electrolyzer Energy Recirculating Micro-Scale Source and Development of J. Mallory, M. Roberts, Western New Energy Storage Production Storage Combustors Reduced Chemical Mechanisms England University, Springfield, MA J. Mo, S. Steen, F. Zhang, University of S. Steen, J. Mo, F. Zhang, University of B. Han, S. Steen, J. Mo, F. Zhang, P. Yelvington, C. Rodriguez, T. Lasko, H. Nozari, A. Karabeyoglu, KOC University, Tennessee Space Institute, Tullahoma, TN Tennessee Space Institute, Tullahoma, TN University of Tennessee Space Institute, Mainstream Engineering Corporation, Istanbul, Turkey Tullahoma, TN Rockledge, FL; B. Wise, C. Holicker, D. Kirk, Florida Institute of Technology, Melbourne, FL Tuesday, 28 July 2015 65-EP-5 Near-Term Higher Power Systems and Application Lake Mizell A Chaired by: J. WALKER and T. SWANSON, AEDC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3921 AIAA-2015-3919 AIAA-2015-3920 AIAA-2015-3922 AIAA-2015-3918 AIAA-2015-4122 Development of High-Power Hall Near-Surface Plasma Non-Contact Thermal Impact of the Magnetic Barrier Advancements in the Numerical Sudies on Plasma Plume Thruster Power Processing Units at Characterization of the 12.5-kW Characterization of NASA’s 12.5-kW Extent on the Performance of a Demonstration of High Thrust to Flows with a Hybrid Method NASA GRC NASA TDU1 Hall Thruster Hall Thruster Krypton-fuelled Hall Thruster Power Ion Thruster Technology C. Cai, New Mexico State University, Las L. Pinero, R. Scheidegger, K. Bozak, NASA R. Shastry, W. Huang, H. Kamhawi, NASA W. Huang, H. Kamhawi, J. Myers, J. Yim, J. Vaudolon, S. Mazouffre, National Center R. Thomas, M. Patterson, NASA Glenn Cruces, NM Glenn Research Center, Cleveland, OH; Glenn Research Center, Cleveland, OH NASA Glenn Research Center, Cleveland, for Scientific Research (CNRS), Orléans, Research Center, Cleveland, OH; M. A. Birchenough, Vantage Partners, LLC, OH; G. Neff, Western Michigan University, France Crofton, J. Young, The Aerospace Cleveland, OH Kalamazoo, MI Corporation, El Segundo, CA; J. Foster, University of Michigan, Ann Arbor, Ann Arbor, MI Tuesday, 28 July 2015 66-EP-6 Resistojets and Arcjets Lake Mizell B Chaired by: J. POLK, Jet Propulsion Laboratory and M. FELDMAN, Princeton University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3923 AIAA-2015-3924 AIAA-2015-3925 AIAA-2015-3926 AIAA-2015-4011 Numerical Optimization of Micro- Performance Characterization of Overcoming Low Nozzle Efficiency: Evaluation of Plasma Properties Electrospray of an Energetic Ionic Nozzle Geomoetries for Low a Low Reynolds Number Micro- A Test-Correlated Numerical in a Microwave Electrothermal Liquid Monopropellant for Multi- Reynolds Number Resisto-Jets Nozzle Flo Investigation of Low Reynolds Thruster Resonant Cavity by Using Mode Micropropulsion Applications T. Holman, M. Osborn, Naval Research L. Williams, Praxis, Inc., Alexandria, VA; Number Micro-Nozzle Flow Two Fluid Global Model S. Berg, J. Rovey, Missouri University of

54 Laboratory, Washington, DC M. McDonald, M. Osborn, Naval Research M. Osborn, T. Holman, D. Rosenberg, M. Yildiz, Turkish Air Force Academy, Science and Technology, Rolla, MO; B. Laboratory, Washington, DC S. Tuttle, Naval Research Laboratory, Istanbul, Turkey; M. Celik, Bogazici Prince, S. Miller, R. Bemish, Air Force Washington, DC; L. Williams, Praxis, Inc., University, Istanbul, Turkey Research Laboratory, Kirtland AFB, NM Alexandria, VA Tuesday, 28 July 2015 67-GTE-4 Turbine II Lake Monroe Chaired by: M. RICKLICK, Embry Riddle Aeronautical University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3927 AIAA-2015-3928 AIAA-2015-3929 AIAA-2015-3930 Numerical Benchmark of Heat Comparison of Computational Aeroacoustics of Flow over One-Dimensional Assessment of Transfer and Friction in Pipes with and Experimental Results for a Rectangular Cavities Supersonic Inlet Turbines Roughness Transonic Variable-speed Power- B. Kutlu, University of Central Florida, J. Sousa, von Kármán Institute for Fluid L. Tran, Z. Little, P. Tran, J. Kapat, turbine Blade Operating with Low Orlando, FL; B. Saracoglu, G. Paniagua, Dynamics, Rhode-Saint-Genèse, Belgium; University of Central Florida, Orlando, FL Inlet Turbulence Levels von Kármán Institute for Fluid Dynamics, G. Paniagua, Purdue University, West D. Booth, Army Research Laboratory, Rhode-Saint-Genèse, Belgium; J. Kapat, Lafayette, IN Aberdeen Proving Ground, MD; A. Flegel, University of Central Florida, Orlando, FL NASA Glenn Research Center, Cleveland, OH Tuesday, 28 July 2015 68-GTE-5 Compressors II Lake Florence Chaired by: K. AHMED 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3931 AIAA-2015-3932 AIAA-2015-3933 AIAA-2015-3934 AIAA-2015-3935 AIAA-2015-3936 Three-dimensional Inverse Design Simulation of Stall Inception of a A Novel Concept with Self-driving Turbogas Engines Rotational Speed The Role of CFD Modeling in the Influence of a Tip Blowing Casing of Centrifugal Impeller Blade High Speed Axial Compressor with Fan for High Bypass Ratio Turbofan Estimation Using Acoustic and Development of the Counter Treatment on the Stator Flow L. Sun, J. Chen, G. Huang, Nanjing Rotor-Stator Interaction engine Vibrational Measurements Rotating Open Fan Engine A. Inzenhofer, A. Hupfer, C. Guinet, University of Aeronautics and Astronautics, J. Gan, University of Miami, Miami, FL; W. Lu, G. Huang, X. Xiang, J. Wang, R. Bertacin, F. Ponti, V. Ravaglioli, F. Jiang, R. Griffiths, B. Smith, The Boeing Technical University of Munich, Garching, Nanjing, China H. Im, Honeywell International, Inc., Nanjing University of Aeronautics and University of Bologna, Bologna, Italy Company, Huntington Beach, CA Germany; H. Schrapp, V. Gümmer, Rolls- Torrance, CA; G. Zha, University of Miami, Astronautics, Nanjing, China Royce Group plc, Blankenfelde-Mahlow, Miami, FL Germany Tuesday, 28 July 2015 69-HR-4 Design Studies Including Cost and Feasibility Analysis I Lake Sheen B Chaired by: A. KARP, Jet Propulsion Laboratory and S. COOGAN, Southwest Research Institute 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3937 AIAA-2015-3938 AIAA-2015-3939 AIAA-2015-3940 AIAA-2015-3941 AIAA-2015-3942 Design and Optimization of Hybrid Low-thrust Hybrid Motor Efficiency Investigation of Flight Profiles Throttled Launch-Assist Hybrid Concept and Design of the Hybrid Structural Performance of Large Propulsion Systems for In-Space Research for Design Optimization Suitable for Altering-Intensity Rocket Motor for an Airborne Test-motor for Development of a Scale Paraffin Wax Based Fuel Application Purposes Swirling-Oxidizer-Flow-Type Hybrid NanoSat Launch Platform Propulsive Decelerator of SARA Grains E. Toson, Technical University of Milan, O. Shynkarenko, A. Andrianov, A. Elias Rocket S. Whitmore, S. Merkley, S. Walker, Z. Re-entry Capsule K. Veale, M. Brooks, J. Pitot, University of Milan, Italy; A. Karabeyoglu, KOC de Morais Bertoldi, University of Brasilia, U. Tomoaki, T. Shimada, Japan Aerospace Spurrier, Utah State University, Logan, UT A. Andrianov, O. Shynkarenko, A. Elias KwaZulu-Natal, Durban, South Africa University, Istanbul, Turkey Brasilia, Brazil Exploration Agency (JAXA), Sagamihara, de Morais Bertoldi, M. Nascimento Dias

55 Japan Barcelos Junior, University of Brasilia, Brasilia, Brazil; C. Alberto Gurgel Veras, Brazilian Space Agency (AEB), Brasilia, Brazil Tuesday, 28 July 2015 70-HSABP-3 Design and Development of Innovative High-Speed Air Breathing System Lake George A Chaired by: D. MUSIELAK, University of Texas at Arlington and J. FULTON 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3943 AIAA-2015-3944 AIAA-2015-3945 AIAA-2015-3946 AIAA-2015-3947 Propulsion Efficiency Considerations Influence Factor Analysis of Numerical Investigation of 3D Flow Visualization and Passive Optical Combustion Sensors for Combined Cycle Propulsion Performance Parameter for a the Injection Scheme for One Geometry Optimization of Cavity for Scramjet Engine Control Systems Strut/Cavity Supersonic Combustor Rectangular RBCC Engine at based Scramjet Combustors using D. Micka, D. Knaus, Creare, LLC, Hanover, J. Bossard, BSRD, LLC, Huntsville, AL C. Zhang, J. Chang, W. Shi, W. Bao, Scramjet-Mode k-ω Model NH; J. Temme, J. Driscoll, University of Harbin Institute of Technology, Harbin, S. Zhang, J. Li, F. Qin, X. Wei, J. Ye, S. Mani, V. Sanal Kumar, Kumaraguru Michigan, Ann Arbor, Ann Arbor, MI China X. Tang, Northwestern Polytechnical College of Technology, Coimbatore, India University, Xi’an, China Tuesday, 28 July 2015 71-ITAR-1 Air Breathing Propulsion Systems: Nozzles and Diffusers Orlando VI Chaired by: P. SMITH, The Boeing Company 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3948 AIAA-2015-3949 AIAA-2015-3950 Swirl Measurements at the Exit of a Aeroacoustic Validation of a Aeroacoustic Experiments on Serpentine Diffuser Simulation for a Rectangular Supersonic Multi-aperture Nozzles C. Nessler, W. Copenhaver, M. List, C. Ruscher, S. Gogineni, Spectral Energies, A. Magstadt, M. Berry, P. Shea, M. Air Force Research Laboratory, Wright- LLC, Beaver Creek, OH; K. Viswanath, Glauser, Syracuse University, Syracuse, NY; Patterson AFB, OH Naval Research Laboratory, Washington, C. Ruscher, S. Gogineni, Spectral Energies, DC; B. Kiel, Air Force Research Laboratory, LLC, Dayton, OH; et al. Wright-Patterson AFB, OH; M. Berry, A. Magstadt, Syracuse University, Syracuse, NY; et al. Tuesday, 28 July 2015 72-LP-10 Spacecraft Propulsion Systems I Orange F Chaired by: P. ALLIOT, Snecma S.A. and H. KAGAWA, JAXA 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3951 AIAA-2015-3952 AIAA-2015-3953 AIAA-2015-3954 AIAA-2015-3955 The Integration and Testing of A Discussion of Two Challenges of Service Life Extension of the ISS NASA Propulsion Sub-System Lessons from the AEHF-1 Four Propulsion Systems for the Non-cooperative Satellite Refueling Propulsion System Elements Concept Studies and Risk Reduction Bipropellant Maneuver Anomaly Magnetospheric MultiScale (MMS) G. Coll, NASA Glenn Research Center, U. Kamath, G. Grant, The Boeing Activities for Resource Prospector with Recurring Themes Mission Greenbelt, MD; B. Nufer, T. Aranyos, M. Company, Houston, TX; S. Kuznetsov, S. Lander M. Mueller, The Aerospace Corporation, El 56 E. Cardiff, NASA Goddard Space Flight Kandula, D. Tomasic, NASA Kennedy Shaevich, Khrunichev State Research and H. Trinh, NASA Marshall Space Flight Segundo, CA Center, Greenbelt, MD Space Center, Cape Canaveral, FL Production Space Center, Moscow, Russia; Center, Huntsville, AL V. Spencer, NASA Johnson Space Center, Houston, TX Tuesday, 28 July 2015 73-LP-11 Liquid Propulsion History: Lessons Learned from Canceled Programs Lake Eola 0900 - 1200 hrs Chaired by: K. PUGMIRE, Spincraft and B. AUSTIN, IN Space LLC Propulsion elements/systems of note associated with programs which were cancelled or postponed. Presentations include propulsion description and discussion of pros/cons. An interactive forum, moderator with topic presenters.

Moderator: Dan Dumbacher, Purdue University Panelists: DC-X/XA Delta Clipper X-34 Fastrac RS-88 Bantam X-33 Linear Aerospike ISS Electrothermal Engine 1. “Stories of Pushing the Limits” by Dan 1. “Review and Lessons Learned from the Approach 1. “System Technology, Program and Derivatives” 1.”Aerospike Engine” by Steve Bouley Aerojet “Supplemental Reboost System” Briefing, T Kent Dumbacher, Purdue to Program Management and System Engineering” by John Vilja. Aerojet Rocketdyne Rocketdyne Pugmire 2. “Morpheus Lander” by Jon Olansen, NASA JSC by Mark Fisher, Schafer Corp. 2. CST-100 Launch Escape System” by Joaquin 2. “Theoretical Evaluation and Briefing of Joint 2. “Technical Implications of Programmatic Castro, Aerojet Rocketdyne. Academic/Industry Flight Test” by Eric Besnard, Decisions” by Mary Beth Koelbl (presenting) and CSU Katherine Van Hooser, NASA MSFC Tuesday, 28 July 2015 74-NFF-3 Nuclear Thermal Propulsion: Missions, Vehicles and Architectures Lake Nona A Chaired by: S. BOROWSKI, NASA Glenn Research Center and G. WILLIAMS, Ohio Aerospace Institute 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3956 AIAA-2015-3957 AIAA-2015-3958 Determining Mars Mission NTP Cryogenic Fluid Management The Nuclear Thermal Turbo Rocket Thrust Size and Architecture Impact Technology Development for - A Conceptual High-Performance for Mission Options Nuclear Thermal Propulsion Earth-to-Orbit Propulsion System C. Joyner, D. Levack, J. Crowley, Aerojet B. Taylor, NASA Marshall Space Flight J. Bucknell, Self, Royal Oak, MI Rocketdyne, Sacramento, CA Center, Huntsville, AL; J. Caffrey, Oregon State University, Corvallis, OR; A. Hedayat, J. Stephens, R. Polsgrove, NASA Marshall Space Flight Center, Huntsville, AL Tuesday, 28 July 2015 75-NW-7 Networking Coffee Break Exposition Hall 0900 - 0930 hrs Tuesday, 28 July 2015 76-PAW-3 S-Duct Inlet Section Lake Concord B Chaired by: C. CHUCK, Boeing Commercial Airplanes; A. DELOT, ONERA and L. GEA, Boeing Engineering Operations & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3959 AIAA-2015-3960 AIAA-2015-3961 AIAA-2015-3962 AIAA-2015-3963 AIAA-2015-3964 BCFD Simulations of the 2nd AIAA CFD Simulation of Serpentine Perspectives on Propulsion CFD Grid Topology Study of the S-duct Simulation of an S-Duct Inlet Using Computational and Experimental

57 Propulsion and Aerodynamics S-Duct with Flow Control for Inlet Applications Relevant to Inlet with Vortex Generators the Lattice-Boltzmann Method Results for Flows in a Diffusing Workshop: S-Duct with Vortex L. Gea, The boeing Company, Huntington the AIAA Propulsion Aerodynamics A. Batista de Jesus, L. Trapp, D. Abreu, A. S. Noelting, S. Gautier, M. Wessels, Exa S-Duct without and with Flow Generators Beach, CA Workshop Lombardi, L. Tobaldini, Embraer S.A, São GmbH, Stuttgart, Germany; I. Gonzalez, Control Devices D. Babcock, M. Mani, The Boeing N. Domel, Lockheed Martin Aeronautics José dos Campos, SP, Brazil Euroxa, Paris, France A. Delot, ONERA, Meudon, France; R. Company, Hazelwood, MO Company, Fort Worth, TX Scharnhorst, The Boeing Company, Hazelwood, MO Tuesday, 28 July 2015 77-PC-5 Modeling of Combustion Dynamics, Instabilities and Noise I Lake Louise Chaired by: C. CADOU, University of Maryland 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3965 AIAA-2015-3966 AIAA-2015-3967 AIAA-2015-3968 AIAA-2015-3969 AIAA-2015-3970 Numerical Simulations of Screech A complex Network Approach to Intermittency in Combustion Large Eddy Simulation of Self- Multifractal Characterization of Direct Simulation of the Instability E. Gonzalez, Combustion Science and Investigate Combustion Dynamics dynamics Excited Combustion Dynamics in a Combustion Dynamics of the Pilot Flame in a Turboengine Engineering, Inc., Columbia, MD M. Murugesan, R. Sujith, Indian Institute M. Murugesan, R. Sujith, Indian Institute Bluff-Body Combustor V. Unni, R. Sujith, Indian Institute of Combustor of Technology Madras, Chennai, India of Technology Madras, Chennai, India F. Ma, W. Proscia, Pratt & Whitney, East Technology Madras, Chennai, India Y. Obikane, Nagaoka University of Hartford, CT; V. Ivanov, F. Montanari, Technology, Nagaoka, Japan; K. Lochin, ANSYS, Inc., Lebanon, NH Mongolia University of Science and Technology, Ulaanbaatar, Mongolia Tuesday, 28 July 2015 78-PC-6 Propellants and Fuels II Lake Virginia Chaired by: B. CHEHROUDI, European Research Council (ERC) and J. MURPHY, The Aerospace Corporation 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3971 AIAA-2015-3972 AIAA-2015-3973 Material Compatibility and Multi-Injector Impinging Jet Studies Aging Effects of Composite AP/ Aging Testing for HAN-Based of Ignition Delay for Hydrogen HTPB Propellants Containing Nano- Monopropellants Peroxide and Gelled Hydrocarbon Sized Additives K. Gaworski, Digital Solid State Propulsion, Fuel Containing Reactive or T. Sammet, A. Demko, C. Dillier, E. LLC, Reno, NV; J. Moore, Moog, Niagara Catalytic Particles Petersen, Texas A&M University, College Falls, NY; T. Manship, M. McPherson, S. T. Connell, G. Risha, R. Yetter, Station, TX Williams, Digital Solid State Propulsion, Pennsylvania State University, State LLC, Reno, NV College, PA; B. Natan, Technion--Israel Institute of Technology, Haifa, Israel Tuesday, 28 July 2015 79-SR-3 Solid Rocket Motor Combustion Flow Fields and Instability II Lake Concord A Chaired by: J. SPURLING, Naval Air Warfare Center Weapons Division and E. CAVALLINI, University of Roma “La Sapienza” 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3974 AIAA-2015-3975 AIAA-2015-3976 AIAA-2015-3977 Vortex-Sound Generation and Q1D Modelling of Vortex-Driven Using a Semi-Infinite Tube to Experimental Study on Combustion Thrust Unsteadiness in Aft-Finocyl Pressure Oscillations in Aft-Finocyl Measure Pressure Oscillations in of Aluminum in Composite Solid Rocket Motor SRMs with Submersed Nozzle Solid Rocket Motors Propellant A. Di Mascio, Centro Nazionale delle Cavity J. Spurling, Naval Air Warfare Center, X. Liu, P. Liu, B. Jin, Northwestern 58 Ricerche, Rome, Italy; E. Cavallini, B. E. Cavallini, B. Favini, University of Rome China Lake, CA Polytechnical University, Xi’an, China Favini, University of Rome “La Sapienza”, “La Sapienza”, Rome, Italy; A. Neri, ESA, Rome, Italy; A. Neri, ESA, Rome, Italy Rome, Italy Tuesday, 28 July 2015 80-ST-2 Space Transportation II Lake George B Chaired by: M. SIR, Aerospace Corp (COMP) 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3978 AIAA-2015-3979 AIAA-2015-3980 Modelling Thermochemical Assessment of Aerospike Nozzle for Conceptual Design of a Two Stage Nonequilibrium during Atmospheric Single-Stage to Orbit Flight Runway based Space Launch Re-Entry E. Lash, T. Moeller, University of Tennessee System T. Piskin, S. Eyi, Middle East Technical Space Institute, Tullahoma, TN A. Renganathan, D. Mavris, Georgia University, Ankara, Turkey Institute of Technology, Atlanta, GA Tuesday, 28 July 2015 81-TM-3 Thermal System Applications and Unique Environments I Lake Down A Chaired by: C. TARAU, Advanced Cooling Technologies and M. CHOI, NASA-Goddard Space Flight Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3981 AIAA-2015-3982 AIAA-2015-3983 AIAA-2015-3984 AIAA-2015-3985 AIAA-2015-3986 Thermal Performance Comparison Water-Titanium Heat Pipes for Optimized Heat Pipe Backup Paraffin Phase Change Material for Low-Cost Radiator for Fission Power Optimized Undergraduate Thermal Between Water-Copper and Water- Spacecraft Fission Power Cooling System Tested with a Maintaining Temperature Stability Thermal Control Analysis of Cube Satellites Stainless Steel Heat Pipes W. Anderson, R. Hay, Advanced Cooling Stirling Convertor of IceCube Type of CubeSats in LEO C. Tarau, T. Maxwell, W. Anderson, R. Oliver, U.S. Military Academy, West D. Silva, E. Marcelino, R. Riehl, National Technologies, Inc., Lancaster, PA C. Schwendeman, C. Tarau, Advanced M. Choi, NASA Goddard Space Flight Advanced Cooling Technologies, Inc., Point, NY; B. Crawford, Quinnipiac, Institute for Space Research (INPE), São Cooling Technologies, Inc., Lancaster, PA; Center, Greenbelt, MD Lancaster, PA Hamden, CT; G. Burrow, U.S. Military José dos Campos, Brazil N. Schifer, NASA Glenn Research Center, Academy, West Point, NY Cleveland, OH; W. Anderson, Advanced Cooling Technologies, Inc., Lancaster, PA Tuesday, 28 July 2015 82-F360-3 Evolution of our National Ground Test Capability Orlando IV 0930 - 1200 hrs As budgets continue to tighten, ground test infrastructure is a common area to look for savings. This session aims to explore how organizations balance operation and maintenance of test facilities against budget reality to accomplish their missions. Key questions that will be explored include: What are the primary factors and metrics influencing sustainability of ground test infrastructure? Is there a general tendency for programs to treat facilities as commodities, and how does this impact our ability to retain national assets? How is our maturing computational capability influencing testing? It has long been the expectation that computational analysis might replace test; are we on the verge of seeing this goal realized or are we reaching a co-dependent steady state between test and computations? Has the industry’s technical risk posture changed as a result of flat to shrinking budgets and the present balance between computations and test?

Moderator: Dave Schuster, NASA Langley Research Center Panelists: 59 Roger Simpson Michael Mastaler Doug Garrard Michael Horton Michael McWithey NASA Stennis Space Flight Center NASA Headquarters Aerospace Testing Alliance CUBRC Lockheed Martin Corporation

Tuesday, 28 July 2015 83-NW-8 Box Lunch with the Exhibitors Exposition Hall 1200 - 1300 hrs Tuesday, 28 July 2015 84-PLNRY-4 Technology Development and Trends in Propulsion and Energy Panel Orange D 1300 - 1430 hrs Panelists will discuss the major technology challenges and opportunities that will shape the future of propulsion and energy, and how those challenges and opportunities should be addressed.

Moderator: Graham Warwick, Managing Editor, Technology, Aviation Week & Space Technology Panelists: Jean Botti Tom Williams Neil Garrigan Doug Juul Chief Technical Officer Airbus Group Director Propulsion Systems Department, Marshall Space Flight Executive Manger, Energy Systems and Technology, GE Aviation Manger, Systems and Technology, GE Aviation Center

Tuesday, 28 July 2015 85-NW-9 Ice Cream Networking Break Exposition Hall 1400 - 1430 hrs Tuesday, 28 July 2015 86-AEC-1 Advanced Engine Controls & Intelligent Systems Lake Concord B Chaired by: A. BEHBAHANI, Air Force Research Laboratory and R. MILLAR, Naval Postgraduate School 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3987 AIAA-2015-3988 AIAA-2015-3989 AIAA-2015-3990 AIAA-2015-3991 AIAA-2015-3992 Investigation of Asymmetric Thrust Reduced Order Modeling of Demonstration of Smart, Framework for Distributed Engine Enhanced Engine Performance HMS Developments for the Rocket Detection with Demonstration in a Compressible Flows with Unsteady High-Temperature Pressure Control System for Sampled-data During Emergency Operation Using Engine Demonstrator Mascotte Real-Time Simulation Testbed Normal Shock Motion Sensors in an Engine Harsh Systems with Uncertain Time- a Model-Based Engine Control A. Iannetti, S. Palerm, French Space A. Chicatelli, A. Rinehart, Vantage C. Marley, K. Duraisamy, J. Driscoll, EnvironmentDemonstration of varying Sampling Intervals and Architecture Agency (CNES), Paris, France; J. Marzat, Partners, LLC, Brook Park, OH; D. Simon, University of Michigan, Ann Arbor, Ann Smart, High-Temperature Pressure Delays with State Estimations J. Csank, J. Connolly, NASA Glenn H. Piet-Lahanier, G. Ordonneau, ONERA, NASA Glenn Research Center, Cleveland, Arbor, MI Sensors in an Engine Harsh R. Yedavalli, Ohio State University, Research Center, Cleveland, OH Palaiseau, France OH; T. Sowers, Vantage Partners, LLC, Environment Columbus, OH; S. Zein-Sabatto, Tennessee Brook Park, OH M. Usrey, B. Knowles, A. Brand, K. Harsh, State University, Nashville, TN; A. Sporian Microsystems, Inc., Lafayette, Behbahani, Air Force Research Laboratory, CO; A. Behbahani, Air Force Research Wright-Patterson AFB, OH Laboratory, Wright-Patterson AFB, OH Tuesday, 28 July 2015 87-APC-2 Advanced Propulsion Concepts Lake Nona B Chaired by: A. REISZ, Reisz Engineers and J. ROBINSON, Retired f/Boeing 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3993 AIAA-2015-3994 AIAA-2015-3995 AIAA-2015-3996 Oral Presentation Film-Evaporation MEMS Tunable Possible Solution for USAF Materiel Aerospace Vehicle Propulsion Shocked Flow Ionization: an Metal/N2O Powder Rocket Array for Low-Mass SmallSat Command Requirement for a 75 System Utilizing Enclosed Vortex Experimental Study Engine-a New Concept for 60 Propulsion: Design Improvements Ton Payload .8 Mach Cruise Global Pressure Gradients P. Vorobieff, University of New Mexico, Controlled Thrust and Thrust Characterization Freighter with Un-refueled Round V. Howard, Northwest Aerospace Systems, Albuquerque, Albuquerque, NM; C. Z. Deng, C. Hu, Northwestern Polytechnical A. Cofer, W. O’Neill, S. Heister, A. the World Range Klamath Falls, OR Davidson, Dark Sea Industries, LLC, University, Xi’an, China Alexeenko, Purdue University, West R. Johnston, KGRS, Inc., Ashland, KY Albuquerque, NM Lafayette, IN; E. Cardiff, NASA Goddard Space Flight Center, Greenbelt, MD Tuesday, 28 July 2015 88-ECD-3 Dual Use Technology: Challenges and Opportunities Lake Eola 1430 - 1800 hrs Dual-use technology is a term that generally is considered applicable to both military and civilian use. For this panel though, we are broadening the definition of dual use and will be exploring the challenges and opportunities of applying technologies across different markets, whether aerospace or terrestrial, military or commercial. The panel will consider: How can you take a technology that is successful in one market and make the leap to another market? What does it take to successfully spinoff a space or military technology to a commercial application? Or how do you spin-in a technology? Panelists from government and industry will provide case studies of technologies that have been applied to different markets, providing insights into what works and how to be successful. We will then open the floor to questions and discussion with the audience.

Moderators: Edward Lewandowski (NASA Glenn Research Center) and Thomas Sutliff (NASA Glenn Research Center) Panelists: Terry Hendricks, Ph.D., P.E. Danny Micka, Ph.D. Michael Piszczor Larry Trager MMRTG Pyroshock Project Manager, NASA Jet Propulsion Engineer, Creare Deputy Chief, Photovoltaic and Electrochemical Systems Branch, Director, Advanced Power Systems, Aerojet Rocketdyne Laboratory NASA Glenn Research Center Tuesday, 28 July 2015 89-ED-2/EE-4 Systems-Level Analysis for Energy Efficiency and Renewable Energy / Electrical Components Lake Down B Chaired by: S. DUNCAN, Aerospace Systems Design Laboratory, Georgia Tech and J. DOMENECH 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-3997 AIAA-2015-3998 AIAA-2015-3999 AIAA-2015-4000 AIAA-2015-4001 AIAA-2015-4002 AIAA-2015-4003 A Systems Engineering Approach to Modeling and Simulation-based Model-based Analysis of the Impact Techniques Utilizing Meter Data to On Board Energy Management Voltage-Mode Solar Inverter with Uniform Time Division of Maximum Site Selection and an Optimization Analysis for Large Scale Campus of Adding Chilled Water Thermal Achieve Energy Savings in District Analysis Tool Active Power Factor Correction Power Tracking among Distributed Model for Sustainable Harvesting Chilled Water Networks Storage to a District Cooling System Cooling System Operations V. de Frutos, Airbus, Getafe, Spain; C. K. Siri, The Aerospace Corporation, El Power Sources of Electricity from Shallow Water M. Balchanos, J. Kim, S. Duncan, D. M. Jalaleddine, S. Duncan, D. Mavris, L. Zhang, S. Duncan, S. Oh, D. Mavris, Antequera, M. Sproesser, Airbus, Toulouse, Segundo, CA K. Siri, The Aerospace Corporation, Tidal Currents Mavris, Georgia Institute of Technology, Georgia Institute of Technology, Atlanta, Georgia Institute of Technology, Atlanta, France; F. Alcántara, L. Morant, Airbus, Torrance, CA J. Domenech, T. Eveleigh, George Atlanta, GA GA GA Getafe, Spain Washington University, Washington, DC Tuesday, 28 July 2015 90-EP-7 Hall Modeling and Cathodes Lake Mizell A Chaired by: C. MULLINS and D. MANZELLA, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-4004 AIAA-2015-4006 AIAA-2015-4008 AIAA-2015-4007 AIAA-2015-4005 AIAA-2015-4009 AIAA-2015-4010 Investigation Of The Ion Transit Plasma Perturbations in High- Numerical Simulations of the XR-5 Optimization Of Magnetic Field Non-Invasive Hall Current Hollow Cathodes for Electric Novel Microwave-Thermionic Time Instability In A Hall Thruster Speed Probing of Hall Thruster Hall Thruster For The Assessment Topology And Anode Geometry For Distribution Measurement in a Hall Propulsion Utilizing Scandate Hollow Cathode Ignition Methods Combining Time-Resolved LIF Discharge Chambers: Quantification Of Erosion Rates At Different A Wall-Less Hall thruster Effect Thruster Cathodes C. Wordingham, P. Taunay, E. Choueiri, Spectroscopy And Analytical and Mitigation Operating Conditions S. Mazouffre, J. Vaudolon, S. Tsikata, C. Mullins, R. Martinez, J. Williams, W. Ohlinger, Self, Babson Park, FL; B. Princeton University, Princeton, NJ Calculations B. Jorns, D. Goebel, R. Hofer, Jet A. Lopez Ortega, B. Jorns, I. Mikellides, R. National Center for Scientific Research Colorado State University, Fort Collins, CO; Vancil, eBeam, Inc., Beaverton, OR; J. J. Vaudolon, S. Mazouffre, National Center Propulsion Laboratory, California Institute Hofer, Jet Propulsion Laboratory, California (CNRS), Orléans, France; C. Henaux, C. Farnell, C. Farnell, Plasma Controls, Polk, Jet Propulsion Laboratory, California 61 for Scientific Research (CNRS), Orléans, of Technology, Pasadena, CA Institute of Technology, Pasadena, CA University of Toulouse, Toulouse, France; LLC, Fort Collins, CO; D. Liu, Air Force Institute of Technology, Pasadena, CA; V. France D. Harribey, National Center for Scientific Institute of Technology, Wright-Patterson Schmidt, J. Lorr, eBeam, Inc., Beaverton, Research (CNRS), Orléans, France; A. AFB, OH; et al. OR Rossi, University of Toulouse, Toulouse, France; et al. Tuesday, 28 July 2015 92-FFP-2 Fossil-Fuel Power Technologies II Lake Down A Chaired by: B. KHANDELWAL, The University of Sheffield 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-4012 AIAA-2015-4013 AIAA-2015-4014 AIAA-2015-4015 AIAA-2015-4016 AIAA-2015-4017 Blowout Limits of Partially Characteristics of Spray Flames of Comparison of Gaseous Emissions Experimental Investigation Of Investigation on Ultrasonic Fuel New Induction Manifold Designs Premixed Methyl Ester and Jet-A Palm Methyl Ester/Diesel Blends at between Jet A-1 and Severely Particle Distributions In Particle- Vaporizaiton and Oxygen Enhanced for High Performance and Low Flames an Injector Exit Equivalence Ratio Hydro-Processed Jet Fuel from Laden Coaxial Jets Combustion Cycles Emission Diesel Engine Running on K. Willingham, R. Parthasarathy, S. of 0.6 Conventional sources J. Yoon, Y. Yoon, Seoul National N. Kurisko, J. Mallory, Western New Alternative Fuels Gollahalli, University of Oklahoma, M. Richichi, R. Parthasarathy, S. Gollahalli, S. Roy, B. Khandelwal, University of University, Seoul, Korea (the Republic of) England University, Springfield, MA A. Sadeq, M. Elgergawi, M. Bassiony, S. Norman, Norman, OK University of Oklahoma, Norman, Sheffield, Sheffield, United Kingdom Ahmed, Qatar University, Doha, Qatar Norman, OK Tuesday, 28 July 2015 93-GTE-6 Combustors Lake George B Chaired by: K. AHMED 1430 hrs 1500 hrs 1530 hrs AIAA-2015-4018 AIAA-2015-4019 AIAA-2015-4020 Experimental Investigation on Determination of Combustion Combustion LES of a Multi-Burner Flame Stabilization with V Gutters Stability Margin Using the Filter Annular Aeroengine Combustor for Afterburner Applications Diagonalization Method using a Skeletal Reaction K. Parammasivam, S. Subramanian, S. A. Damiao, J. Quinlan, B. Zinn, Georgia Mechanism for Jet-A Air Mixtures Baskaran, S. Ahamed, Anna University, Institute of Technology, Atlanta, GA N. Zettervall, E. Fedina, K. Nordin-Bates, Chennai, India; J. Venkatesan, Notion Swedish Defense Research Agency (FOI), Robotics, Bangalore, India Stockholm, Sweden; E. Heimdal Nilsson, Lund University, Lund, Sweden; C. Fureby, Swedish Defense Research Agency (FOI), Stockholm, Sweden Tuesday, 28 July 2015 94-GTE-7 Engine Design I Lake Monroe Chaired by: S. RAGHAVAN, University of Central Florida 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-4021 AIAA-2015-4022 AIAA-2015-4023 AIAA-2015-4024 AIAA-2015-4025 AIAA-2015-4026 AIAA-2015-4027 Three-dimensional Full Annulus High Bypass Ratio Turbofan Engine A Methodology To Assess The Techno-economic and Common Core Engine Design Using A Multi-Stage Method for the Development of Velocity Profile Unsteady RANS Simulation of an with Additional Tip-Driving Fan: a Capability Of Engine Designs To Environmental Risk Assessment Bayesian Networks for Design Evaluation of the Performance Generating Screens for Gas Turbine Integrated Propulsion System Design Innovation Meet Closed-Loop Performance And of a Blended Wing Body with Uncertainty Analysis Impact of Manufacturing Variations Components

62 D. Guegan, M. Schvallinger, F. Julienne, X. Xin, G. Huang, W. Lu, J. Wang, Nanjing Operability Requirements Distributed Propulsion R. Treubig, C. Perullo, D. Mavris, Georgia for Steam Turbines J. Tate, M. Medina, D. Gonzalez, W. Safran Group, Moissy-Cramayel, France; N. University of Aeronautics and Astronautics, A. Zinnecker, N&R Engineering, Inc., C. Goldberg, D. Nalianda, R. Singh, Institute of Technology, Atlanta, GA J. Yang, Peking University, Beijing, China; Wang, J. Kapat, University of Central Gourdain, University of Toulouse, Toulouse, Nanjing, China Parma Heights, OH; J. Csank, NASA Glenn Cranfield University, Cranfield, United J. Xiong, University of Califonia, Irvine, Florida, Orlando, FL; J. Rodriguez, France; M. Gazaix, ONERA, Châtillon, Research Center, Cleveland, OH Kingdom Irvine, CA; I. Mcbean, Alstom, Baden, Siemens, Orlando, FL; et al. France Switzerland; F. Liu, University of Califonia, Irvine, Irvine, CA; S. Havakechian, Alstom, Baden, Switzerland; J. Luo, Peking University, Beijing, China Tuesday, 28 July 2015 95-GTE-8 Engine Design II Lake Florence Chaired by: D. FOUTCH, The Boeing Company 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-4028 AIAA-2015-4029 AIAA-2015-4030 AIAA-2015-4031 AIAA-2015-4032 A Composite Cycle Engine Concept Assessment of Distributed A Parametric Gas Turbine Modeling Nonlinear Dynamic Modeling of a Preliminary Design of a Gas with Hecto-Pressure Ratio Propulsion Systems Used with Approach for Assessing Transient Supersonic Commerical Transport Turbine to Drive a South African S. Kaiser, Bauhaus Luftfahrt e.V., Different Aircraft Configurations Technologies in the Conceptual Turbo-Machinery Propulsion System Commercial Booster Engine Munich, Germany; S. Donnerhack, MTU P. Laskaridis, Cranfield University, Design Phase for Aero-Propulso-Servo-Elasticity D. Fitzgerald, G. Smith, M. Brooks, Aero Engines AG, Munich, Germany; Cranfield, United Kingdom M. Ozcan, C. Perullo, J. Tai, D. Mavris, Reserach University of KwaZulu-Natal, Durban, A. Lundbladh, GKN Aerospace Engine Georgia Institute of Technology, Atlanta, J. Connolly, G. Kopasakis, NASA Glenn South Africa; G. Snedden, Council for Systems, Trollhättan, Sweden GA Research Center, Cleveland, OH; J. Scientific and Industrial Research, Durban, Carlson, NASA Langley Research Center, South Africa Hampton, VA; K. Woolwine, University of Colorado, Boulder, Boulder, CO Tuesday, 28 July 2015 96-HR-5 Design and Development of Novel Hybrid Rocket Concepts Lake Sheen B Chaired by: T. SHIMADA, Japan Aerospace Exploration Agency and Y. CHEN, National Space Organization Taiwan 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-4033 AIAA-2015-4034 AIAA-2015-4035 AIAA-2015-4036 AIAA-2015-4037 AIAA-2015-4038 Perforfance Characterisation of A Survey of Additively Testing and Evaluation of a Double- Design and Testing of an Additively Study on a Plasma Jet Igniter for a Testing and Modeling of a Porous a Hybrid Propulsion System for Manufactured Propellant Materials Tube Hybrid Rocket Motor Manufactured Advanced Hybrid Hybrid Rocket Polyethylene Axial-Injection, End- Cubesat Missions for Arc-Ignition of Hybrid Rockets A. Pons Lorente, N. Yu, B. Zhao, Beihang Rocket Motor Propulsion Unit for R. Kimura, I. Nakagawa, Tokai University, Burning Hybrid Rocket Motor O. Ahmed, University of Surrey, Guildford, S. Whitmore, Z. Spurrier, J. Fuller, J. University, Beijing, China CubeSats (PUC) Kanagawa, Japan M. Hitt, R. Frederick, University of United Kingdom Desain, Utah State University, Logan, UT B. McKnight, J. Boyer, P. Nardozzo, A. Alabama, Huntsville, Huntsville, AL Cortopassi, Pennsylvania State University, State College, PA Tuesday, 28 July 2015 97-HR-6 Development and Evaluation of Novel Oxidizer and Fuel Formulations Lake Highland B Chaired by: G. STORY, NASA Marshall Space Flight Center and J. DAVITIAN, The Aerospace Corporation 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-4039 AIAA-2015-4040 AIAA-2015-4041 AIAA-2015-4042 Manufacturing Processes of Thermal Decomposition of Aqueous Hybrid Rocket Enhancement by Paraffin-based Fuels and Energetic Paraffin Grains as Fuel for Hybrid Hydroxyl-Ammonium Nitrate Micro- and Nano-Scale Additives in Additives for Hybrid Rocket Rocket Engines Solutions Using a Hybrid Propellant HTPB Fuel Grains Propulsion F. Piscitelli, G. Saccone, A. Gianvito, G. Gas Generator J. Thomas, E. Petersen, Texas A&M M. Boiocchi, F. Maggi, C. Paravan, L. Cosentino, L. Mazzola, Italian Aerospace S. Whitmore, D. Merkley, S. Walker, Z. University, College Station, TX; J. Desain, Galfetti, Technical University of Milan, Research Center (CIRA), Capua, Italy Spurrier, Utah State University, Logan, UT B. Brady, The Aerospace Corporation, El Milan, Italy

63 Segundo, CA Tuesday, 28 July 2015 98-HR-7 Hybrid Rockets - Current Programs Objectives and Updates Lake Sheen A Chaired by: S. WHITMORE, Utah State University and A. KARABEYOGLU, Space Propulsion Group Inc. 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-4043 AIAA-2015-4044 AIAA-2015-4045 AIAA-2015-4046 AIAA-2015-4047 AIAA-2015-4048 Multifunction Sounding Rocket Hybrid Rocket Motor Upscaling and Development of the North Star Preliminary Design of a 30kN Flight Test of the Phoenix-1A Preliminary Design of the Phoenix- System Development with Development Test Campaign at Sounding Rocket: Getting ready for Paraffin-Based Hybrid Rocket Hybrid Rocket 1B Hybrid Rocket Advanced Hybrid Propulsion Nammo Raufoss the first demonstration Launch Engine B. Genevieve, J. Pitot, M. Brooks, S. U. Balmogim, M. Brooks, J. Pitot, K. Y. Chen, R. Cheng, H. Chang, National A. Boiron, O. Verberne, M. Faenza, B. O. Verberne, A. Boiron, M. Faenza, B. R. Votta, M. Di Clemente, Italian Chowdhury, K. Veale, U. Balmogim, Veale, L. Roberts, B. Genevieve, University Space Organization, Hsinchu Science Haemmerli, Nammo Raufoss, Raufoss, Haemmerli, Nammo Raufoss, Raufoss, Aerospace Research Center (CIRA), University of KwaZulu-Natal, Durban, of KwaZulu-Natal, Durban, South Africa Park, Taiwan; G. Lai, J. Lin, T. Chou, Norway Norway Capua, Italy South Africa; et al. National Chiao Tung University, Hsinchu, Taiwan; et al. Tuesday, 28 July 2015 99-ITAR-2 Orlando VI Advanced Rocket and Space Technology: Propellants, Docking and Additive Manufacturing Chaired by: P. SMITH, Boeing 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-4049 AIAA-2015-4050 AIAA-2015-4254 AIAA-2015-4052 AIAA-2015-4055 AIAA-2015-4053 AIAA-2015-4054 Performance Evaluation of a Vapor Containment and Mitigation Enabling Beyond Earth Exploration Investigation of a Dual Bell Nozzle Destructive Removal of Candidate Flame Studies of LMP-103S Catalytic Studies of LMP-103S Candidate Full-scale Dynamic of Monomethylhydrazine and with the Space Launch System for the MR-104G Monopropellant Subscale Two-Piece Silicone Decomposition Products Decomposition Interface Seal for the International Nitrogen Tetroxide B. Donahue, The Boeing Company, Thruster on the Orion Capsule Elastomer Docking Seals J. Barragan, University of Texas, El Paso, J. Barragan, A. Vazquez, A. Choudhuri, Low Impact Docking System B. Austin, IN Space, LLC, West Lafayette, Huntsville, AL S. Stanley, M. Walker, Aerojet H. Oravec, C. Daniels, University of Akron, El Paso, TX University of Texas, El Paso, El Paso, TX S. Taylor, University of Toledo, Toledo, IN; T. Voskuilen, J. Gabl, T. Pourpoint, Rocketdyne, Sacramento, CA Akron, OH; N. Penney, Ohio Aerospace OH; J. Mather, University of Akron, Akron, Purdue University, West Lafayette, IN Institute, Cleveland, OH OH; N. Penney, Ohio Aerospace Institute, Cleveland, OH; H. Oravec, C. Daniels, University of Akron, Akron, OH Tuesday, 28 July 2015 100-LP-12 Green Propulsion Orange E Chaired by: T. POURPOINT, Purdue University and D. SARGENT, Federal Aviation Administration 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-4056 AIAA-2015-4057 AIAA-2015-4058 AIAA-2015-4059 AIAA-2015-4060 AIAA-2015-4061 AIAA-2015-4062 Test Bench for the Unsteady Pulse Mode Operation of a 1 N PulCheR-Pulsed Chemical Rocket Propulsive Performance of a 1 N A Light Unsaturated Hydrocarbon Experimental and Numerical Development of 500 N Scale Green Characterization of a Pulsed Green 98% Hydrogen Peroxide Thruster with Green High Performance 98% Hydrogen Peroxide Thruster and Hydrogen Peroxide as Future Analysis of the Heat Flux Occurring Hypergolic Bipropellant Thruster Monopropellant Thruster L. Torre, A. Pasini, G. Pace, Alta S.p.A., Propellants: Second Year Project A. Pasini, L. Torre, G. Pace, Alta S.p.A., Green Propellants for Bipropellant in a Nitrous Oxide/Ethene using Hydrogen Peroxide as an Pisa, Italy Pisa, Italy 64 G. Pace, A. Pasini, L. Torre, Alta S.p.A., Overview Thrusters Green Propellant Combustion Oxidizer Pisa, Italy A. Pasini, L. Torre, G. Pace, Alta S.p.A., A. Pasini, G. Pace, L. Torre, Alta S.p.A., Demonstrator H. Kang, S. Kwon, Korea Advanced Pisa, Italy Pisa, Italy L. Werling, B. Hochheimer, A. Baral, Institute of Science and Technology, A. Gernoth, S. Schlechtriem, German Daejeon, Korea (the Republic of) Aerospace Center (DLR), Lampoldshausen, Germany Tuesday, 28 July 2015 101-LP-13 Liquid Rocket Engines Orange F Chaired by: J. SCHNACKEL, United Launch Alliance, LLC and J. MOORE, MOOG Inc, ISP Division 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-4063 AIAA-2015-4064 AIAA-2015-4065 AIAA-2015-4066 AIAA-2015-4067 VINCI, the European Reference For False Positive and False Negative Development of a Reusable LOX/ A Liquid Rocket Engine Conceptual CNES Future Preparation For Liquid Ariane 6 Upper Stage Cryogenic Analysis for Enhancing Liquid LH2 Rocket Engine - Firing Tests Design Tradeoff Methodology Propulsion Propulsive System Propulsion System Reliability and and Lifetime Evaluation Analysis Using An A Priori Articulation S. Palerm, C. Bonhomme, S. Petitot, P. Alliot, Safran Group, Paris, France; J. Safety T. Kimura, T. Hashimoto, M. Sato, S. Of Preference Information With French Space Agency (CNES), Paris, Delange, Airbus, Paris, France; A. Lekeux, Z. Huang, Aerojet Rocketdyne, Los Takada, S. Moriya, Japan Aerospace Epistemic Uncertaintie France; J. Chopinet, Snecma, Vernon, French Space Agency (CNES), Paris, Angeles, CA Exploration Agency (JAXA), Kakuda, S. Krueger, R. Strunz, Airbus, Munich, France France Japan; T. Yagishita, Japan Aerospace Germany; J. Herrmann, University of Exploration Agency (JAXA), Sagamihara, Maryland, College Park, College Park, MD Japan; et al. Tuesday, 28 July 2015 102-LP-14 Materials & Manufacturing Lake Lucerne Chaired by: D. GUADAGNOLI, Orbital ATK and M. MEYER, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-4252 AIAA-2015-4068 AIAA-2015-4069 AIAA-2015-4070 AIAA-2015-4071 AIAA-2015-4051 Results Of Material Compatibility Use of Additive Manufacturing Thermo-Structural Enhancement Comparison Of Damage Parameter A TMF Panel Optimization Strategy Designing and Testing Liquid Investigation Of Hydrogen to Model and Develop Advanced of Liquid-Propellant Rocket Engine Based Finite Element Fatigue Life Applied To The FLPP Storable Engines for Additive Manufacturing Peroxide Liquid Propulsion Designs Thrust Chambers Using Functionally Analysis Results To Combustion Engine Hot Gas Wall Geometry D. Atyam, N. Nguyen, University of C. Scharlemann, University of Applied J. Catina, K. Castonguay, U.S. Naval Graded Alloys Chamber Type TMF Panel Test J. Riccius, B. Jayaganesan, German California, San Diego, La Jolla, CA Sciences, Wiener Neustadt, Austria Academy, Annapolis, MD M. Knight, K. Adriany, S. Guerin, A. Results Aerospace Center (DLR), Lampoldshausen, Kieatiwong, E. Bayat, University of G. Thiede, E. Zametaev, J. Riccius, German Germany California, San Diego, La Jolla, CA Aerospace Center (DLR), Lampoldshausen, Germany; S. Reese, RWTH Aachen University, Aachen, Germany Tuesday, 28 July 2015 103-LP-15 Propellant Slosh Lake Highland A Chaired by: G. COLL, Orbital ATK and E. JACOB, GTL 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-4072 AIAA-2015-4073 AIAA-2015-4074 AIAA-2015-4075 AIAA-2015-4076 AIAA-2015-4077 Modeling of Non-isothermal Preliminary Design Tools for Design Of A Liquid Sloshing Characterization of Elastomeric Validation and Rules-of-Thumb for Experimental, Numerical and Cryogenic Fluid Sloshing Axisymmetric Propellant Tanks: Experiment To Operate In The Diaphragm Motion within a Computational Predictions of Liquid Analytical Characterization of J. Agui, J. Moder, NASA Glenn Research Geometry and Liquid Slosh International Space Station Spacecraft Propellant Tank Slosh Dynamics Slosh Dynamics Applied to In- Center, Cleveland, OH S. Coogan, Southwest Research Institute, G. Lapilli, Florida Institute of Technology, G. Lapilli, Florida Institute of Technology, G. Musgrove, S. Coogan, Southwest Space Propellant Storage and 65 San Antonio, TX Melbourne, FL Melbourne, FL Research Institute, San Antonio, TX Management J. Storey, D. Kirk, H. Gutierrez, Florida Institute of Technology, Melbourne, FL; B. Marsell, P. Schallhorn, NASA Kennedy Space Center, Cape Canaveral, FL Tuesday, 28 July 2015 104-NFF-4 Future Flight Propulsion Systems Lake Nona A Chaired by: G. MEHOLIC, The Aerospace Corporation and H. FEARN, California State University, Fullerton 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-4078 AIAA-2015-4079 AIAA-2015-4080 AIAA-2015-4081 AIAA-2015-4082 AIAA-2015-4083 Atmospheric Mining in the Outer Space-to-Space Power Beaming Design and First Measurements of Replication and Experimental New Theoretical Results for the Direct Thrust Measurements of an Solar System: Aerial Vehicle Mission Enabling High Performance Rapid a Superconducting Gravity-Impulse- Characterization of the Wallace Mach Effect Thruster EMDrive and Evaluation of Possible and Design Issues Geocentric Orbit Transfer Generator Dynamic Force Field Generator H. Fearn, California State University, Side-Effects B. Palaszewski, NASA Glenn Research J. Dankanich, NASA Marshall Space I. Lörincz, M. Tajmar, Technical University M. Tajmar, Technical University of Dresden, Fullerton, CA M. Tajmar, Technical University of Dresden, Center, Cleveland, OH Flight Center, Huntsville, AL; C. Vassallo, of Dresden, Dresden, Germany Dresden, Germany Dresden, Germany University of Texas, Austin, Austin, TX; M. Tadge, Purdue University, West Lafayette, IN Tuesday, 28 July 2015 105-PC-7 Combustion Diagnostics and Experiments Lake George A Chaired by: J. GORD, Air Force Reseach Laboratory and W. KULATILAKA, Texas A & M Univrsity 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-4084 AIAA-2015-4085 AIAA-2015-4086 AIAA-2015-4087 AIAA-2015-4088 AIAA-2015-4089 AIAA-2015-4090 Dynamics of Flame Lift-Off in Simultaneous Kerosene/OH LIF An Experimental and Measurement Of Local Flame Methane Ignition Delay Times in Measurements to Determine the Experimental Studies on Behaviour Biogas Swirl Flames Visualization Inside The Pre-Mixing Computational Study of Turbulent Speeds In The Thickened Flamelet CO2 Diluted Mixtures in a Shock Regimes of Turbulent Premixed of Flame Structure due to Vortex in Q. An, B. Geraedts, A. Steinberg, Duct And Combustion Chamber Lean Premixed Flames Regime Using Simultaneous 10 kHz Tube Flames V-Gutter Combustors University of Toronto, Toronto, Canada Of A Lean Staged Aero-Engine D. Han, V. Hasti, J. Gore, Purdue TPIV and OH/CH2O PLIF B. Koroglu, O. Pryor, J. Lopez, L. Nash, A. Skiba, T. Wabel, J. Temme, J. Driscoll, K. Parammasivam, K. Kirubhakaran, Anna Combustor Under Combustion University, West Lafayette, IN J. Osborne, A. Steinberg, University of S. Vasu, University of Central Florida, University of Michigan, Ann Arbor, Ann University, Chennai, India Oscillations At Elevated Pressure Toronto, Toronto, Canada; C. Carter, Orlando, FL Arbor, MI And Temperature Air Force Research Laboratory, Wright- K. Matsuura, Japan Aerospace Exploration Patterson AFB, OH; S. Ramji, University Agency (JAXA), Chofu, Japan; T. Eguchi, of Toronto, Toronto, Canada; S. Peltier, S. Oide, Hosei University, Koganei, Japan; Wright Patterson Air Force Base, Wright H. Yamada, Y. Kurosawa, T. Yamamoto, Patterson AFB, OH; S. Hammack, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan; et al. Tuesday, 28 July 2015 106-PC-8 Combustion Modeling and Simulation II Lake Louise Chaired by: J. OEFELEIN, Sandia National Laboratories and R. HAUSEN, Honeywell 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-4091 AIAA-2015-4092 AIAA-2015-4093 AIAA-2015-4094 AIAA-2015-4095

66 Optimized Ethylene Skeletal Velocity-Induced Flame Extinction On the Computations of NOx and Heat Transfer and Flow One Dimensional Network Model Chemical Kinetic Mechanisms For Dynamics of Lean Premixed Bluff- CO Formation in A 200 kW Swirl Chrecterictics in a Gas Turbine Can for a Reverse Flow Combustor Diluted Turbulent Flames Body Stabilized Flames Burner Combustor: Turbulent Interaction O. Tuncer, G. Sarikaya, G. Varol, Istanbul B. Liu, F. Qin, D. Cao, Northwestern M. Geikie, K. Ahmed, University of Central E. Khalil, A. Ahmed, M. Aly Hassan, H. S. Mohammed, E. Khalil, H. Hariedy, E. Technical University, Istanbul, Turkey Polytechnical University, Xi’an, China Florida, Orlando, FL Hariedy, Cairo University, Giza, Egypt Bially, Cairo University, Giza, Egypt Tuesday, 28 July 2015 107-PC-9 Deflagrations and Detonations Lake Virginia Chaired by: C. LI, Air Force Office of Scientific Research 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-4096 AIAA-2015-4097 AIAA-2015-4098 AIAA-2015-4099 AIAA-2015-4100 AIAA-2015-4101 AIAA-2015-4102 Laminar Deflagrated Flame Detonation Initiation with Thermal A New Packing Code for Creating A Computational Method for the An Isoconversional Method for On The Elasto-Plastic Response Schlieren-System-Visualization of Interaction with a Fluidic Jet Flow Deposition due to Pore Collapse Mirostructures of Propellants and Simulation of Hot Spot Formations Extracting Reaction Kinetics of Of Combustion Tube Subjected To Combustion Phenomena in a Two- for Deflagration-to-Detonation in Energetic Materials - Towards Explosives and Detonation in Polymer-Bonded Aluminized Cyclotrimethylene- Kerosene-Air Detonation Loading Parallel-Plane Combustor Flame Acceleration the Coupling between Micro- and G. Amadio, University of Illinois, Urbana- Explosives Trinitramine for Propulsion J. Yoh, Seoul National University, Seoul, S. Nakagami, K. Matsuoka, J. Kasahara, J. McGarry, K. Ahmed, University of Macro-scale Champaign, Urbana, IL; T. Jackson, T. Gallagher, M. Akiki, S. Menon, Georgia Y. Kim, J. Yoh, Seoul National University, Korea (the Republic of) Nagoya University, Nagoya, Japan; A. Central Florida, Orlando, FL J. Zhang, Florida Institute of Technology, University of Florida, Gainesville, Institute of Technology, Atlanta, GA Seoul, Korea (the Republic of) Matsuo, Keio University, Yokohama, Melbourne, FL; T. Jackson, University of Gainesville, FL Japan; I. Funaki, Japan Aerospace Florida, Gainesville, Gainesville, FL Exploration Agency (JAXA), Sagamihara, Japan Tuesday, 28 July 2015 108-SR-4 Solid Rocket Motor Propellant Characteristics Analysis Lake Concord A Chaired by: B. LEARY, The Johns Hopkins University Applied Physics Laboratory and A. GERARDS, US Army AMRDEC 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-4103 AIAA-2015-4104 AIAA-2015-4105 AIAA-2015-4106 AIAA-2015-4107 An Advanced Digital Cross Using Real-Time Radioscopy to Surface Temperature of Ignition Delay Times of Composite Time-Temperature Superposition Correlation Method for Solid Measure the Burning Rate of Solid Agglomerated Aluminum Particle Solid Propellants Using Novel Principle Applied to Thermally Aged Propellant Burning Rate Rocket Propellant in the Reaction Zone of AP/HTPB Nano-Additive Catalysts Composite Propellant Determination M. Denny, R. Frederick, University of Composite Propellants A. Demko, C. Dillier, E. Petersen, Texas L. Villar, L. Rezende, Aeronautics and D. Jones, M. Mascaro, D. Lineberry, Alabama, Huntsville, Huntsville, AL R. Doi, M. Nakagaki, T. Kuwahara, A&M University, College Station, TX; D. Space Institute (IAE), São José dos R. Frederick, University of Alabama, Nihon University, Funabashi, Japan; K. Reid, S. Seal, University of Central Florida, Campos, Brazil Huntsville, Huntsville, AL; M. Moser, Yamamoto, A. Fukuchi, IHI Corporation, Orlando, FL Exquadrum, Inc., Adelanto, CA Tomioka, Japan Tuesday, 28 July 2015 109-F360-4 Integrated Roles of Experimental Fluid Dynamics and Computational Fluid Dynamics Orlando IV 1500 - 1730 hrs For years, the computational and experimental fluid dynamic communities have had separate advocacies with mixed results. Many stakeholders and decision-makers may not understand the integrated roles of experimental and computational fluid dynamics (EFD/CFD) in the RDT&E process for new aero products. Do we need an integrated RDT&E map going forward for capability needs in terms of ground testing, computational methods, and flight testing?

Moderator: James Heidmann, NASA Glenn Research Center Panelists: Richard “Dick” Scharnhost Keith Blodgett Mike Mastaler Paul Van Slooten Roy Schulz

67 The Boeing Company GE Aviation NASA Headquarters United Technologies Research Center MiraFacilities2 Inc.

Tuesday, 28 July 2015 110-RLA-2 Leadership Exchange/Speed Mentoring Orange G 1600 - 1730 hrs Tuesday, 28 July 2015 111-LECT-2 Propulsion and Energy Lecture: The Transformation of the Kennedy Space Center Orange D 1800 - 1900 hrs An informational presentation on the transformation of the Kennedy Space Center from a single, program-dependent launch complex, to a diverse, multi-user spaceport of the future enabling both Government and commercial operations to and from low Earth orbit and beyond. The presentation will discuss the planning and execution of the Center’s transition from the 30-year Shuttle program; the modernization of launch and ground processing infrastructure to support NASA’s evolving Space Launch System and Orion multi-purpose crew vehicle; and the turnover of facilities and assets left underutilized by the retirement of the space shuttles to private industry and other Government agencies. Challenges related to downsizing of workforce, budget constraints, and contract and agreement strategies will be discussed, as well as overcoming barriers to change. In addition, the presentation will describe NASA’s journey to Mars and the critical work taking place at Kennedy Space Center to enable it. Speaker: Robert Cabana Center Director, NASA Kennedy Space Center Wednesday Wednesday, 29 July 2015 112-NW-10 Networking Coffee Break Ballroom Foyer 0730 - 0800 hrs Wednesday, 29 July 2015 113-SB-3 Wednesday Speaker’s Briefing In Session Room 0730 - 0800 hrs Speakers, presenters and session chairs for both the morning and afternoon technical sessions, please meet in your session room to load presentations and discuss the flow of your session. Wednesday, 29 July 2015 114-PLNRY-5 Workforce Development Panel Orange D 0800 - 0900 hrs Discover how the make-up of the workforce will change over the next decade, how we need to adapt, and how to attract the necessary talent.

Moderator: Mark Lewis, Director, IDA Science and Technology Policy Institute Panelists: Carole Hedden Yvette Weber Michael Hawes Steve Gorrell Executive Editorial Director, Aviation Week and Executive Engineering Manager, U.S. Air Force Material Command Vice President and Orion Program Manager, Lockheed Martin Associate Professor, Brigham Young University Intelligence Space Systems Company

Wednesday, 29 July 2015 115-ABPSI-4/AEP-2 Emerging Propulsion System Technologies Orange E Chaired by: S. HIRT, NASA Glenn Research Center and I. CHAKRABORTY 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-4108 AIAA-2015-4109 AIAA-2015-4110 AIAA-2015-4111 AIAA-2015-4112 Airvolt Aircraft Electric Propulsion Influence of Flow Path Model Identification Applied To Team of Unmanned Aircraft A Preliminary Database for Low Test Stand Configuration on the Performance Temperature Extrapolations of Systems (UAS) and Unmanned Reynolds Number Propeller 68 A. Samuel, Y. Lin, NASA Armstrong Flight of Hybrid Turbine - Solid Oxide Fuel Aircraft Propulsion System Items Ground Vehicles (UGV) for Performance Validations Research Center, Edwards, CA Cell Systems for Aircraft Propulsion O. Verseux, Airbus, Toulouse, France; F. Emergency Response in Mining A. Ghoddoussi, Wichita State University, and Power Uriz, Altran, Blagnac, France Applications Wichita, KS D. Waters, S. Vannoy, C. Cadou, University P. Gill, M. Hatfield, D. Randle, R. Wies, R. of Maryland, College Park, College Ganguli, S. Rosetti, University of Alaska, Park, MD Fairbanks, Fairbanks, AK; et al. Wednesday, 29 July 2015 116-APS-3 Power Generation for Planetary Missions Lake Highland B Chaired by: M. PATEL, US Merchant Marine Academy and J. HAINES, Retired - formerly ESA/ESTEC 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-4113 AIAA-2015-4114 AIAA-2015-4115 AIAA-2015-4116 A Martian Technology General Atomics Radioisotope Reestablishing the Supply of NASA’s Radioisotope Power Systems Demonstration Mission and Fueled Thermophotovoltaic Power Plutonium-238 - Plans Subsequent Human Mission Support Systems for Space Applications R. Wham, L. Felker, E. Collins, D. Benker, J. Hamley, P. McCallum, C. Sandifer, T. Use for a Space Solar Power J. Strauch, A. Klein, P. Charles, General R. Owens, R. Hobbs, Oak Ridge National Sutliff, J. Zakrajsek, NASA Glenn Research Wireless Power Transfer System Atomics, San Diego, CA; C. Murray, L3 Laboratory, Oak Ridge, TN; et al. Center, Cleveland, OH J. Straub, University of North Dakota, Power Paragon, Anaheim, CA; M. Du, Oak Grand Forks, Grand Forks, ND Ridge National Laboratory, Oak Ridge, TN Wednesday, 29 July 2015 117-EDU-2 Propulsion Education II Lake George B Chaired by: R. NARDI, Inotech LTDA and J. BENNEWITZ 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-4117 AIAA-2015-4118 AIAA-2015-4119 AIAA-2015-4120 AIAA-2015-4121 LSU Launch and Glide Program An Improved Nozzle Performance Computed Tomography Use of Generalized Fluid System Dynamic Calibration and Analysis Development of a Solid and Hybrid Laboratory Using Schlieren Flow Characterization of a Porous Hybrid Simulation Program (GFSSP) for of Crack Tip Propagation in Powered Rocket Glider: “Khaos” Visualization Motor Grain Teaching and Performing Senior Energetic Materials using Real-Time A. Baran, C. Blanchard, P. de la Vergne, P. C. Thorn, D. Olmstead, K. Tucker, U.S. Air J. Buckley, M. Denny, G. Nelson, Design Projects at the Educational Radiography Spyridon, C. Medick, J. Zimmer, Louisiana Force Academy, Colorado Springs, CO University of Alabama, Huntsville, Institutions A. Butt, R. Frederick, UAH Propulsion State University, Baton Rouge, LA; et al. Huntsville, AL A. Majumdar, A. Hedayat, NASA Marshall Research Center, Huntsville, AL Space Flight Center, Huntsville, AL Wednesday, 29 July 2015 118-EE-5 Renewable and Sustainable Energy in Florida Lake Eola 0900 - 1130 hrs This is a discussion panel where the panel members will talk about renewable and sustainable energy in Florida. Each panel member will also make a short presentation to highlight his/her scope of involvement in renewable and sustainable energy. The panel consists of leaders from the renewable and sustainable energy sectors in Florida.

Moderator: Dr. S.A. Sherif, Professor of Mechanical and Aerospace Engineering, University of Florida. Panelists: Jon Ippel Jennifer S. Szaro Dr. Prabir Barooah Dr. Saeed Moghaddam Sustainability Director and Senior Aide to the CAO, City of Manager, Renewables, Orlando Utilities Commission, Orlando, Department of Mechanical and Aerospace Engineering, University Department of Mechanical and Aerospace Engineering, University

69 Orlando, Florida. Florida. of Florida. of Florida

Wednesday, 29 July 2015 120-GE-1 Green Engineering Lake Florence Chaired by: E. KHALIL, Cairo University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-4123 AIAA-2015-4124 AIAA-2015-4125 AIAA-2015-4126 A Flight Control System for the Flashing Behavior of Ionic Liquid Personalized Air Conditioning Of Flow Modelling of Excess Carrier Rocket-Propelled and Ballistic Flight Propellants under Vacuum Air Craft Cabins For Passengers between the Microchannels of an Phases for a SubOrbital SpacePlane Conditions Comfort And Efficient Energy Use Organic Photovoltaic Solar Cell Application C. Hendrich, S. Schlechtriem, German A. Farag, E. Khalil, Cairo University, Giza, M. Shitta, E. Ogedengbe, University of D. Welberg, M. Werner, Airbus, Bremen, Aerospace Center (DLR), Lampoldshausen, Egypt Lagos, Akoka-Yaba, Nigeria Germany; J. Dutheil, Airbus, St. Medard- Germany en-Jalles, France Wednesday, 29 July 2015 121-GTE-9 Turbine III Lake Monroe Chaired by: S. VASU, University of Central Florida 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-4127 AIAA-2015-4128 AIAA-2015-4129 AIAA-2015-4130 AIAA-2015-4131 Experimental Research of Reducing Exploring an LBM-VLES Based CFD Workflow Optimization of Multi-row Turbine Blade Investigation of Pressure Drop and Turbine Tip Leakage Flow Using Approach for Predictions of Aero- Multistage Axial Turbine Aerothermal Optimization Using Heat Transfer Behavior of a Square Backward Vortex Generators Thermal Flows in Generic Turbo- V. Matveev, G. Popov, O. Baturin, E. Evolution Strategies with Viscous Channel with 45° Angle Ribs at C. Xia, G. Huang, Nanjing University of machinery Devices Goryachkin, D. Kolmakova, Samara State Flow Analysis Wide Range of Reynolds Numbers Aeronautics and Astronautics, Nanjing, Y. Li, A. Jammalamadaka, Exa Aerospace University, Samara, Russia C. Thorn, R. Hartfield, Auburn University, L. Ahmed, C. Vergos, P. Tran, W. Wang, China Corporation, Burlington, MA Auburn, AL J. Kapat, University of Central Florida, Orlando, FL Wednesday, 29 July 2015 122-HR-8 Combustion Stability, Motor Performance, and Related Issues Lake Sheen B Chaired by: P. LEMIEUX, California State Polytechnic University and S. COOGAN, Southwest Research Institute 0900 hrs 0930 hrs 1000 hrs AIAA-2015-4132 AIAA-2015-4133 AIAA-2015-4134 Indirect Heat Flux Measurements Failure Mode Investigation of a Applicability of a LOx Vaporization at the Nozzle Throat of a Hybrid Sorbitol-based Hybrid Rocket Flight Preburner for Swirling-Flow Hybrid Rocket Motor Motor for the Stratos II Sounding Rocket Engines P. Narsai, E. Momanyi, K. Venkataraman, Rocket T. Sakurai, T. Tomizawa, Tokyo B. Evans, B. Cantwell, Stanford University, T. Knop, J. Wink, R. Huijsman, R. Werner, Metropolitan University, Hino, Japan Stanford, CA J. Ehlen, S. Powell, Delft University of

70 Technology, Delft, The Netherlands; et al. Wednesday, 29 July 2015 123-HR-9 Combustion Dynamics and Mixing Efficiencies II Lake Sheen A Chaired by: J. DAVITIAN, The Aerospace Corporation and T. SHIMADA, Japan Aerospace Exploration Agency 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-4135 AIAA-2015-4136 AIAA-2015-4137 AIAA-2015-4138 AIAA-2015-4139 Numerical and Experimental Combustion Characteristics of Gas Combustion Visualization and A Fundamental Study of a End- Effect of Nano Particle Addition on

Investigation of HDPE Hybrid Hybrid Rocket using H2O/HNO3 as Characterization of Liquefying Burning Swirling-Flow Hybrid the Regression Rate of Liquefying Propulsion with Dual Vortical-Flow Oxidizer Hybrid Rocket Fuels Rocket Engine using Low Melting Fuels Chamber Designs I. Suzuki, T. Kuwahara, Nihon University, M. Kobald, A. Petrarolo, S. Schlechtriem, Temperature Fuels O. Dermanci, BLIS, Ankara, Turkey; A. G. Lai, S. Wei, T. Chou, J. Lin, J. Wu, Funabashi, Japan German Aerospace Center (DLR), T. Sakurai, D. Hayashi, Tokyo Metropolitan Karabeyoglu, KOC University, Istanbul, National Chiao Tung University, Hsinchu, Lampoldshausen, Germany University, Hino, Japan Turkey Taiwan; Y. Chen, National Space Organization, Hsinchu, Taiwan Wednesday, 29 July 2015 124-HSABP-4 Experimental and Computational Research in Supersonic Injection Including Predictive Capability Lake Mizell B Chaired by: R. MOEHLENKAMP, Aerojet Rocketdyne and E. AXDAHL, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs AIAA-2015-4140 AIAA-2015-4141 AIAA-2015-4142 The Interaction of Variable Duty Investigation of Large-Scale On Mode-transition within Cycle Pulsed Injection and a Structures in Supersonic Planar Diverging Dual-mode Combustors Supersonic Shear Layer in a non-reactive Shear Layer with a S. Tomioka, K. Kobayashi, Japan Scramjet Combustor Base Flow Region Aerospace Exploration Agency (JAXA), L. Smith, S. Farokhi, University of Kansas, J. Wu, H. Zhang, J. Chen, Y. Zhao, Kakuda, Japan; K. Nojima, S. Ishizaki, Lawrence, Lawrence, KS National University of Defense Technology, Tohoku University, Sendai, Japan Changsha, China Wednesday, 29 July 2015 125-HSABP-5/GTE-10 High-Speed Pressurized Systems Lake George A Chaired by: V. TANGIRALA, General Electric and R. STARKEY, University of Colorado Boulder 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-4143 AIAA-2015-4144 AIAA-2015-4145 AIAA-2015-4146 AIAA-2015-4147 Stage-by-Stage and Parallel Flow Numerical Investigation A New Method to Predict Flow Performance Evaluation of Understanding the Effects of Fractal Path Compressor Modeling for a of Expanded and Stepped Rates of Gaseous Fuels Injected a Turbine driven by a Pulse Blockage Geometries on Flame Variable Cycle Engine Centerbodiless RDE Designs Intermittently for Pulse Detonation Detonation Combustor for Micro Acceleration in Propane-Air Flames G. Kopasakis, NASA Glenn Research W. Stoddard, E. Gutmark, University of Engines Gas Turbines J. Knapton, S. Blakey, F. Nicolleau, Center, Cleveland, OH; L. Cheng, Cincinnati, Cincinnati, OH D. Joshi, F. Lu, University of Texas, T. Sakurai, Tokyo Metropolitan University, University of Sheffield, Sheffield, United University of Washington, Seattle, Seattle, Arlington, Arlington, TX Hino, Japan Kingdom

71 WA; J. Connolly, NASA Glenn Research Center, Cleveland, OH Wednesday, 29 July 2015 126-LP-16 Propellant Storage & Management II Orange F Chaired by: V. AHUJA, CRAFT Tech and M. DEANS 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-4148 AIAA-2015-4149 AIAA-2015-4150 AIAA-2015-4151 Transient Capillary Vane Analysis Microgravity PMD investigations by Satellite Fuel Estimation Algorithm Simulated Propellant Loading R. Manning, I. Ballinger, Keystone miniaturization of the test sample and Application to the Defense System: A test bed for launch Engineering Company, Long Beach, CA; M. A. De Quero, International Air Transport Satellite Communication System III systems research and development Dowdy, Angeles Crest Engineering, Inc., Association, Geneva, Switzerland; P. (DSCS III) J. Toro Medina, J. Sass, J. Youney, NASA Pasadena, CA; Y. Chen, Portland State Pontelandolfo, R. Putzu, Hepia, Geneva, B. Rhodes, M. Mueller, The Aerospace Kennedy Space Center, Cape Canaveral, FL University, Portland, OR Switzerland Corporation, El Segundo, CA Wednesday, 29 July 2015 127-LP-17 Rocket Nozzles I Lake Lucerne Chaired by: P. GLOYER, Gloyer-Taylor Laboratory and S. BARSI, NASA 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-4152 AIAA-2015-4153 AIAA-2015-4154 AIAA-2015-4155 AIAA-2015-4156 Simulation of Cold Flow in a Flow Separation Study In Stiff Flow Separation Study in Stiff LOX/CH4 Hot Firing Dual Bell LOX/CH4 Hot Firing Dual Truncated Ideal Nozzle with Film Ovalized Rocket Nozzles, Part I: Ovalized Rocket Nozzles, Part II: Nozzle Testing: Part I -Transitional Bell Nozzle Testing: Part II Cooling Experimental Approach Numerical Approach Behavior- -Characteristics of Combustion K. Braman, Tuskegee University, C. Genin, S. Jack, German Aerospace S. Jack, German Aerospace Center C. Genin, D. Schneider, German Aerospace Instability and Heat Flux- Huntsville, AL; J. Ruf, NASA Marshall Center (DLR), Lampoldshausen, Germany (DLR), Braunschweig, Germany; C. Center (DLR), Lampoldshausen, Germany; H. Takahashi, T. Tomita, Japan Aerospace Space Flight Center, Huntsville, AL Genin, German Aerospace Center (DLR), H. Takahashi, T. Tomita, Japan Aerospace Exploration Agency (JAXA), Kakuda, Lampoldshausen, Germany Exploration Agency (JAXA), Kakuda, Japan Japan; C. Genin, D. Schneider, German Aerospace Center (DLR), Lampoldshausen, Germany Wednesday, 29 July 2015 128-LP-18 Spacecraft Propulsion Systems II Lake Nona B Chaired by: E. BESNARD, California State University-Long Beach and H. KAGAWA, JAXA 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-4157 AIAA-2015-4158 AIAA-2015-4159 AIAA-2015-4160 AIAA-2015-4161 AIAA-2015-4162 Development of the MPCV ESM Density Fit for MON Oxidizer Vapor Pressure Fit for MON Empirical Relations for Assessing Development and Test of a 3D Performance Evaluation of a 70 propellant tanks Blends Including Accuracy Oxidizer Blends Including Accuracy the Formation of Iron Nitrate in printed Hydrogen Peroxide Flight N Hydrazine Thruster According P. Behruzi, D. Gaulke, J. Klatte, N. Fries, M. Mueller, The Aerospace Corporation, El M. Mueller, The Aerospace Corporation, El Nitrogen Tetroxide Systems Control Thruster to the Variation of Characteristic Airbus, Bremen, Germany Segundo, CA Segundo, CA M. Mueller, The Aerospace Corporation, El U. Gotzig, Airbus, Lampoldshausen, Length 72 Segundo, CA Germany J. Kim, H. Jung, S. Bae, D. Bae, Pukyong National University, Busan, Korea (the Republic of); J. Kim, Hanwha Corporation, Daejeon, Korea (the Republic of) Wednesday, 29 July 2015 129-NFF-5 Conversations in Breakthrough Propulsion Physics: Gravity Lake Nona A 0900 - 1200 hrs Round table members: Dr. George J. Williams Prof. Martin Tajmar Dr. Bryan A. Palaszewsk Senior Scientist, Ohio Aerospace Institute, NASA Glenn Research Center Dresden Univ. of Technology, Dresden, Germany Senior Scientist, NASA Glenn Research Center, Cleveland, OH

Wednesday, 29 July 2015 130-NW-11 Networking Coffee Break Exposition Hall 0900 - 0930 hrs Wednesday, 29 July 2015 131-PC-10 Modeling of Combustion Dynamics, Instabilities and Noise II Lake Louise Chaired by: R. SUJITH, IHI Marine United Inc. 0900 hrs 0930 hrs 1000 hrs AIAA-2015-4163 AIAA-2015-4164 AIAA-2015-4165 Global POD-Based Adaption Development and Analysis of a Development of Combustion Scheme for Reduced Order Models Novel Two-Dimensional Flame Instability Analysis Tool by of the Reaction-Advection Equation Transfer Function Incorporating Combustion Response C. Huang, W. Anderson, C. Merkle, Purdue V. Rani, S. Rani, University of Alabama, Models University, West Lafayette, IN Huntsville, Huntsville, AL G. Tamanampudi, W. Anderson, Purdue University, West Lafayette, IN Wednesday, 29 July 2015 132-PC-11 Scramjets, Supersonic Combustion Lake Virginia Chaired by: E. LYNCH, Aerojet Rocketdyne 0900 hrs 0930 hrs AIAA-2015-4166 AIAA-2015-4167 Quasi-One-Dimensional and Two- Numerical Investigation Of The Dimensional Numerical Simulation Effect Of Reaction Models On The of Scramjet Combustors Supersonic Combustion Of Liquid R. Seleznev, All-Russian Scientific Research Kerosene Institute of Automatics, Moscow, Russia; L. Gang, Z. Hua, T. Liang, L. Yu, X. Xu, S. Surzhikov, Russian Academy of Science, Beihang University, Beijing, China Moscow, Russia 73 Wednesday, 29 July 2015 133-PP-1 Propulsion and Power Systems of Unmanned Systems Lake Highland A Chaired by: L. CHEN, TAMUCC 0900 hrs 0930 hrs AIAA-2015-4168 AIAA-2015-4169 Development of a Series Hybrid Performance Characteristics of Propulsion System for Unmanned Fluidic-Based Thrust Augmentation Aerial Vehicles Using a Slot Jet for Unmanned D. Trawick, D. Moroniti, D. Mavris, Georgia Aerial Vehicle Propulsion Institute of Technology, Atlanta, GA B. Wiedow, Old Dominion University, Norfolk, VA; K. Ahmed, University of Central Florida, Orlando, FL Wednesday, 29 July 2015 134-SC-1 Engineering and Analysis for Propulsion System Design Lake Down B Chaired by: T. GIEL, Jacobs Technology and C. GATTO, Jet Propulsion Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-4170 AIAA-2015-4171 AIAA-2015-4172 AIAA-2015-4173 Lotus: Standardized ESPA Effects of Gravity on Cryogenic Fuel Pump Trade Study for a “Resurrected” DSCOVR Propulsion Propulsion System Flow Boiling and Chilldown Conceptual Design of an Integrated System - Challenges and Lessons C. singh-derewa, Jet Propulsion Laboratory, Efficiency Air Vehicle System Lesson Learned California Institute of Technology, S. Darr, H. Hu, J. Chung, University of A. Donovan, R. Roberts, M. Wolff, Wright A. Varia, A. Scroggins, NASA Goddard Pasadena, CA; S. Fisher, A. Vora, Surrey Florida, Gainesville, Gainesville, FL; J. State University, Dayton, OH Space Flight Center, Greenbelt, MD Satellite Technology, Ltd., Surrey, United Hartwig, NASA Glenn Research Center, Kingdom; S. Raviprasad, Manipal Institute Cleveland, OH; A. Majumdar, NASA of Technology, Manipal, India; C. Iwata, Marshall Space Flight Center, Huntsville, International Space University, Illkirch- AL Graffenstaden, France; M. Seymour, Asteria Space Consulting, Rochester, NY Wednesday, 29 July 2015 135-SR-5 Solid Rocket Motor Nozzles, Thrust Management, and Ignition Lake Concord A Chaired by: M. BERDOYES, Herakles and D. BIANCHI, Sapienza University of Rome 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-4174 AIAA-2015-4175 AIAA-2015-4176 AIAA-2015-4177 AIAA-2015-4178 Evaluation of Quasi-One- Numerical Simulation of Chemical Investigation of Dual-Thrust Rocket Active Interruption of Solid- Influence of Starting Chamber Dimensional Modeling for Nozzle Erosion in VEGA Launcher Solid- Motor with Subsonic Intermediate Propellant Combustion in a Choked Dynamics on Nozzle Flow Choking

74 Flow Separation Propellant Rocket Motor Nozzles Nozzle Chamber Time and the Liftoff Time of Dual- B. Maicke, Pennsylvania State University, D. Bianchi, University of Rome “La A. El-Nady, M. Ahmed, M. ALsenbawy, M. Tanaka, G. Shibasawa, National thrust Rockets Middletown, PA Sapienza”, Rome, Italy; A. Neri, ESA, Military Technical College, Cairo, Egypt; Defense Academy, Yokosuka, Japan S. Mani, R. Tharikaa, S. Ajith, N. Naveen, Rome, Italy A. Sarhan, Modern Academy in Maadi, R. Vignesh, J. John, Kumaraguru College Cairo, Egypt of Technology, Coimbatore, India; et al. Wednesday, 29 July 2015 136-TM-4 Future Demands for Thermal Management: Opportunities and Challenges Lake Down A 0900 - 1130 hrs This is a discussion panel where the panel members will talk about the future demand of thermal management technologies, with emphasis on challenges and opportunities. Each panel member will also make a short presentation to highlight his/her scope of involvement in thermal management technologies and view of the future demands for these technologies.

Moderator: Michael Choi, NASA Goddard Space Flight Center Panelists: Steven M. Iden Dr. Louis Chow Guy Wagner Tapan Desai OPTIMUS Program Manager, MDO Systems, AFRL/RQVC, Wright Professor & Univ. Chair of Department of Mechanical and Director, Electronic Cooling Solution, Inc. R&D manager, Defense-Aerospace, Advanced Cooling Patterson Air Force Base. Aerospace Engineering, University of Central Florida. Technologies, Inc., Lancaster, PA Wednesday, 29 July 2015 137-F360-5 Work Life Balance Orlando IV 0930 - 1200 hrs The costs for educating and training a worker in the aerospace profession are extremely high. In today’s environment, a good number of households are dual income; and the incoming workforce of Millennials value family, personal connection, and loyalty. Panelists will explore policies and methods for creating an environment that will enable individuals to balance work and life needs in order to maintain a reliable, diverse, and effective workforce.

Moderator: Barbara Esker, NASA ARMD Panelists: Amanda Billot Jim Free Elizabeth Bierman Klod Kokini Pratt and Whitney NASA Glenn Research Center Honeywell Aerospace Purdue University

Wednesday, 29 July 2015 138-NW-12 Recognition Luncheon Florida Ballroom 1200 - 1330 hrs Wednesday, 29 July 2015 139-PLNRY-6 Closing Keynote Orange D 1330 - 1500 hrs Developing Creative Storytelling Using Model Based Design Michael Tschanz Director, Technology and Analysis, Design and Engineering, Walt Disney World® Wednesday, 29 July 2015 75 140-ECD-4 Magnetohydrodynamic, Brayton, AMTEC, and Other Advanced Concepts Lake Nona B Chaired by: M. PISZCZOR, NASA Glenn Research Center and E. LEWANDOWSKI, NASA Glenn Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-4179 AIAA-2015-4180 AIAA-2015-4181 AIAA-2015-4182 Effects of Magnetohydrodynamic Numerical Simulation of Characteristic Investigation on Flow Numerical Research on Combustion Energy Generation on Planetary Performance of a High and Heat Transfer of Capillary Flow Field in Li/SF6 Surface Entry Vehicle Flight Dynamics Temperature Inert Gas Plasma Pump in AMTEC Injection Reactor H. Ali, R. Braun, Georgia Institute of Faraday-type MHD Generator with C. Zhou, Harbin Engineering University, C. Zhou, Harbin Engineering University, Technology, Atlanta, GA various working gases Harbin, China Harbin, China M. Tanaka, Y. Okuno, Tokyo Institute of Technology, Yokohama, Japan Wednesday, 29 July 2015 141-ECS-3 Energetic Components & Systems Educational Series Lake Eola 1500 - 1800 hrs Chaired by: J. SCOTT, United Launch Alliance, LLC Have you ever wondered how the world of explosives and propellants crosses over into the Aerospace world? Come join the Energetic Components Subcommittee expert panel as we discuss the world of aerospace pyrotechnics. We will review the history of our technology, how we cross over into all disciplines of chemistry, strength of materials, thermodynamics, statistics etc.

Moderator / Participant - John G. Scott, ULA Launch Systems, Ordnance Engineer Panelists: Selma Goldstein Lien Yang Thomas Blachowski John Burchett Hobin S. Lee John G. Scott Aerospace Corporation, Ordnance Consultant Navy (NSWCIHEODTD) - Ordnance Navy (NSWCIHEODTD) - System Safety / Chemring Energetics Devices, Director of ULA Launch Systems, Ordnance Engineer Engineering Engineer Ordnance Engineer Engineering

Wednesday, 29 July 2015 142-EP-10 Pulsed and Micro Thrusters Lake Mizell A Chaired by: K. POLZIN, NASA Marshall Space Flight Center and S. BERG, Missouri University of Science and Technology 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-4186 AIAA-2015-4184 AIAA-2015-4183 Oral Presentation AIAA-2015-4185 AIAA-2015-4187 Dynamic Modeling and Using Additive Manufacturing to A Short-Pulse Laser-Assisted Pulsed High Frequency Operation of a Plasma Plume Characterization Development of Long-Lifetime Experimental Validation of Thrust- Print a CubeSat Propulsion System Plasma Thruster Low-power Short-pulse Plasma of Electric Solid Propellant Micro Pulsed Gas Valves for Pulsed stand for Micropropulsion Testing W. Marshall, J. Stegeman, M. Zemba, K. Matsubara, H. Hosokawa, N. Akashi, Thruster Pulsed Plasma Thrusters Electric Thrusters D. Lee, W. O’Neill, A. Cofer, A. Alexeenko, NASA Glenn Research Center, Cleveland, Y. Oigawa, H. Horisawa, Tokai University, Y. Nakamura, H. Hosokawa, H. Horisawa, M. Glascock, J. Rovey, Missouri University W. Burkhardt, J. Crapuchettes, WASK Purdue University, West Lafayette, IN OH; E. MacDonald, C. Shemelya, R. Hiratsuka, Japan Tokai University, Hiratsuka, Japan of Science and Technology, Rolla, MO; S. Engineering, Inc., Cameron Park, CA; B. 76 Wicker, University of Texas, El Paso, El Williams, J. Thrasher, Digital Solid State Addona, K. Polzin, NASA Marshall Space Paso, TX; et al. Propulsion, LLC, Reno, NV Flight Center, Huntsville, AL Wednesday, 29 July 2015 143-GTE-11/HSABP-6 Detonation Engines Lake Florence Chaired by: S. VASU, University of Central Florida 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-4188 AIAA-2015-4189 AIAA-2015-4190 AIAA-2015-4191 AIAA-2015-4192 Wave Rotor Combustor Turbine Numerical Study of Pulse Parametric Study of Pulse- Unsteady Heat Transfer Numerical Investigation of Effects Model Development Detonation Engine Nozzle and Combustor-Driven Ejectors at Analysis to Predict Combustor of Fuel Injection on Rotating R. Jagannath, S. Bane, Purdue University, Exhaust Flow Phenomena High-Pressure Wall Temperature in Rotating Detonation Engine West Lafayette, IN; M. Nalim, Indiana J. Peace, F. Lu, University of Texas, S. Yungster, Ohio Aerospace Institute, Detonation Engine S. Yao, J. Wang, Peking University, University-Purdue University Indianapolis, Arlington, Arlington, TX Brookpark, OH; D. Paxson, H. Perkins, A. Roy, P. Strakey, T. Sidwell, D. Ferguson, Beijing, China Indianapolis, IN NASA Glenn Research Center, Cleveland, National Energy Technology Laboratory, OH Morgantown, WV Wednesday, 29 July 2015 144-GTE-12 Turbine Durability Lake Monroe Chaired by: S. RAGHAVAN, University of Central Florida 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-4193 AIAA-2015-4194 AIAA-2015-4195 AIAA-2015-4196 AIAA-2015-4197 AIAA-2015-4198 Blade Surface-Particle Interaction Using Gas Turbine Engine Casing Material Properties of Hard Identification of Material Damage High Accuracy Total Temperature The Effect of Inclination Angle on and Multifunctional Coatings For Accelerometer Measurements for Coatings Developed for High Precursors using Nonlinear Measurements in a Turbine Turbulent Quantities of a Single Gas Turbine Engine Rotor Blade Health Monitoring Damping Ultrasonics Powered Simulator Unit Row of Cylindrical Jets in Crossflow M. Murugan, A. Ghoshal, B. Barnett, J. Cox, P. Anusonti-Inthra, S. Arnold, P. Torvik, Self, Kettering, OH; B. Langley, G. Bunget, Luna Innovations, Inc., D. Murakami, NASA Ames Research J. Hodges, Z. Little, C. Fernandes, G. M. Pepi, Army Research Laboratory, University of Tennessee Space Institute, Universal Technology Corporation, Charlottesville, VA; A. Ghoshal, M. Center, Moffett Field, CA; S. Schery, Natsui, J. Kapat, University of Central Aberdeen Proving Ground, MD; K. Kerner, Tullahoma, TN Dayton, OH Pepi, Army Research Laboratory, K. Long, Aerospace Computing, Inc., Florida, Orlando, FL Army Aviation and Missile Research Aberdeen Proving Ground, MD; Y. Liu, A. Mountain View, CA Development and Engineering Center, Chattopadhyay, Arizona State University, Fort Eustis, VA; D. Booth, Army Research Tempe, AZ; A. Goff, Luna Innovations, Inc., Laboratory, Aberdeen Proving Ground, MD Charlottesville, VA; et al. Wednesday, 29 July 2015 145-GTE-13 AIAA Undergraduate Engine Design Competition Lake Highland B 1500 - 1800 hrs Chaired by: J. TAI, Georgia Institute of Technology AIAA Foundation and the Gas Turbine Engine Technical Committee have again teamed up to sponsor a design competition. Undergraduate students from universities all over the world were asked to prepare a design report to respond to a Request for Proposal (RFP). This RFP asked students to design an ultra-high bypass turbofan engine. All of the responses have been reviewed and ranked by technical experts, and this session features the top three proposals, who have been invited to the AIAA Propulsion and Energy Forum to make an oral presentation to a panel of judges. These judges will assess the design, presentation, and responses to questions. They will add their scores to those provided by the technical judges to come up with a final 1st-3rd place ranking. The final rankings will be announced at the conclusion of the session. 77 Wednesday, 29 July 2015 146-HR-10 Design Studies Including Cost and Feasibility Analysis II Lake Sheen B Chaired by: B. MADHANABHARATAM, Aerospace Consultant and B. EVANS, Stanford University 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-4199 AIAA-2015-4200 AIAA-2015-4201 AIAA-2015-4202 AIAA-2015-4203 Verification Firings of End-burning Hybrid Propulsion In-Situ Resource Continued Testing of the High A Straightfotward Approach for Genetic Algorithm Optimization of Type Hybrid Rockets Utilization Test Facility Results Performance Hybrid Propulsion Robust Design of Hybrid Rocket a Cost Competitive Hybrid Rocket H. Nagata, H. Teraki, Y. Saito, R. Kanai, A. Karp, B. Nakazono, D. Vaughan, System for Small Satellites Engine Upper Stage Booster Hokkaido University, Sapporo, Japan; H. W. Warner, Jet Propulsion Laboratory, L. Simurda, Stanford University, Stanford, L. Casalino, D. Pastrone, Technical G. Story, NASA Marshall Space Flight Yasukochi, University of Tokyo, Tokyo, California Institute of Technology, CA; G. Zilliac, NASA Ames Research Center, University of Turin, Turin, Italy Center, Huntsville, AL Japan; M. Wakita, Hokkaido University, Pasadena, CA Moffett Field, CA Sapporo, Japan; et al. Wednesday, 29 July 2015 147-HSABP-7 High Fidelity Simulations of High-Speed Air Breathing System Lake George A Chaired by: T. OBRIEN, Aerojet and V. TANGIRALA, General Electric 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-4204 AIAA-2015-4205 AIAA-2015-4206 AIAA-2015-4207 Modeling of Turbulence in a Turbulence Model Modification for Preliminary Investigation of LES Model Assessment for High Supersonic Wall Cavity Fake Amplification of Turbulence Unstart-Related Transients in a Speed Combustion using Mesh- D. Peterson, Innovative Scientific Kinetic Energy by Shock-Turbulence Dual-Mode Scramjet Sequenced Realizations Solutions, Inc., Dayton, OH; E. Hassan, Interation L. Riley, D. Gaitonde, Ohio State C. Patton, T. Wignall, H. Mirgolbabaei, J. Air Force Research Laboratory, Wright- Z. Zhang, Z. Gao, C. Jiang, C. Lee, University, Columbus, OH; J. Donbar, Edwards, T. Echekki, North Carolina State Patterson AFB, OH Beihang University, Beijing, China Air Force Research Laboratory, Wright- University, Raleigh, NC Patterson AFB, OH Wednesday, 29 July 2015 148-LP-19 Combustion Dynamics II Lake Lucerne Chaired by: D. LINEBERRY, UAH Propusion Research Center and S. SCHUMAKER, Air Force Reseach Laboratory 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-4208 AIAA-2015-4209 AIAA-2015-4210 AIAA-2015-4211 System Analysis of Low Frequency Investigation of Combustion Control Transverse Combustion Instability Triggering and Re-Stabilization of Combustion Instabilities in Liquid in a Dump Combustor Using the in a Rectangular Rocket Motor Combustion Instability with Rocket Rocket Engines Feedback Free Fluidic Oscillator P. Popov, W. Sirignano, University of Motor Acceleration M. Leonardi, University of Rome “La E. Meier, Purdue University, West California, Irvine, Irvine, CA P. Popov, A. Sideris, W. Sirignano, Sapienza”, Rome, Italy; F. Di Matteo, Lafayette, IN; M. Casiano, NASA Marshall University of California, Irvine, Irvine, CA J. Steelant, ESA, Noordwijk, The Space Flight Center, Huntsville, AL; W. Netherlands; F. Nasuti, M. Onofri, Anderson, S. Heister, Purdue University, University of Rome “La Sapienza”, West Lafayette, IN Rome, Italy Wednesday, 29 July 2015 149-LP-20 Propellant Feed Systems & Fluid Machinery Lake Highland A Chaired by: B. MARCU, Space Exploration Technologies Corporation and J. LOCKE, United Technologies Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-4212 AIAA-2015-4213 AIAA-2015-4214 AIAA-2015-4215 AIAA-2015-4216 Simulation of Rocket-Grade Sounding Rocket Experiment on Two-Phase Flow Modelling Of The Towards Physics Based Autonomous Design and Analysis of a High- Kerosene Flowing In An Electrically Chill-down Process with Liquid Cryogenic Propellant Loading Control Of The Cryogenic Propellant Pressure Turbopump at Purdue Heated Experimental Apparatus Nitrogen in a Complex Channel System Loading System University A. Himansu, M. Billingsley, Air Force W. Sarae, K. Kinefuchi, D. Yabusaki, D. Luchinsky, Mission Critical Technologies, E. Ponizovskaya-Devine, Stinger Ghaffarian D. Stechmann, C. Sese, R. Duvvur, Y.

78 Research Laboratory, Edwards AFB, CA D. Sugimori, T. Fujita, K. Okita, Japan Inc., El Segundo, CA; E. Ponizovskaya- Technologies, Inc., Greenbelt, MD; D. Huang, M. Bilyeu, D. Goldberg, Purdue Aerospace Exploration Agency (JAXA), Devine, M. Khasin, Stinger Ghaffarian Luchinsky, Mission Critical Technologies, University, West Lafayette, IN; et al. Tsukuba, Japan; et al. Technologies, Inc., Greenbelt, MD; A. Inc., El Segundo, CA; M. Khasin, Stinger Kodali, NASA Goddard Space Flight Center, Ghaffarian Technologies, Inc., Greenbelt, Greenbelt, MD; J. Perotti, J. Sass, NASA MD; J. Perotti, J. Sass, B. Brown, NASA Kennedy Space Center, Cape Canaveral, Kennedy Space Center, Cape Canaveral, FL FL; et al. Wednesday, 29 July 2015 150-LP-21 Rocket Nozzles II Orange E Chaired by: P. GLOYER, Gloyer-Taylor Laboratory and S. BARSI, NASA 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-4217 AIAA-2015-4218 AIAA-2015-4219 AIAA-2015-4220 A Complete and Robust Approach Separation Shock Cutoff Frequency Numerical Investigation of Flow Suppressing Restricted Shock to Axisymmetric Method of in Dual Bell Nozzles Transition Behavior in Cold Flow Separation in Thrust-Optimized Characteristics for Nozzle Design E. Martelli, Second University of Naples, Dual Bell Rocket Nozzles Rocket Nozzles Using Contour R. Hartfield, J. Burkhalter, Auburn Aversa, Italy; B. Betti, F. Nasuti, University D. Schneider, C. Genin, German Aerospace Geometry University, Auburn, AL of Rome “La Sapienza”, Rome, Italy Center (DLR), Lampoldshausen, Germany K. Schomberg, J. Olsen, University of New South Wales, Sydney, Australia; A. Neely, University of New South Wales at the Australian Defence Force Academy, Canberra, Australia; G. Doig, California Polytechnic State University, San Luis Obispo, CA Wednesday, 29 July 2015 151-LP-22/ PGC-1/ PC-12 Pressure Gain Combustion for Liquid Propulsion Orange F 1500 - 1800 hrs In this session, speakers are invited to provide the results of their studies and recommendations regarding Pressure Gain Combustion (PGC) for rocket applications. The covered topics include university level research and industry level development from domestic and international efforts.

Moderators: Steven Stanley, Aerojet Rocketdyne and Shane Coogan, Southwest Research Institute Panelists: Prof. Steven Heister Dr. Greg Meholic Prof. J.P. Wang Dr. Scott Claflin Prof. Jiro Kasahara Dr. Richard D. Smith Purdue University, USA The Aerospace Corporation Peking University Aerojet-Rocketdyne, USA Nagoya University, Japan GHKN Engineering, USA “Rocket Applications of PGC- An “Potential Applications of RDE Technology “Recent Progress on Continuously Rotating “Development of Rotating Detonation “500-N Class Rotating Detonation Rocket “Experimental Investigation of CDRE’s for Introduction.” in Liquid Rocket Engines”. Detonation Engine at Peking University”. Engine Technology for Rocket Propulsion Engine Experiment and Sounding Rocket In Space Propulsion.” Systems at Aerojet Rocketdyne” Flight Test Program.”

Wednesday, 29 July 2015 152-PC-13 Propellants and Fuels III Lake Louise Chaired by: T. NGUYEN, Aerojet Rocketdyne and C. BROPHY, Naval Postgraduate School 1500 hrs 1530 hrs 1600 hrs AIAA-2015-4221 AIAA-2015-4222 AIAA-2015-4223 Enhancing Micrometric Aluminum Characterization of Solid Combustion Behavier of a High Reactivity by Mechanical Activation Propellants Based On ADN and GAP Burning Rate AP-HTPB Solid S. Dossi, C. Paravan, F. Maggi, L. Galfetti, N. Wingborg, Swedish Defense Research Propellant under Transient Pressure Technical University of Milan, Milan, Italy Agency (FOI), Stockholm, Sweden Condition 79 L. Shipeng, N. Wang, Beijing Institute of Technology, Beijing, China Wednesday, 29 July 2015 153-PC-14 Rocket Motor Studies Lake Concord B Chaired by: M. COIL, Orbital Technologies Corporation 1500 hrs 1530 hrs 1600 hrs AIAA-2015-4224 AIAA-2015-4225 AIAA-2015-4226 An Experimental Investigation of Study of Alunima Flow in a Diagnostic Investigation of Flame Sheet Velocity and Jet Diameter propulsion Chamber Spread Mechanism in Dual-thrust Assumptions of Non-Newtonian R. Amano, University of Wisconsin, Solid Propellant Rocket Motors Impinging Jets Milwaukee, Glendale, WI S. Ajith, S. Mani, R. Tharikaa, H. Nagaraju P. Collins, J. Mallory, Western New Doddi, V. Sanal Kumar, Kumaraguru England University, Springfield, MA College of Technology, Coimbatore, India Wednesday, 29 July 2015 154-PC-15 Combustion Dynamics Experiments and Control Lake Virginia Chaired by: A. STEINBERG, University of Toronto 1500 hrs 1530 hrs 1600 hrs AIAA-2015-4227 AIAA-2015-4228 AIAA-2015-4229 Concurrent Experimental and Oxidizer Post Resonance Response Effect of Acoustic Oscillations on the Computational Study of Combustion of a High Pressure Combustor Upstream Mixing Layer of Triple Dynamics in a Single-Element Lean M. Wierman, W. Hallum, W. Anderson, Flames Direct Injection (LDI) Gas Turbine Purdue University, West Lafayette, IN; B. M. Saito, N. Sugiu, K. Motohashi, M. Combustor Austin, IN Space, LLC, West Lafayette, IN Tanabe, Nihon University, Funabashi, R. Gejji, C. Huang, R. Lucht, W. Anderson, Japan Purdue University, West Lafayette, IN Wednesday, 29 July 2015 155-SC-2 Seal Material Advancements and Advanced Seal Technology Lake George B Chaired by: N. SARAWATE, GE Global Research and P. DUNLAP, NASA Glenn Research Center 1500 hrs 1530 hrs AIAA-2015-4230 AIAA-2015-4231 Aspects of Brush Seal Design Leak Rate Quantification Method A. Bowsher, P. Crudgington, T. Kirk, R. for Gas Pressure Seals with Chupp, Cross Manufacturing Company, Controlled Pressure Differential Ltd., Devizes, United Kingdom C. Daniels, M. Braun, H. Oravec, J. Mather, University of Akron, Akron, OH; S. Taylor, University of Toledo, Toledo, OH 80 Wednesday, 29 July 2015 156-SR-6/HSABP-8 Solid Propellant Ducted Rockets Lake Mizell B Chaired by: K. NAUMANN, Bayern-Chemie GmbH and F. MALO-MOLINA, Raytheon Missile Systems 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-4232 AIAA-2015-4233 AIAA-2015-4234 AIAA-2015-4235 AIAA-2015-4236 Development and Testing of a C/ Air Intake Development for a Mach Performance Assessment for Effects of Mg-Al Particle Additions Gas Generator Pressure Control SiC Combustion Chamber for High 5+ Throttleable Ducted Rocket a Throttleable Ducted Rocket on Combustion Characteristics of in Throttleable Ducted Rockets: Speed Throttleable Ducted Rocket Propelled Lower Tier Interceptor Powered Lower Tier Interceptor Ducted Rockets A Classical and Adaptive Control Applications G. Kurth, C. Bauer, Bayern-Chemie, Aschau G. Kurth, C. Bauer, N. Hopfe, Bayern- N. Negishi, T. Kuwahara, Nihon University, Approach G. Kurth, C. Bauer, T. Meyer, J. Ramsel, am Inn, Germany Chemie, Aschau am Inn, Germany Funabashi, Japan A. Alan, Y. Yildiz, Bilkent University, A. Thumann, Bayern-Chemie, Aschau am Ankara, Turkey; U. Poyraz, ROKETSAN Inn, Germany Missile Industries, Inc., Ankara, Turkey Wednesday, 29 July 2015 157-SR-7 Solid Rocket Motor Propellant Modeling and Simulation Lake Concord A Chaired by: A. NERI and H. CIEZKI, DLR - German Aerospace Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-4237 AIAA-2015-4238 AIAA-2015-4239 AIAA-2015-4240 AIAA-2015-4241 AIAA-2015-4242 Random Close Packing Modeling Lifetime Numerical Prediction of Numerical Simulation Of Luminous Accelerated Aging and Structural Feasibility Analysis for Long-term Impact of Phase transitions on the and evaluation of a Castability Solid Rocket Motors with HTPB Flame Around Ignited Aluminum Integrity Analysis Approach to Non-turnover Storage of Solid Flow Structure of Gaseous Jets Margin for Solid Propellants Binder Based Propellants Using a Particle Near Burning Surface Predict the Service Life of Solid Rocket Motors Injected into Water D. Fedele, F. Ponti, R. Bertacin, University Multiscale Model Of Composite Propellant With Rocket Motor W. Ma, X. Sui, R. Lei, L. Shipeng, N. X. Zhang, Y. Tang, Beijing Institute of of Bologna, Forlì, Italy B. Dalby, A. Caraës, DGA, Saint-Médard-en- Changing Pressure D. Zhou, X. Liu, X. Sui, Z. Wei, N. Wang, Wang, Beijing Institute of Technology, Technology, Beijing, China; J. Tang, China Jalles, France K. Takahashi, Nihon University, Funabashi, Beijing Institute of Technology, Beijing, Beijing, China North Industries Group Corporation, Japan; T. Shimada, Japan Aerospace China Beijing, China; L. Shipeng, N. Wang, Exploration Agency (JAXA), Sagamihara, Beijing Institute of Technology, Beijing, Japan China Wednesday, 29 July 2015 158-TM-5 Thermal System Applications and Unique Environment II Lake Down A Chaired by: E. KHALIL, Cairo University and C. TARAU, Advanced Cooling Technologies 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2015-4243 AIAA-2015-4244 AIAA-2015-4245 AIAA-2015-4246 AIAA-2015-4247 AIAA-2015-4248 Design of the Ventilation System Experimental study on effect Various Integrated Aerospace Experiment Design for Measuring Liquefied Natural Gas as the Next Developing an All-speed Finite in an Underground Car Park: Local of pyrolysis on heat transfer of Systems for a Cryogenic Based Accommodation Coefficients Aviation Fuel Volume Method to Predict Short Mean Age of Air n-decane at different pressure Directed Energy Weapon for Modeling of Long-Duration R. Roberts, S. Nuzum, M. Wolff, Wright Duration Pressure Peaks of Water S. Gomaa, M. Fouad, Cairo University, W. Zhou, W. Yu, Z. Jia, S. Lin, Harbin S. Nuzum, R. Roberts, M. Wolff, Wright Spaceflight Cryogenic Propellants State University, Dayton, OH Column Separation 81 Giza, Egypt; A. Fahim, Housing and Institute of Technology, Harbin, China State University, Dayton, OH S. Alberts, P. Srikanth, S. Collicott, S. M. Darbandi, A. Beige, Sharif University Building National Research Center, Giza, Heister, Purdue University, West Lafayette, of Technology, Tehran, Iran (the Islamic Egypt; E. Khalil, Cairo University, Giza, IN Republic of); G. Schneider, University of Egypt Waterloo, Waterloo, Canada Wednesday, 29 July 2015 159-VS-1 Advanced Vehicle System Concepts Lake Down B Chaired by: F. CHANDLER, Boeing Defense, Space & Security and T. CHEN, NASA 1500 hrs 1530 hrs AIAA-2015-4249 AIAA-2015-4250 Design and Construction of an Heliopause Electrostatic Rapid Astronaut Assistance Martian Rover Transit System (HERTS) [Electric for the University Rover Challenge Saill] T. Bernard, A. Alvarez Rolins, S. B. Wiegmann, NASA Marshall Space Flight Chintalapati, Florida Institute of Center, Huntsville, AL Technology, Melbourne, FL Wednesday, 29 July 2015 160-F360-6 Advancing Engineering Through Effective Communication with the Media Orlando IV 1530 - 1800 hrs Sooner or later, most engineers will end up talking to a reporter. Learn how to interact more effectively with and through the media, how to make engineering more relevant to the general public, how public perception through the media effects the aerospace industry and why interacting with the media matters. Learn how to make the most of this opportunity to help yourself and your profession. Bring your hardest-hitting questions to this panel of media experts as they discuss their trade.

Moderator: Victor Beck, Northrop Grumman Corporation Panelists: Marcia Dunn Michael Curie Scott Powers William Harwood William Allen Cape Canaveral Correspondent, Associated Press NASA Kennedy Space Center Orlando Sentinel CBS News Florida Southern College 82 Author / Session Chair Index Abd Elatif, O., 7-EE-1 Aulisio, M., 61-APS-2 Bertacin, R., 68-GTE-5, 157-SR-7 Cadou, C., 77-PC-5, 115-ABPSI-4/AEP-2 Chintalapati, S., 159-VS-1 Abreu, D., 76-PAW-3 Austin, B., 73-LP-11, 99-ITAR-2, 154-PC-15 Besnard, E., 128-LP-18 Caffrey, J., 74-NFF-3 Choi, G., 39-HR-2 Addona, B., 142-EP-10 Axdahl, E., 124-HSABP-4 Betti, B., 16-LP-2, 150-LP-21 Cai, C., 65-EP-5 Choi, H., 48-PC-3 Adriany, K., 102-LP-14 Ayad, S., 7-EE-1 Bially, E., 36-EE-2, 51-TM-2, 106-PC-8 Cai, G., 39-HR-2 Choi, M., 26-TM-1, 51-TM-2, 81-TM-3 Agui, J., 103-LP-15 Babcock, D., 76-PAW-3 Bianchi, D., 16-LP-2, 40-HR-3, 135-SR-5 Calhoon, W., 16-LP-2 Choi, S., 49-PC-4 Ahamed, S., 93-GTE-6 Badawiyeh, M., 36-EE-2 Billingsley, M., 149-LP-20 Cano, J., 63-ECS-2 Choijil, B., 35-EDU-1 Ahmed, A., 106-PC-8 Bae, D., 128-LP-18 Bilyeu, M., 149-LP-20 Cantwell, B., 39-HR-2, 122-HR-8 Chopinet, J., 101-LP-13 Ahmed, K., 68-GTE-5, 93-GTE-6, 106-PC-8, Bae, S., 128-LP-18 Birchenough, A., 61-APS-2, 65-EP-5 Cao, D., 106-PC-8 Chou, T., 98-HR-7, 123-HR-9 107-PC-9, 133-PP-1 Baglini, J., 6-ECS-1, 63-ECS-2 Blachowski, T., 63-ECS-2 Caraës, A., 157-SR-7 Choudhuri, A., 99-ITAR-2 Ahmed, L., 121-GTE-9 Baisden, A., 61-APS-2 Blakey, S., 125-HSABP-5/GTE-10 Cardiff, E., 37-EP-3, 72-LP-10, 87-APC-2 Choueiri, E., 9-EP-2, 90-EP-7 Ahmed, M., 135-SR-5 Balchanos, M., 89-ED-2/EE-4 Blanchard, C., 117-EDU-2 Carlson, J., 95-GTE-8 Chowdhury, S., 98-HR-7 Ahmed, O., 96-HR-5 Baldwin, R., 25-ST-1 Boiocchi, M., 97-HR-6 Carmicino, C., 40-HR-3 Christiansen, M., 47-PAW-2, 58-ABPSI-3 Ahmed, S., 92-FFP-2 Ballinger, I., 126-LP-16 Boiron, A., 98-HR-7 Carr, J., 61-APS-2 Chuck, C., 21-PAW-1, 76-PAW-3 Ahuja, V., 45-LP-8, 126-LP-16 Balmogim, U., 98-HR-7 Bolat, H., 23-PC-2 Carter, C., 105-PC-7 Chung, J., 134-SC-1 Ajith, S., 135-SR-5, 153-PC-14 Bane, S., 143-GTE-11/HSABP-6 Bonhomme, C., 101-LP-13 Casalino, L., 146-HR-10 Chung, Y., 17-LP-3 Ajmani, K., 23-PC-2 Bao, W., 70-HSABP-3 Booth, D., 67-GTE-4, 144-GTE-12 Casiano, M., 148-LP-19 Chupp, R., 155-SC-2 Akashi, N., 142-EP-10 Baral, A., 100-LP-12 Borowski, S., 19-NFF-1, 74-NFF-3 Cassenti, B., 46-NFF-2 Ciezki, H., 157-SR-7 Akiki, M., 107-PC-9 Baran, A., 117-EDU-2 Boss, M., 8-EP-1 Cassibry, J., 46-NFF-2 Claflin, S., 39-HR-2 Aktas, D., 59-AEP-1 Baran, Ö., 32-ABPSI-2 Bossard, J., 70-HSABP-3 Cassidy, J., 61-APS-2 Cofer, A., 87-APC-2, 142-EP-10 Alan, A., 156-SR-6/HSABP-8 Barato, F., 40-HR-3 Botha, J., 35-EDU-1 Castonguay, K., 102-LP-14 Coil, M., 153-PC-14 Alberto Gurgel Veras, C., 69-HR-4 Barber, T., 44-LP-7 Bouldin, B., 26-TM-1 Catina, J., 102-LP-14 Coll, G., 72-LP-10, 103-LP-15 Alberts, S., 158-TM-5 Barnett, B., 144-GTE-12 Bowsher, A., 155-SC-2 Cavallini, E., 79-SR-3 Collicott, S., 158-TM-5 Alcántara, F., 89-ED-2/EE-4 Barnhart, P., 4-ABPSI-1 Boyer, J., 96-HR-5 Cavillon, R., 16-LP-2 Collins, E., 116-APS-3 83 Alexeenko, A., 87-APC-2, 142-EP-10 Barragan, J., 99-ITAR-2 Bozak, K., 61-APS-2, 65-EP-5 Cecil, O., 13-HR-1, 24-SR-1, 44-LP-7 Collins, J., 33-ECD-1 Ali, H., 140-ECD-4 Barsi, S., 127-LP-17, 150-LP-21 Brady, B., 97-HR-6 Celik, M., 37-EP-3, 66-EP-6 Collins, P., 153-PC-14 Ali, M., 7-EE-1 Baskaran, S., 93-GTE-6 Braman, K., 127-LP-17 Cetegen, B., 22-PC-1 Connell, T., 78-PC-6 Allen, B., 50-SR-2 Bassiony, M., 92-FFP-2 Brand, A., 15-LP-1, 86-AEC-1 Chakraborty, I., 115-ABPSI-4/AEP-2 Connolly, J., 86-AEC-1, 95-GTE-8, Alliot, P., 72-LP-10, 101-LP-13 Batista de Jesus, A., 76-PAW-3 Braun, M., 155-SC-2 Chamayou, B., 63-ECS-2 125-HSABP-5/GTE-10 ALsenbawy, M., 135-SR-5 Batterson, J., 24-SR-1, 42-LP-5 Braun, R., 140-ECD-4 Chan, T., 62-ECD-2 Coogan, S., 16-LP-2, 69-HR-4, 103-LP-15, 122-HR-8, Alvarez Rolins, A., 159-VS-1 Battista, F., 44-LP-7 Breisacher, K., 45-LP-8 Chandler, F., 159-VS-1 151-LP-22/ PGC-1/ PC-12 Aly Hassan, M., 106-PC-8 Baturin, O., 121-GTE-9 Brinckman, K., 17-LP-3 Chang, H., 98-HR-7 Coote, D., 19-NFF-1 Amadio, G., 107-PC-9 Bauer, C., 156-SR-6/HSABP-8 Briot, D., 25-ST-1 Chang, J., 14-HSABP-1, 70-HSABP-3 Copenhaver, W., 71-ITAR-1 Amano, R., 153-PC-14 Bayat, E., 102-LP-14 Brooks, M., 7-EE-1, 69-HR-4, 95-GTE-8, 98-HR-7 Chap, A., 46-NFF-2 Corrigan, A., 22-PC-1 Amrousse, R., 49-PC-4 Beck, G., 18-LP-4 Brophy, C., 152-PC-13 Charles, P., 116-APS-3 Cortopassi, A., 96-HR-5 An, Q., 105-PC-7 Behbahani, A., 86-AEC-1 Brown, B., 149-LP-20 Charneski, J., 22-PC-1 Cosentino, G., 97-HR-6 Anand, M., 23-PC-2 Behruzi, P., 128-LP-18 Brown, G., 59-AEP-1 Chattopadhyay, A., 144-GTE-12 Cox, J., 35-EDU-1, 144-GTE-12 Anderson, C., 11-GTE-1 Beige, A., 158-TM-5 Buckley, J., 117-EDU-2 Chehroudi, B., 78-PC-6 Crapuchettes, J., 142-EP-10 Anderson, P., 5-APS-1 Bell, M., 33-ECD-1 Bucknell, J., 74-NFF-3 Chen, G., 16-LP-2 Crawford, B., 81-TM-3 Anderson, W., 42-LP-5, 81-TM-3, 131-PC-10, Bemish, R., 66-EP-6 Budica, R., 46-NFF-2 Chen, H., 12-GTE-2, 21-PAW-1, 32-ABPSI-2 Crofton, M., 8-EP-1, 65-EP-5 148-LP-19, 154-PC-15 Bemont, C., 7-EE-1 Bulman, M., 19-NFF-1 Chen, J., 68-GTE-5, 124-HSABP-4 Crowley, J., 74-NFF-3 Andrianov, A., 69-HR-4 Benhidjeb-Carayon, A., 15-LP-1 Bunget, G., 144-GTE-12 Chen, L., 133-PP-1 Crudgington, P., 155-SC-2 Antequera, C., 89-ED-2/EE-4 Benker, D., 116-APS-3 Burchett, J., 63-ECS-2 Chen, T., 159-VS-1 Csank, J., 86-AEC-1, 94-GTE-7 Anusonti-Inthra, P., 35-EDU-1, 144-GTE-12 Bennewitz, J., 117-EDU-2 Burkhalter, J., 150-LP-21 Chen, Y., 17-LP-3, 43-LP-6, 96-HR-5, 98-HR-7, Dahl, D., 58-ABPSI-3 Aranyos, T., 72-LP-10 Berdoyes, M., 135-SR-5 Burkhardt, W., 142-EP-10 123-HR-9, 126-LP-16 Daimon, Y., 16-LP-2, 42-LP-5 Arnold, S., 35-EDU-1, 144-GTE-12 Berens, T., 32-ABPSI-2 Burrow, G., 81-TM-3 Cheng, L., 125-HSABP-5/GTE-10 Dalby, B., 157-SR-7 Arrington, L., 15-LP-1 Berg, S., 66-EP-6, 142-EP-10 Burt, J., 37-EP-3 Cheng, R., 98-HR-7 Damiao, A., 93-GTE-6 Arthur, N., 8-EP-1 Bernard, T., 159-VS-1 Busari, O., 15-LP-1 Chianese, S., 17-LP-3, 43-LP-6 Daniels, C., 99-ITAR-2, 155-SC-2 Atyam, D., 102-LP-14 Berry, M., 71-ITAR-1 Butt, A., 117-EDU-2 Chicatelli, A., 86-AEC-1 Dankanich, J., 9-EP-2, 37-EP-3, 104-NFF-4 Author / Session Chair Index Darbandi, M., 10-FFP-1, 158-TM-5 Duraisamy, K., 86-AEC-1 Fraeman, M., 33-ECD-1 Glauser, M., 71-ITAR-1 Harribey, D., 90-EP-7 Darr, S., 134-SC-1 Dutheil, J., 120-GE-1 Franke, A., 8-EP-1 Glorieux, G., 8-EP-1 Harsh, K., 86-AEC-1 Dasque, N., 41-HSABP-2 Duvvur, R., 149-LP-20 Frankford, D., 33-ECD-1 Gloyer, P., 127-LP-17, 150-LP-21 Hartfield, R., 121-GTE-9, 150-LP-21 Davidson, C., 87-APC-2 Echekki, T., 41-HSABP-2, 147-HSABP-7 Frederick, R., 35-EDU-1, 43-LP-6, 96-HR-5, Goebel, D., 90-EP-7 Hartman, J., 35-EDU-1 Davidson, J., 50-SR-2 Edwards, J., 41-HSABP-2, 147-HSABP-7 108-SR-4, 117-EDU-2 Goff, A., 144-GTE-12 Hartwig, J., 134-SC-1 Davis, D., 4-ABPSI-1 Eguchi, T., 105-PC-7 French, A., 16-LP-2 Gogineni, S., 71-ITAR-1 Harvazinski, M., 42-LP-5 Davitian, J., 97-HR-6, 123-HR-9 Ehlen, J., 122-HR-8 Frezzotti, M., 42-LP-5 Goldberg, B., 50-SR-2 Hashimoto, T., 101-LP-13 Deans, M., 15-LP-1, 126-LP-16 Eldegwy, A., 36-EE-2 Fries, N., 128-LP-18 Goldberg, C., 94-GTE-7 Hassan, E., 147-HSABP-7 Dechent, W., 8-EP-1 Elgergawi, M., 92-FFP-2 Frohnapfel, D., 32-ABPSI-2 Goldberg, D., 149-LP-20 Hasti, V., 105-PC-7 de Frutos, V., 89-ED-2/EE-4 ElHaroun, A., 51-TM-2 Fujita, T., 149-LP-20 Goldstein, S., 63-ECS-2 Hatai, K., 49-PC-4 Delange, J., 101-LP-13 Elias de Morais Bertoldi, A., 69-HR-4 Fukuchi, A., 108-SR-4 Gollahalli, S., 92-FFP-2 Hatfield, M., 115-ABPSI-4/AEP-2 de la Vergne, P., 117-EDU-2 Elisii, R., 62-ECD-2 Fuller, J., 96-HR-5 Gollor, M., 8-EP-1 Hausen, R., 106-PC-8 Delgado, J., 8-EP-1 Elliott, T., 13-HR-1 Fulton, J., 70-HSABP-3 Gomaa, S., 26-TM-1, 158-TM-5 Havakechian, S., 94-GTE-7 Delot, A., 21-PAW-1, 76-PAW-3 Elmaghraby, H., 36-EE-2 Funaki, I., 9-EP-2, 107-PC-9 Gonçalves, R., 49-PC-4 Hay, R., 81-TM-3 Demko, A., 78-PC-6, 108-SR-4 El-Nady, A., 135-SR-5 Fureby, C., 41-HSABP-2, 93-GTE-6 Gonthier, K., 6-ECS-1 Hayashi, D., 123-HR-9 Deng, Z., 87-APC-2 Emrich, W., 19-NFF-1 Gabl, J., 99-ITAR-2 Gonzalez, D., 94-GTE-7 Hedayat, A., 74-NFF-3, 117-EDU-2 Denny, M., 108-SR-4, 117-EDU-2 Escher, D., 60-APC-1 Gaitonde, D., 147-HSABP-7 Gonzalez, E., 77-PC-5 Heimdal Nilsson, E., 93-GTE-6 De Quero, A., 126-LP-16 Evans, B., 40-HR-3, 122-HR-8, 146-HR-10 Galfetti, L., 97-HR-6, 152-PC-13 Gonzalez, G., 50-SR-2 Heister, S., 17-LP-3, 48-PC-3, 87-APC-2, 148-LP-19, Dermanci, O., 123-HR-9 Eveleigh, T., 89-ED-2/EE-4 Gallagher, T., 107-PC-9 Gonzalez, I., 76-PAW-3 158-TM-5 Desain, J., 96-HR-5, 97-HR-6 Eyi, S., 14-HSABP-1, 26-TM-1, 51-TM-2, 80-ST-2 Gallego, M., 26-TM-1 Gonzalez, M., 61-APS-2 Henaux, C., 90-EP-7 de Swardt, J., 35-EDU-1 Fabisinski, L., 61-APS-2 Gan, J., 68-GTE-5 Gord, J., 105-PC-7 Henderson, E., 60-APC-1 Dextre, R., 9-EP-2 Faenza, M., 98-HR-7 Gang, L., 132-PC-11 Gore, J., 48-PC-3, 105-PC-7 Hendrich, C., 120-GE-1

84 Di Clemente, M., 98-HR-7 Fahim, A., 51-TM-2, 158-TM-5 Ganguli, R., 115-ABPSI-4/AEP-2 Goryachkin, E., 121-GTE-9 Hernanz, J., 26-TM-1 Dillier, C., 78-PC-6, 108-SR-4 Farag, A., 120-GE-1 Gao, Z., 147-HSABP-7 Gotzig, U., 128-LP-18 Herrmann, J., 101-LP-13 DiMare, F., 23-PC-2 Farnell, C., 90-EP-7 Garner, C., 8-EP-1 Gourdain, N., 94-GTE-7 Hickman, R., 19-NFF-1 Di Mascio, A., 79-SR-3 Farokhi, S., 124-HSABP-4 Gatto, C., 134-SC-1 Grant, G., 72-LP-10 Hidalgo, V., 32-ABPSI-2 Di Matteo, F., 148-LP-19 Favini, B., 79-SR-3 Gaulke, D., 128-LP-18 Greatrix, D., 40-HR-3 Hill, D., 33-ECD-1, 62-ECD-2 Dobson, R., 26-TM-1 Fearn, H., 104-NFF-4 Gautier, S., 76-PAW-3 Grech, N., 21-PAW-1 Himansu, A., 149-LP-20 Doi, R., 108-SR-4 Fedele, D., 157-SR-7 Gaworski, K., 78-PC-6 Grey, Z., 12-GTE-2 Himeno, T., 45-LP-8, 59-AEP-1 Doig, G., 150-LP-21 Fedina, E., 93-GTE-6 Gazaix, M., 94-GTE-7 Griffiths, R., 68-GTE-5 Hirt, S., 115-ABPSI-4/AEP-2 Domel, N., 21-PAW-1, 76-PAW-3 Felder, J., 59-AEP-1 Gea, L., 76-PAW-3 Guadagnoli, D., 102-LP-14 Hitt, M., 35-EDU-1, 96-HR-5 Domenech, J., 89-ED-2/EE-4 Feldman, G., 17-LP-3 Geikie, M., 106-PC-8 Guan, H., 22-PC-1 Hobbs, R., 116-APS-3 Donahue, B., 99-ITAR-2 Feldman, M., 9-EP-2, 66-EP-6 Gejji, R., 154-PC-15 Guegan, D., 94-GTE-7 Hochheimer, B., 100-LP-12 Donbar, J., 147-HSABP-7 Felker, L., 116-APS-3 Genevieve, B., 98-HR-7 Guerin, S., 102-LP-14 Hodges, J., 11-GTE-1, 144-GTE-12 Donnerhack, S., 95-GTE-8 Ferguson, D., 143-GTE-11/HSABP-6 Genin, C., 127-LP-17, 150-LP-21 Guinet, C., 68-GTE-5 Hofer, R., 8-EP-1, 90-EP-7 Donovan, A., 134-SC-1 Ferguson, F., 41-HSABP-2 Geraedts, B., 105-PC-7 Gümmer, V., 68-GTE-5 Holicker, C., 64-EE-3 Dossi, S., 152-PC-13 Fernandes, C., 144-GTE-12 Gerards, A., 108-SR-4 Gur, H., 26-TM-1 Holman, T., 66-EP-6 Doughty, G., 19-NFF-1 Fernandes, R., 11-GTE-1 Gernoth, A., 100-LP-12 Gutierrez, H., 103-LP-15 Hopfe, N., 156-SR-6/HSABP-8 Dowdy, M., 126-LP-16 Fernando, P., 25-ST-1 Gerrish, H., 19-NFF-1 Gutmark, E., 125-HSABP-5/GTE-10 Hori, K., 49-PC-4 Drennan, S., 12-GTE-2 Fischer, D., 15-LP-1 Ghaddar, N., 7-EE-1, 36-EE-2 Haemmerli, B., 98-HR-7 Horisawa, H., 142-EP-10 Driscoll, J., 14-HSABP-1, 70-HSABP-3, 86-AEC-1, Fisher, S., 134-SC-1 Ghafourizadeh, M., 10-FFP-1 Haidn, O., 18-LP-4 Hornick, J., 24-SR-1 105-PC-7 Fittje, J., 19-NFF-1 Ghali, K., 7-EE-1, 36-EE-2 Haines, J., 116-APS-3 Horton, J., 18-LP-4 Du, J., 22-PC-1 Fitzgerald, D., 95-GTE-8 Ghoddoussi, A., 115-ABPSI-4/AEP-2 Hallum, W., 154-PC-15 Hosangadi, A., 16-LP-2, 17-LP-3 Du, M., 116-APS-3 Flegel, A., 67-GTE-4 Ghoshal, A., 144-GTE-12 Hamley, J., 116-APS-3 Hosoda, S., 8-EP-1 Duffy, K., 59-AEP-1 Font, G., 37-EP-3 Gianvito, A., 97-HR-6 Hammack, S., 105-PC-7 Hosokawa, H., 142-EP-10 Dugala, G., 33-ECD-1 Foster, J., 8-EP-1, 65-EP-5 Giel, T., 18-LP-4, 134-SC-1 Han, B., 64-EE-3 Hou, A., 12-GTE-2 Duncan, S., 89-ED-2/EE-4 Fouad, M., 158-TM-5 Gill, P., 115-ABPSI-4/AEP-2 Han, D., 105-PC-7 Houts, M., 19-NFF-1 Dunlap, P., 155-SC-2 Foutch, D., 95-GTE-8 Glascock, M., 37-EP-3, 142-EP-10 Hariedy, H., 106-PC-8 Howard, V., 87-APC-2 Author / Session Chair Index Hsiao, R., 6-ECS-1 Johnston, R., 87-APC-2 Kim, T., 19-NFF-1, 49-PC-4 Kwon, S., 100-LP-12 Liu, P., 79-SR-3 Hu, C., 87-APC-2 Jolly, B., 19-NFF-1 Kim, Y., 107-PC-9 Lai, G., 98-HR-7, 123-HR-9 Liu, R., 12-GTE-2 Hu, H., 134-SC-1 Jones, D., 35-EDU-1, 108-SR-4 Kimura, R., 96-HR-5 Langhenry, M., 50-SR-2 Liu, T., 9-EP-2 Hua, Z., 132-PC-11 Jones, T., 35-EDU-1 Kimura, T., 101-LP-13 Langley, B., 144-GTE-12 Liu, X., 79-SR-3, 157-SR-7 Huang, B., 17-LP-3, 43-LP-6 Joo, J., 32-ABPSI-2 Kinefuchi, K., 45-LP-8, 149-LP-20 Lapilli, G., 103-LP-15 Liu, Y., 144-GTE-12 Huang, C., 42-LP-5, 131-PC-10, 154-PC-15 Jorns, B., 8-EP-1, 90-EP-7 Kirchberger, C., 45-LP-8 Lash, E., 80-ST-2 Lochin, K., 77-PC-5 Huang, G., 14-HSABP-1, 68-GTE-5, 94-GTE-7, Joshi, D., 125-HSABP-5/GTE-10 Kirk, D., 64-EE-3, 103-LP-15 Laskaridis, P., 95-GTE-8 Locke, J., 149-LP-20 121-GTE-9 Joyner, C., 19-NFF-1, 74-NFF-3 Kirk, T., 155-SC-2 Lasko, T., 64-EE-3 Lombardi, A., 76-PAW-3 Huang, W., 65-EP-5 Julienne, F., 94-GTE-7 Kirubhakaran, K., 105-PC-7 Launglucknavalai, K., 22-PC-1 Long, K., 144-GTE-12 Huang, Y., 149-LP-20 Jung, H., 128-LP-18 Kitagawa, K., 40-HR-3 Lawrence, C., 7-EE-1 Long, M., 18-LP-4 Huang, Z., 101-LP-13 Justice, B., 17-LP-3 Kizito, J., 41-HSABP-2 Leary, B., 108-SR-4 Lopez, J., 105-PC-7 Hubbard, S., 39-HR-2 Kading, B., 61-APS-2 Klatte, J., 128-LP-18 Leavitt, L., 4-ABPSI-1 Lopez Ortega, A., 90-EP-7 Hughes, M., 61-APS-2 Kagawa, H., 49-PC-4, 72-LP-10, 128-LP-18 Klein, A., 116-APS-3 Leccese, G., 16-LP-2 Lord, C., 10-FFP-1 Huijsman, R., 122-HR-8 Kailasanath, K., 22-PC-1 Knapton, J., 125-HSABP-5/GTE-10 Leclair, A., 44-LP-7 Lörincz, I., 104-NFF-4 Hupfer, A., 68-GTE-5 Kaiser, S., 95-GTE-8 Knaus, D., 70-HSABP-3 Lee, C., 39-HR-2, 147-HSABP-7 Lorr, J., 90-EP-7 Hwang, K., 48-PC-3 Kakudo, H., 43-LP-6 Knight, M., 102-LP-14 Lee, D., 39-HR-2, 58-ABPSI-3, 142-EP-10 Lou, F., 4-ABPSI-1 Hyde, S., 50-SR-2 Kamath, U., 72-LP-10 Knop, T., 122-HR-8 Lee, H., 6-ECS-1, 48-PC-3, 63-ECS-2 Lu, F., 125-HSABP-5/GTE-10, 143-GTE-11/HSABP-6 Iannetti, A., 86-AEC-1 Kamhawi, H., 65-EP-5 Knowles, B., 86-AEC-1 Lee, P., 23-PC-2 Lu, W., 68-GTE-5, 94-GTE-7 Iha, K., 49-PC-4 Kamis, Y., 37-EP-3 Kobald, M., 123-HR-9 Lei, R., 157-SR-7 Luchinsky, D., 149-LP-20 Ikeda, H., 49-PC-4 Kammash, T., 46-NFF-2 Kobayashi, H., 45-LP-8 Lekeux, A., 18-LP-4, 44-LP-7, 101-LP-13 Lucht, R., 154-PC-15 Im, H., 68-GTE-5 Kan, B., 17-LP-3 Kobayashi, K., 42-LP-5, 124-HSABP-4 Lemieux, P., 13-HR-1, 122-HR-8 Lundbladh, A., 95-GTE-8 Inzenhofer, A., 68-GTE-5 Kanai, R., 146-HR-10 Koc, S., 63-ECS-2 Lentini, D., 16-LP-2 Luo, J., 94-GTE-7

85 Ishizaki, S., 124-HSABP-4 Kandula, M., 72-LP-10 Kodali, A., 149-LP-20 Leonardi, M., 148-LP-19 Luo, M., 18-LP-4 Isochi, H., 43-LP-6 Kang, H., 100-LP-12 Kohga, M., 49-PC-4 Levack, D., 74-NFF-3 Lynch, E., 132-PC-11 Isono, T., 58-ABPSI-3 Kapat, J., 11-GTE-1, 51-TM-2, 67-GTE-4, 94-GTE-7, Kojima, J., 15-LP-1 Lewandowski, E., 33-ECD-1, 62-ECD-2, 88-ECD-3, Lynch, S., 11-GTE-1 Itani, M., 36-EE-2 121-GTE-9, 144-GTE-12 Kolmakova, D., 121-GTE-9 140-ECD-4 Ma, F., 77-PC-5 Ivanov, V., 77-PC-5 Kappagantula, K., 63-ECS-2 Kopasakis, G., 95-GTE-8, 125-HSABP-5/GTE-10 Leyva, I., 17-LP-3, 43-LP-6 Ma, W., 157-SR-7 Iwata, C., 134-SC-1 Karabeyoglu, A., 40-HR-3, 64-EE-3, 69-HR-4, Koroglu, B., 105-PC-7 Li, C., 107-PC-9 MacDonald, E., 142-EP-10 Jack, S., 127-LP-17 98-HR-7, 123-HR-9 Kovacic, P., 24-SR-1 Li, J., 22-PC-1, 24-SR-1, 70-HSABP-3 MacInnis, D., 41-HSABP-2 Jackson, T., 49-PC-4, 107-PC-9 Karp, A., 13-HR-1, 69-HR-4, 146-HR-10 Kozmic, J., 6-ECS-1 Li, S., 12-GTE-2 Madhanabharatam, B., 40-HR-3, 146-HR-10 Jacob, E., 42-LP-5, 103-LP-15 Kartuzova, O., 18-LP-4 Krasowski, M., 61-APS-2 Li, Y., 121-GTE-9 Maggi, F., 97-HR-6, 152-PC-13 Jagannath, R., 143-GTE-11/HSABP-6 Kasahara, J., 107-PC-9 Krueger, S., 101-LP-13 Li, Z., 21-PAW-1 Magstadt, A., 71-ITAR-1 Jalaleddine, M., 89-ED-2/EE-4 Kassemi, M., 18-LP-4 Kubo, N., 41-HSABP-2 Liang, R., 8-EP-1 Mahaffy, K., 35-EDU-1 Jammalamadaka, A., 121-GTE-9 Kawasaki, A., 9-EP-2 Kubota, K., 9-EP-2 Liang, T., 132-PC-11 Maicke, B., 44-LP-7, 135-SR-5 Jansen, R., 59-AEP-1 Kelly, D., 19-NFF-1 Küçük, U., 32-ABPSI-2 Lim, D., 17-LP-3 Majdalani, J., 13-HR-1, 24-SR-1, 44-LP-7 Jayaganesan, B., 102-LP-14 Kerner, K., 144-GTE-12 Kuehl, H., 62-ECD-2 Lin, J., 98-HR-7, 123-HR-9 Majumdar, A., 44-LP-7, 117-EDU-2, 134-SC-1 Jens, E., 39-HR-2 Key, N., 4-ABPSI-1, 12-GTE-2 Kulatilaka, W., 105-PC-7 Lin, S., 158-TM-5 Mallory, J., 48-PC-3, 64-EE-3, 92-FFP-2, 153-PC-14 Jeong, S., 17-LP-3 Khalil, E., 26-TM-1, 36-EE-2, 51-TM-2, 106-PC-8, Kumar, G., 12-GTE-2 Lin, Y., 115-ABPSI-4/AEP-2 Malo-Molina, F., 41-HSABP-2, 156-SR-6/HSABP-8 Jia, Z., 158-TM-5 120-GE-1, 158-TM-5 Kuninaka, H., 8-EP-1 Lindstrom, M., 22-PC-1 Mani, M., 76-PAW-3 Jiang, C., 147-HSABP-7 Khan, M., 23-PC-2 Kurisko, N., 92-FFP-2 Lineberry, D., 35-EDU-1, 42-LP-5, 108-SR-4, Mani, S., 58-ABPSI-3, 70-HSABP-3, 135-SR-5, Jiang, F., 68-GTE-5 Khandelwal, B., 10-FFP-1, 92-FFP-2 Kurosawa, Y., 105-PC-7 148-LP-19 153-PC-14 Jin, B., 79-SR-3 Khasin, M., 149-LP-20 Kurosu, A., 16-LP-2, 42-LP-5 Liou, M., 32-ABPSI-2 Manning, R., 126-LP-16 Jin, Y., 48-PC-3 Kibbey, T., 25-ST-1 Kurth, G., 156-SR-6/HSABP-8 List, M., 71-ITAR-1 Manship, T., 78-PC-6 Johansen, C., 26-TM-1 Kieatiwong, A., 102-LP-14 Kutlu, B., 67-GTE-4 Little, Z., 11-GTE-1, 67-GTE-4, 144-GTE-12 Marcelino, E., 81-TM-3 John, F., 4-ABPSI-1 Kiel, B., 71-ITAR-1 Kuwahara, T., 108-SR-4, 123-HR-9, Liu, B., 106-PC-8 Marcu, B., 149-LP-20 John, J., 135-SR-5 Kim, B., 6-ECS-1 156-SR-6/HSABP-8 Liu, C., 32-ABPSI-2 Marley, C., 86-AEC-1 Johnson, C., 61-APS-2 Kim, H., 17-LP-3, 32-ABPSI-2 Kuznetsov, S., 72-LP-10 Liu, D., 90-EP-7 Marquardt, T., 13-HR-1 Johnson, L., 46-NFF-2, 60-APC-1 Kim, J., 89-ED-2/EE-4, 128-LP-18 Kwon, O., 49-PC-4 Liu, F., 94-GTE-7 Marsell, B., 103-LP-15 Author / Session Chair Index Marshall, W., 19-NFF-1, 142-EP-10 Millar, R., 86-AEC-1 Nakaya, S., 43-LP-6 Oh, S., 89-ED-2/EE-4 Penney, N., 99-ITAR-2 Martelli, E., 150-LP-21 Miller, S., 66-EP-6 Nakazono, B., 146-HR-10 Ohlinger, W., 90-EP-7 Pepi, M., 144-GTE-12 Martin, C., 19-NFF-1 Miller, V., 39-HR-2 Nalianda, D., 32-ABPSI-2, 94-GTE-7 Oide, S., 105-PC-7 Perez, V., 35-EDU-1 Martinez, J., 15-LP-1 Mirgolbabaei, H., 41-HSABP-2, 147-HSABP-7 Nalim, M., 23-PC-2, 143-GTE-11/HSABP-6 Oigawa, Y., 142-EP-10 Perkins, H., 143-GTE-11/HSABP-6 Martinez, R., 90-EP-7 Mitchell, D., 19-NFF-1 Naraghi, M., 16-LP-2 Okai, K., 59-AEP-1 Perotti, J., 149-LP-20 Marzat, J., 86-AEC-1 Miyairi, Y., 59-AEP-1 Nardi, R., 35-EDU-1, 117-EDU-2 Okaya, S., 61-APS-2 Perullo, C., 59-AEP-1, 94-GTE-7, 95-GTE-8 Mascaro, M., 35-EDU-1, 108-SR-4 Mo, J., 64-EE-3 Nardozzo, P., 96-HR-5 Okita, K., 149-LP-20 Perumal, A., 58-ABPSI-3 Mason, L., 33-ECD-1, 62-ECD-2 Moder, J., 45-LP-8, 103-LP-15 Narsai, P., 122-HR-8 Okuno, Y., 9-EP-2, 140-ECD-4 Perumall, P., 7-EE-1 Masquelet, M., 44-LP-7 Modgil, G., 12-GTE-2 Nascimento Dias Barcelos Junior, M., 69-HR-4 Oliver, R., 81-TM-3 Petersen, E., 78-PC-6, 97-HR-6, 108-SR-4 Mather, J., 99-ITAR-2, 155-SC-2 Moehlenkamp, R., 124-HSABP-4 Nash, L., 105-PC-7 Olmstead, D., 117-EDU-2 Peterson, D., 147-HSABP-7 Matsubara, K., 142-EP-10 Moeller, T., 80-ST-2 Nasuti, F., 16-LP-2, 40-HR-3, 42-LP-5, 44-LP-7, Olsen, J., 150-LP-21 Petitot, S., 101-LP-13 Matsuo, A., 107-PC-9 Mohammed, S., 106-PC-8 148-LP-19, 150-LP-21 Onay, O., 51-TM-2 Petrarolo, A., 123-HR-9 Matsuoka, K., 107-PC-9 Momanyi, E., 122-HR-8 Natale, P., 16-LP-2, 44-LP-7 Onofri, M., 148-LP-19 Pfeiffer, J., 62-ECD-2 Matsuura, K., 105-PC-7 Mongia, H., 23-PC-2 Natan, B., 78-PC-6 Oravec, H., 99-ITAR-2, 155-SC-2 Piet-Lahanier, H., 86-AEC-1 Matveev, V., 121-GTE-9 Montanari, F., 77-PC-5 Natsui, G., 144-GTE-12 Ordonneau, G., 86-AEC-1 Pimenta, A., 35-EDU-1 Mavris, D., 59-AEP-1, 80-ST-2, 89-ED-2/EE-4, Moon, Y., 39-HR-2 Naumann, K., 156-SR-6/HSABP-8 Oriti, S., 33-ECD-1, 62-ECD-2 Pinero, L., 61-APS-2, 65-EP-5 94-GTE-7, 95-GTE-8, 133-PP-1 Moore, J., 78-PC-6, 101-LP-13 Naveen, N., 135-SR-5 Osborn, M., 66-EP-6 Piscitelli, F., 97-HR-6 Maxwell, T., 81-TM-3 Moore, R., 44-LP-7 Neely, A., 150-LP-21 Osborne, J., 105-PC-7 Piskin, T., 80-ST-2 Mazouffre, S., 65-EP-5, 90-EP-7 Moore, T., 50-SR-2 Neff, G., 65-EP-5 Oshilalu, A., 7-EE-1 Piszczor, M., 140-ECD-4 Mazzola, L., 97-HR-6 Morant, L., 89-ED-2/EE-4 Negishi, H., 16-LP-2, 45-LP-8 Otto, M., 11-GTE-1 Pitot, J., 7-EE-1, 69-HR-4, 98-HR-7 Mbagwu, C., 14-HSABP-1 Moriya, S., 101-LP-13 Negishi, N., 156-SR-6/HSABP-8 Otto, S., 4-ABPSI-1 Pitz, R., 22-PC-1 Mcbean, I., 94-GTE-7 Moroniti, D., 133-PP-1 Negoro, N., 16-LP-2 Owens, R., 116-APS-3 Pizzarelli, M., 16-LP-2, 44-LP-7

86 McCallum, P., 116-APS-3 Moser, M., 35-EDU-1, 108-SR-4 Nelson, G., 117-EDU-2 Ozawa, K., 40-HR-3 Podleski, S., 47-PAW-2 McCauley, R., 50-SR-2 Motohashi, K., 154-PC-15 Neri, A., 50-SR-2, 79-SR-3, 135-SR-5, 157-SR-7 Ozcan, M., 95-GTE-8 Poe, D., 50-SR-2 McDonald, M., 66-EP-6 Mourad, M., 7-EE-1 Nessler, C., 71-ITAR-1 Ozgun, M., 51-TM-2 Polk, J., 66-EP-6, 90-EP-7 McGarry, J., 107-PC-9 Mourad, S., 36-EE-2 Nguyen, N., 102-LP-14 Paccagnella, E., 40-HR-3 Polsgrove, R., 74-NFF-3 McHenry, S., 50-SR-2 Mrema, H., 41-HSABP-2 Nguyen, T., 152-PC-13 Pace, G., 100-LP-12 Polzin, K., 9-EP-2, 37-EP-3, 142-EP-10 McKnight, B., 96-HR-5 Mueller, M., 72-LP-10, 126-LP-16, 128-LP-18 Ni, Q., 12-GTE-2 Pafford, B., 35-EDU-1 Ponizovskaya-Devine, E., 149-LP-20 McLean, C., 15-LP-1 Mugenda, A., 15-LP-1 Nichols, R., 58-ABPSI-3 Paik, K., 23-PC-2 Pons Lorente, A., 96-HR-5 McManus, K., 48-PC-3 Mullins, C., 90-EP-7 Nicolleau, F., 125-HSABP-5/GTE-10 Palaszewski, B., 104-NFF-4 Pontelandolfo, P., 126-LP-16 McPherson, M., 78-PC-6 Murakami, D., 144-GTE-12 Nishiyama, K., 8-EP-1 Palerm, S., 86-AEC-1, 101-LP-13 Ponti, F., 68-GTE-5, 157-SR-7 Mechentel, F., 39-HR-2 Murakami, N., 9-EP-2 Noelting, S., 76-PAW-3 Pan, H., 41-HSABP-2 Popov, G., 121-GTE-9 Medick, C., 117-EDU-2 Murphy, J., 78-PC-6 Nojima, K., 124-HSABP-4 Panagiotis, L., 32-ABPSI-2 Popov, P., 148-LP-19 Medina, M., 94-GTE-7 Murray, C., 116-APS-3 Nomura, H., 59-AEP-1 Paniagua, G., 11-GTE-1, 67-GTE-4 Pourpoint, T., 15-LP-1, 49-PC-4, 99-ITAR-2, Meholic, G., 104-NFF-4 Murugan, M., 144-GTE-12 Nordeen, C., 22-PC-1 Pantoya, M., 63-ECS-2 100-LP-12 Mehta, J., 22-PC-1 Murugesan, M., 77-PC-5 Nordin-Bates, K., 41-HSABP-2, 93-GTE-6 Parammasivam, K., 11-GTE-1, 93-GTE-6, 105-PC-7 Powell, S., 122-HR-8 Mehta, Y., 11-GTE-1 Musgrove, G., 103-LP-15 Norris, S., 25-ST-1 Paravan, C., 97-HR-6, 152-PC-13 Power, K., 19-NFF-1 Meier, E., 148-LP-19 Musielak, D., 70-HSABP-3 Nozari, H., 64-EE-3 Parker, D., 61-APS-2 Poyraz, U., 156-SR-6/HSABP-8 Meng, H., 51-TM-2 Muslubas, Y., 14-HSABP-1 Nufer, B., 72-LP-10 Parthasarathy, R., 92-FFP-2 Prince, B., 66-EP-6 Menon, S., 107-PC-9 Myers, J., 65-EP-5 Nunome, Y., 42-LP-5 Pasini, A., 100-LP-12 Prokop, N., 61-APS-2 Merkle, C., 42-LP-5, 131-PC-10 Myers, M., 61-APS-2 Nuzum, S., 158-TM-5 Pastrone, D., 13-HR-1, 39-HR-2, 146-HR-10 Proscia, W., 77-PC-5 Merkley, D., 13-HR-1, 97-HR-6 Myren, D., 58-ABPSI-3 O’Brien, W., 32-ABPSI-2 Patel, M., 116-APS-3 Pryor, O., 105-PC-7 Merkley, S., 69-HR-4 Nagaraju Doddi, H., 153-PC-14 O’Neill, W., 87-APC-2, 142-EP-10 Patterson, M., 8-EP-1, 65-EP-5 Pugmire, K., 73-LP-11 Meyer, M., 102-LP-14 Nagata, H., 146-HR-10 Obikane, Y., 35-EDU-1, 77-PC-5 Patton, C., 41-HSABP-2, 147-HSABP-7 Putzu, R., 126-LP-16 Meyer, T., 156-SR-6/HSABP-8 Nakagaki, M., 108-SR-4 OBrien, T., 147-HSABP-7 Pavarin, D., 40-HR-3 Qin, F., 41-HSABP-2, 70-HSABP-3, 106-PC-8 Micka, D., 70-HSABP-3 Nakagami, S., 107-PC-9 Ochs, S., 32-ABPSI-2 Paxson, D., 143-GTE-11/HSABP-6 Quach, P., 15-LP-1 Mikellides, I., 90-EP-7 Nakagawa, I., 96-HR-5 Oefelein, J., 106-PC-8 Peace, J., 143-GTE-11/HSABP-6 Qualls, A., 19-NFF-1 Mikkelsen, K., 47-PAW-2, 58-ABPSI-3 Nakamura, Y., 142-EP-10 Ogedengbe, E., 7-EE-1, 120-GE-1 Peltier, S., 105-PC-7 Quinlan, J., 93-GTE-6 Author / Session Chair Index Raghavan, S., 94-GTE-7, 144-GTE-12 Ruf, J., 127-LP-17 Schumaker, S., 42-LP-5, 148-LP-19 Smith, T., 41-HSABP-2 Swanson, T., 65-EP-5 Raman, V., 49-PC-4 Ruscher, C., 71-ITAR-1 Schvallinger, M., 94-GTE-7 Snedden, G., 95-GTE-8 Sweeney, B., 43-LP-6 Ramji, S., 105-PC-7 Russell, T., 61-APS-2 Schwab, U., 8-EP-1 Sobey, A., 60-APC-1 Sweidan, A., 7-EE-1 Ramsel, J., 156-SR-6/HSABP-8 Saccone, G., 97-HR-6 Schwendeman, C., 81-TM-3 Sobhi, M., 36-EE-2 Sykes, K., 60-APC-1 Randle, D., 115-ABPSI-4/AEP-2 Sadeq, A., 92-FFP-2 Schwer, D., 22-PC-1 Sojka, P., 48-PC-3 Tadge, M., 104-NFF-4 Rani, S., 131-PC-10 Saito, M., 154-PC-15 Scogin, T., 9-EP-2 Sojourner, T., 50-SR-2 Tagashira, T., 59-AEP-1 Rani, V., 131-PC-10 Saito, Y., 146-HR-10 Scott, J., 46-NFF-2, 141-ECS-3 Sokhey, J., 21-PAW-1, 47-PAW-2 Taha, A., 23-PC-2 Rao, P., 6-ECS-1 Sakaki, K., 43-LP-6 Scroggins, A., 134-SC-1 Song, W., 12-GTE-2 Tai, J., 95-GTE-8, 145-GTE-13 Rathakrishnan, E., 58-ABPSI-3 Sakurai, T., 122-HR-8, 123-HR-9, Seal, S., 108-SR-4 Song, X., 12-GTE-2 Tajmar, M., 37-EP-3, 104-NFF-4 Ravaglioli, V., 68-GTE-5 125-HSABP-5/GTE-10 Sedwick, R., 46-NFF-2 Sousa, J., 67-GTE-4 Takada, S., 101-LP-13 Ravi, D., 11-GTE-1 Sakuranaka, N., 58-ABPSI-3 Sefcik, R., 19-NFF-1 Sowers, T., 86-AEC-1 Takahashi, H., 127-LP-17 Raviprasad, S., 134-SC-1 Salloum, S., 36-EE-2 Seleznev, R., 132-PC-11 Spencer, V., 72-LP-10 Takahashi, K., 157-SR-7 Rayman, M., 8-EP-1 Sammet, T., 78-PC-6 Semrau, G., 61-APS-2 Spores, R., 15-LP-1 Talley, D., 42-LP-5 Redden, J., 50-SR-2 Sampson, J., 15-LP-1 Senda, F., 26-TM-1 Sproesser, M., 89-ED-2/EE-4 Tamanampudi, G., 131-PC-10 Reed, B., 15-LP-1 Samuel, A., 115-ABPSI-4/AEP-2 Sese, C., 149-LP-20 Spurling, J., 79-SR-3 Tanabe, M., 154-PC-15 Reese, S., 102-LP-14 Sanal Kumar, V., 58-ABPSI-3, 70-HSABP-3, Seymour, M., 134-SC-1 Spurrier, Z., 69-HR-4, 96-HR-5, 97-HR-6 Tanaka, M., 135-SR-5, 140-ECD-4 Reid, D., 108-SR-4 153-PC-14 Shaevich, S., 72-LP-10 Spyridon, P., 117-EDU-2 Tang, J., 157-SR-7 Reid, T., 62-ECD-2 Sanchez Arribas, P., 13-HR-1 Shastry, R., 9-EP-2, 65-EP-5 Srikanth, P., 158-TM-5 Tang, W., 14-HSABP-1 Reisz, A., 9-EP-2, 87-APC-2 Sandifer, C., 116-APS-3 Shea, P., 71-ITAR-1 Stanley, S., 99-ITAR-2, 151-LP-22/ PGC-1/ PC-12 Tang, X., 41-HSABP-2, 70-HSABP-3 Ren, Z., 48-PC-3 Sankar, L., 7-EE-1 Shemelya, C., 142-EP-10 Starkey, R., 125-HSABP-5/GTE-10 Tang, Y., 157-SR-7 Renganathan, A., 80-ST-2 Sankaran, V., 42-LP-5 Sherif, S., 118-EE-5 Stechmann, D., 17-LP-3, 149-LP-20 Tangirala, V., 125-HSABP-5/GTE-10, 147-HSABP-7 Rezende, L., 108-SR-4 Saracoglu, B., 67-GTE-4 Shi, W., 70-HSABP-3 Steelant, J., 148-LP-19 Tani, N., 45-LP-8

87 Rhodes, B., 126-LP-16 Sarae, W., 149-LP-20 Shibasawa, G., 135-SR-5 Steen, S., 64-EE-3 Tarau, C., 26-TM-1, 51-TM-2, 81-TM-3, 158-TM-5 Rhodes, R., 60-APC-1 Sarawate, N., 155-SC-2 Shimada, T., 40-HR-3, 69-HR-4, 96-HR-5, 123-HR-9, Steffan, S., 61-APS-2 Tarditi, A., 46-NFF-2 Riccius, J., 102-LP-14 Sargent, D., 15-LP-1, 100-LP-12 157-SR-7 Stegeman, J., 142-EP-10 Tasdelen, V., 12-GTE-2 Richardson, D., 50-SR-2 Sarhan, A., 135-SR-5 Shimizu, T., 42-LP-5 Steinberg, A., 105-PC-7, 154-PC-15 Tate, J., 94-GTE-7 Richichi, M., 92-FFP-2 Sarikaya, G., 106-PC-8 Shin, E., 62-ECD-2 Stephens, J., 74-NFF-3 Taunay, P., 90-EP-7 Ricklick, M., 11-GTE-1, 67-GTE-4 Sass, J., 126-LP-16, 149-LP-20 Shioya, S., 49-PC-4 Stewart, M., 45-LP-8 Taylor, B., 74-NFF-3 Riehl, R., 81-TM-3 Sasson, J., 4-ABPSI-1 Shipeng, L., 152-PC-13, 157-SR-7 Stoddard, W., 125-HSABP-5/GTE-10 Taylor, J., 22-PC-1 Riley, L., 147-HSABP-7 Sato, M., 101-LP-13 Shitta, M., 120-GE-1 Storey, J., 103-LP-15 Taylor, L., 33-ECD-1 Rinehart, A., 86-AEC-1 Schallhorn, P., 44-LP-7, 103-LP-15 Shynkarenko, O., 69-HR-4 Story, G., 97-HR-6, 146-HR-10 Taylor, S., 99-ITAR-2, 155-SC-2 Risha, G., 78-PC-6 Scharlemann, C., 102-LP-14 Sideris, A., 148-LP-19 Strakey, P., 143-GTE-11/HSABP-6 Temme, J., 70-HSABP-3, 105-PC-7 Roberts, L., 98-HR-7 Scharnhorst, R., 59-AEP-1, 76-PAW-3 Sidwell, T., 143-GTE-11/HSABP-6 Straub, J., 61-APS-2, 116-APS-3 Teraki, H., 146-HR-10 Roberts, M., 64-EE-3 Scheidegger, R., 61-APS-2, 65-EP-5 Silva, D., 81-TM-3 Strauch, J., 116-APS-3 Tharikaa, R., 135-SR-5, 153-PC-14 Roberts, R., 134-SC-1, 158-TM-5 Schery, S., 144-GTE-12 Simon, D., 86-AEC-1 Strunz, R., 101-LP-13 Thiede, G., 102-LP-14 Robinson, J., 60-APC-1, 87-APC-2 Schifer, N., 81-TM-3 Simurda, L., 146-HR-10 Su, W., 24-SR-1 Thomas, J., 97-HR-6 Rocco, J., 49-PC-4 Schillo, K., 46-NFF-2 Singh, R., 32-ABPSI-2, 94-GTE-7 Su, Y., 17-LP-3 Thomas, R., 8-EP-1, 65-EP-5 Rodrigues, N., 48-PC-3 Schlechtriem, S., 100-LP-12, 120-GE-1, 123-HR-9 Singh-derewa, C., 134-SC-1 Subramanian, S., 93-GTE-6 Thompson, S., 46-NFF-2 Rodriguez, C., 64-EE-3 Schloeder, N., 9-EP-2 Sir, M., 25-ST-1, 80-ST-2 Sugimori, D., 149-LP-20 Thorn, C., 117-EDU-2, 121-GTE-9 Rodriguez, J., 94-GTE-7 Schmidt, V., 90-EP-7 Siri, K., 89-ED-2/EE-4 Sugiu, N., 154-PC-15 Thorpe, D., 60-APC-1 Rodriguez, M., 46-NFF-2 Schmitz, P., 33-ECD-1 Sirignano, W., 148-LP-19 Sui, X., 49-PC-4, 157-SR-7 Thrasher, J., 142-EP-10 Rosenberg, D., 66-EP-6 Schnackel, J., 101-LP-13 Skiba, A., 105-PC-7 Sujith, R., 77-PC-5, 131-PC-10 Thumann, A., 156-SR-6/HSABP-8 Rosetti, S., 115-ABPSI-4/AEP-2 Schneider, D., 127-LP-17, 150-LP-21 Slaby, M., 21-PAW-1 Sun, B., 24-SR-1 Tian, H., 39-HR-2 Rossi, A., 90-EP-7 Schneider, G., 10-FFP-1, 158-TM-5 Slater, J., 4-ABPSI-1 Sun, L., 68-GTE-5 Tillman, G., 32-ABPSI-2 Rouzbar, R., 14-HSABP-1 Schnitzler, B., 19-NFF-1 Smith, B., 68-GTE-5 Surzhikov, S., 132-PC-11 Tobaldini, L., 76-PAW-3 Rovey, J., 66-EP-6, 142-EP-10 Schomberg, K., 150-LP-21 Smith, G., 95-GTE-8 Sutliff, T., 88-ECD-3, 116-APS-3 Tomasic, D., 72-LP-10 Roy, A., 143-GTE-11/HSABP-6 Schrapp, H., 68-GTE-5 Smith, L., 61-APS-2, 124-HSABP-4 Suzuki, I., 123-HR-9 Tomioka, S., 41-HSABP-2, 58-ABPSI-3, 124-HSABP-4 Roy, S., 10-FFP-1, 92-FFP-2 Schreiber, J., 33-ECD-1 Smith, P., 71-ITAR-1, 99-ITAR-2 Suzuki, K., 43-LP-6 Tomita, T., 42-LP-5, 127-LP-17 Author / Session Chair Index Tomizawa, T., 122-HR-8 Vasu, S., 105-PC-7, 121-GTE-9, Wei, Z., 157-SR-7 Wordingham, C., 9-EP-2, 90-EP-7 Yungster, S., 143-GTE-11/HSABP-6 Tomoaki, U., 69-HR-4 143-GTE-11/HSABP-6 Weitzberg, A., 19-NFF-1 Wu, J., 123-HR-9, 124-HSABP-4 Zakrajsek, J., 116-APS-3 Toro Medina, J., 126-LP-16 Vaudolon, J., 65-EP-5, 90-EP-7 Welberg, D., 120-GE-1 Xia, C., 121-GTE-9 Zambon, A., 16-LP-2 Torre, L., 100-LP-12 Vaughan, D., 146-HR-10 Werling, L., 100-LP-12 Xiang, X., 68-GTE-5 Zametaev, E., 102-LP-14 Torvik, P., 144-GTE-12 Vazquez, A., 99-ITAR-2 Werner, M., 120-GE-1 Xin, X., 94-GTE-7 Zamora, M., 35-EDU-1 Toson, E., 69-HR-4 Veale, K., 7-EE-1, 69-HR-4, 98-HR-7 Werner, R., 122-HR-8 Xiong, J., 94-GTE-7 Zapata, E., 25-ST-1, 60-APC-1 Trammell, M., 19-NFF-1 Vellakal, M., 23-PC-2 Wessels, M., 76-PAW-3 Xiong, Y., 49-PC-4 Zarbo, N., 49-PC-4 Tran, L., 11-GTE-1, 51-TM-2, 67-GTE-4 Venkataraman, K., 122-HR-8 West, J., 45-LP-8 Xu, K., 14-HSABP-1, 51-TM-2 Zein-Sabatto, S., 86-AEC-1 Tran, P., 11-GTE-1, 67-GTE-4, 121-GTE-9 Venkatesan, J., 93-GTE-6 Wham, R., 116-APS-3 Xu, X., 132-PC-11 Zemba, M., 142-EP-10 Trapp, L., 76-PAW-3 Verberne, O., 98-HR-7 White, J., 14-HSABP-1, 62-ECD-2 Yabusaki, D., 149-LP-20 Zeng, P., 39-HR-2 Trawick, D., 133-PP-1 Vergos, C., 121-GTE-9 Whitmore, S., 13-HR-1, 69-HR-4, 96-HR-5, 97-HR-6, Yagishita, T., 101-LP-13 Zettervall, N., 93-GTE-6 Trefny, C., 4-ABPSI-1 Verma, S., 58-ABPSI-3 98-HR-7 Yahyaoui, M., 10-FFP-1 Zha, G., 68-GTE-5 Treubig, R., 94-GTE-7 Verseux, O., 115-ABPSI-4/AEP-2 Wicker, R., 142-EP-10 Yamada, H., 105-PC-7 Zhang, C., 70-HSABP-3 Trinh, H., 72-LP-10 Vignesh, R., 135-SR-5 Wiedow, B., 133-PP-1 Yamamoto, K., 108-SR-4 Zhang, F., 64-EE-3 Trivedi, M., 26-TM-1 Vijayakumar, N., 21-PAW-1 Wiegmann, B., 159-VS-1 Yamamoto, T., 105-PC-7 Zhang, H., 124-HSABP-4 Tsikata, S., 90-EP-7 Villar, L., 108-SR-4 Wierman, M., 154-PC-15 Yang, H., 45-LP-8 Zhang, J., 107-PC-9 Tsue, M., 43-LP-6 Viswanath, K., 71-ITAR-1 Wies, R., 115-ABPSI-4/AEP-2 Yang, J., 94-GTE-7 Zhang, L., 89-ED-2/EE-4 Tsukizaki, R., 8-EP-1 Vora, A., 134-SC-1 Wiest, H., 48-PC-3 Yang, L., 6-ECS-1 Zhang, S., 41-HSABP-2, 70-HSABP-3 Tu, S., 47-PAW-2 Vorobieff, P., 87-APC-2 Wignall, T., 41-HSABP-2, 147-HSABP-7 Yao, S., 143-GTE-11/HSABP-6 Zhang, X., 157-SR-7 Tucker, K., 117-EDU-2 Voskuilen, T., 99-ITAR-2 Williams, G., 15-LP-1, 74-NFF-3, 129-NFF-5 Yasukochi, H., 146-HR-10 Zhang, Y., 21-PAW-1 Tuncer, O., 106-PC-8 Votta, R., 44-LP-7, 98-HR-7 Williams, J., 8-EP-1, 90-EP-7 Ye, J., 41-HSABP-2, 70-HSABP-3 Zhang, Z., 147-HSABP-7 Tuttle, S., 66-EP-6 Voytovych, D., 32-ABPSI-2 Williams, L., 66-EP-6 Yedavalli, R., 86-AEC-1 Zhao, B., 96-HR-5

88 Tyson, R., 35-EDU-1 Wabel, T., 105-PC-7 Williams, S., 78-PC-6, 142-EP-10 Yelvington, P., 64-EE-3 Zhao, S., 39-HR-2 Ulas, A., 63-ECS-2 Wakita, M., 146-HR-10 Willingham, K., 92-FFP-2 Yetter, R., 78-PC-6 Zhao, Y., 124-HSABP-4 Umemura, Y., 45-LP-8 Walker, J., 65-EP-5 Wilson, D., 21-PAW-1 Yildiz, M., 66-EP-6 Zhou, C., 140-ECD-4 Unni, V., 77-PC-5 Walker, M., 9-EP-2, 99-ITAR-2 Wilson, K., 33-ECD-1 Yildiz, Y., 156-SR-6/HSABP-8 Zhou, D., 157-SR-7 Uriz, F., 115-ABPSI-4/AEP-2 Walker, S., 13-HR-1, 69-HR-4, 97-HR-6 Wilson, S., 33-ECD-1, 62-ECD-2 Yim, J., 37-EP-3, 65-EP-5, 90-EP-7 Zhou, W., 14-HSABP-1, 158-TM-5 Uslu, S., 23-PC-2 Wang, J., 68-GTE-5, 94-GTE-7, 143-GTE-11/HSABP-6 Wingborg, N., 152-PC-13 Yoh, J., 6-ECS-1, 107-PC-9 Zilliac, G., 39-HR-2, 146-HR-10 Usrey, M., 86-AEC-1 Wang, N., 24-SR-1, 49-PC-4, 152-PC-13, 157-SR-7 Winglee, R., 9-EP-2 Yoon, J., 92-FFP-2 Zimmer, J., 117-EDU-2 Uzol, O., 32-ABPSI-2 Wang, P., 39-HR-2 Wink, J., 122-HR-8 Yoon, Y., 17-LP-3, 92-FFP-2 Zimmerman, J., 39-HR-2 Valencia, E., 32-ABPSI-2 Wang, W., 94-GTE-7, 121-GTE-9 Winkler, C., 47-PAW-2 Youney, J., 126-LP-16 Zinn, B., 93-GTE-6 Vancil, B., 90-EP-7 Warmoth, G., 15-LP-1 Wise, B., 64-EE-3 Young, J., 8-EP-1, 65-EP-5 Zinnecker, A., 94-GTE-7 Vannoy, S., 115-ABPSI-4/AEP-2 Warner, W., 146-HR-10 Wolff, M., 134-SC-1, 158-TM-5 Yu, D., 14-HSABP-1 Zuo, F., 14-HSABP-1 Varia, A., 134-SC-1 Warren, J., 19-NFF-1 Wolford, D., 61-APS-2 Yu, L., 132-PC-11 Varol, G., 106-PC-8 Watanabe, T., 59-AEP-1 Wolinski, J., 46-NFF-2 Yu, N., 39-HR-2, 96-HR-5 Vasques, B., 18-LP-4 Waters, D., 115-ABPSI-4/AEP-2 Wong, W., 33-ECD-1 Yu, W., 158-TM-5 Vassallo, C., 104-NFF-4 Wei, S., 123-HR-9 Woo, N., 47-PAW-2 Yu, Z., 14-HSABP-1 Wei, X., 41-HSABP-2, 70-HSABP-3 Woolwine, K., 95-GTE-8 Yuan, T., 17-LP-3, 43-LP-6 2O16

25–27 JULY 2016 SALT LAKE CITY, UTAH SEE YOU NEXT YEAR! Propulsion and energy systems are at the very heart of25-27 aerospace, whetherJULY you 2016are flying passengers to SALT LAKE CITY, UT London or satellites to LEO. Every move forward in our exploration of the world, and the universe, is enabled by new technologies coming from the researchers and engineers who will assemble at the AIAA Propulsion and Energy Forum and Exposition 2016. Salt Lake City, Utah The forum will take place at the Salt Palace Convention Center, with participants staying at either the Hilton Salt Lake City or Radisson Salt Lake City. While there, take in the breathtaking scenery, visit the Clark Planetarium or visit one of the fifteen national parks and monuments that are within a few hours’ drive of the city. Utah has a rich history in the aviation and aerospace industries and is one of the top states in the nation in the concentration of aerospace employment. Utah’s core aerospace and aviation competencies include composites and advanced materials, propulsion systems, avionics, and control systems. Aerospace and aviation companies within the state include the full spectrum of the industry, from design and manufacturing to advanced space systems and regional air service, from repair and maintenance to software and control systems. For exhibits and sponsorship information please contact [email protected]

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