2O16 25–27 JULY 2016 SALT LAKE CITY, UT

Innovations in Propulsion and Energy Driving System Solutions

FINAL PROGRAM www.aiaa-propulsionenergy.org #aiaaPropEnergy

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NO DOWNLOADING REQUIRED! Executive Steering Committee 2O16 AIAA Propulsion and Energy 2016 Welcome Welcome to Salt Lake City, Utah, and AIAA Propulsion and Energy 2016. We are excited to share the next few days with you as we explore the most pressing issues facing the future of propulsion and energy systems – the true heart of aerospace. With so many insightful and dynamic speakers and panelists, we are confident you will find the information presented here thought-provoking, impactful, and immediately useful to you in your work.

Daniel “Dan” Michael Heil During the forum you will hear from thought leaders, learn about the latest technical Dumbacher Ohio Aerospace breakthroughs, and most importantly collaborate with other attendees from Purdue University Institute (Ret.) government, industry, and academia. It is these collaborations and opportunities for dialogue that really are the essence of our AIAA forums. The knowledge and insight gained from these interactions can give you an immediate edge in your career development.

Bran Ferren will kick off our plenary program with a keynote address that will set the tone for the days ahead. The rest of our plenary program examines the diverse areas and issues that we must consider if we are to advance the state of the art in propulsion and energy systems and technology. Issues that we will examine include: system needs in propulsion and energy; how technological innovation and invention are Randall B. Furnas Alton D. Romig Jr. changing the game in propulsion; high power systems for aerospace applications; how NASA Glenn National Academy of additive manufacturing is impacting how you design systems and platforms; and the Research Center Engineering formula for success and longevity in the aerospace business. Pierre Chao will close our program with his insights on the future of our community.

With over 700 presentations our technical program is second-to-none in terms of the scope, breadth, and depth of the cutting-edge research being presented – material that you will not find anywhere but here. We thank the Technical Program Committee for working hard to assemble these tracks.

AIAA Propulsion and Energy 2016 will energize, inspire, and sustain our Julie Van Kleeck community’s efforts to power the next bold steps in space commercialization and Aerojet Rocketdyne exploration, while improving the efficiency and reliability of terrestrial systems. We thank you for making the choice to be here with us for this forum, and we are confident you will find the experience personally and professionally rewarding.

52nd AIAA/SAE/ASEE Joint AIAA Propulsion and Energy Propulsion Conference 2016 is proud to feature the following conferences: 14th International Energy Conversion Engineering Conference www.aiaa-propulsionenergy.org 3 #aiaaPropEnergy IntroOrganizing Committee

Forum Organizing Committee Aircraft Electric Propulsion Hybrid Rockets Charles Beard, The Boeing Company Bala (Han) Madhan, SPG Forum General Chair Daniel “Dan” Dumbacher, Purdue Electricity Delivery, Grid and Energy Liquid Rocket Propulsion University Storage Technologies William Marshall, NASA Glenn Scott Duncan, Georgia Institute of Research Center Forum 360 Chair Technology John Horack, Ohio State University Nuclear and Future Flight Propulsion Carson Vaisden, John Hopkins University Greg Meholic, The Aerospace Corporation Technical Program Chair Applied Physics Laboratory Justin Locke, United Technologies Jason Cassibry, University of Alabama, Joseph Troutman, EnerSys Advanced Huntsville Technical Program Committee Systems Propellants and Combustion Forum Technical Chair Electric Propulsion Oskar Haidn, Technische Universität Justin Locke, United Technologies Josh Rovey, Missouri University of Science München & Technology Deputy Technical Chair Energy Propulsion and Power Systems of Michael Choi, NASA Goddard Space Flight Energetic Components & Systems Unmanned Systems Center John Scott, United Launch Alliance Lea-Der Chen, University of Iowa Deputy Technical Chair Space Energy Conversion Device Technology Propulsion Education David Ransom, Southwest Research Edward Lewandowski, NASA Glenn Robert Frederick, University of Alabama in Institute Research Center Huntsville ITAR Chair Energy-Efficient and Renewable Small Satellites Knox Millsaps, Office of Naval Research Energy Technologies Jeremy Straub, University of North Dakota Essam Khalil, Cairo University SAE Liaison Solid Rockets Richard Millar, Naval Postgraduate School Scott Duncan, Georgia Institute Alana Spurling, U.S. Navy of Technology ASME Liaison Spacecraft and Aircraft Power John Robinson, The Boeing Company (Ret.) Fossil-Fuel Power Technologies System Technologies Bhupendra Khandelwal, University Salim Abbas, Lockheed Martin (Ret.) ASEE Liaison of Sheffield Robert Frederick, University of Alabama, Mark Liffring, The Boeing Company Huntsville Essam Khalil, Cairo University Pavel Tsvetkov, Texas A&M University Technical Area Organizers Gas Turbine Engines Jayanta Kapat, University of Thermal Management Technology Additive Manufacturing for Central Florida Michael Choi, NASA Goddard Space Propulsion Systems Flight Center Corrine Gatto, NASA Jet Propulsion Robert Thacker-Dey, Naval Air Systems Laboratory Command

Advanced Engine Control and Chukwuka Mbagwu, University of Intelligent Systems Michigan Alireza “Al” Behbahani, U.S. Air Force Green Engineering/Green Energy Advanced Propulsion Concepts Tarek Absel-Salam, East Carolina John Robinson, The Boeing Company University (Ret.) High Speed Air Breathing Propulsion Advanced Vehicle Systems Faure “Joel” Malo-Molina, Raytheon Frank Chandler, The Boeing Company Missile Systems

Air Breathing Propulsion Systems Integration Erik Axdahl, NASA Langley Research Eric Loth, University of Virginia Center

www.aiaa-propulsionenergy.org 4 #aiaaPropEnergy IntroContents

Welcome 3

Organizing Committee 4

Forum Overview 6

Sponsors 7 www.twitter.com/aiaa

Keynote Speakers and Plenary Sessions 8 www.facebook.com/AIAAfan

Forum 360 10 www.youtube.com/AIAATV

Networking and Special Events 12 www.linkedin.com/companies/aiaa

www.flickr.com/aiaaevents Recognition Event 13

www.instagram.com/aiaaerospace ITAR Information 16 livestream.com/AIAAvideo/PropEnergy2016 Exposition Hall 18 Join the conversation! Join the Q&A! #aiaaPropEnergy aiaa.cnf.io Exhibitors 20

On-Site Wi Fi Information General Information 25 Network Name: AIAA Password: propenergy Author and Session Chair Information 27 Photography or the video or audio recording Committee Meetings 28 of sessions or exhibits, as well as the unauthorized sale of AIAA-copyrighted Sessions at a Glance 30 material, is prohibited.

The American Institute of Aeronautics and Astronautics Session Detail Matrix 36 (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, Author and Session Chair Index 78 more connected, more accessible, and more prosperous. For more information, visit www.aiaa.org, or follow us on Twitter @AIAA. Venue Map Inside Back Cover www.aiaa-propulsionenergy.org 5 #aiaaPropEnergy IntroForum Overview

MONDAY TUESDAY WEDNESDAY 25 July 26 July 27 July

Speakers’ Briefing in Technical Speakers’ Briefing in Technical Speakers’ Briefing in Technical 0730hrs Session Rooms (both am & pm sessions) Session Rooms (both am & pm sessions) Session Rooms (both am & pm sessions)

0800 hrs Welcome/Intro Plenary Panel Plenary Panel 0830 hrs Opening Plenary Session

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

0930 hrs Technical 1000 hrs Exposition Rising Leaders Exposition Rising Sessions Exposition Hall Open in Aerospace Technical Forum 360 Hall Open Technical Forum 360 Leaders Hall Open 1030 hrs & Rising and Sessions Session Sessions Session Speed Leaders in Forum 360 Networking 1100 hrs Aerospace Session Panel 1130 hrs Genera- tion 1200 hrs STEM Lunch in Exposition Hall Event 1230 hrs Lunch on Own Forum Recognition Luncheon

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

1500 hrs Networking Break in Exposition Hall Exposition Exposition Hall Open 1530 hrs Hall Open

1600 hrs Technical Forum 360 Technical Technical Forum 360 Sessions Session Sessions 1630 hrs Sessions Session

1700 hrs

1730 hrs

1800 hrs

1830 hrs Reception in Exposition Hall Propulsion and Energy Lecture

1900 hrs

1930 hrs Rising Leaders in Aerospace Reception 2000 hrs

www.aiaa-propulsionenergy.org 6 #aiaaPropEnergy IntroSponsors

AIAA would like to thank the following organizations for their support of AIAA Propulsion and Energy 2016

Executive Sponsor Executive Sponsor and Student Reception Sponsor

Rising Leaders in Aerospace Sponsor Lanyard Sponsor

Sustaining Small Business and Tuesday Supporting Sponsors Afternoon Coffee Break Sponsor

Small Business Sponsor Media Sponsors

www.aiaa-propulsionenergy.org 7 #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. Monday, 25 July 1800–1900 hrs Ballroom A-D 0800–0900 hrs Ballroom A-D Keynote Address Formula for Success and Longevity in the Aerospace Business Innovate or Die! (Note: Dying is Easier) Moderators: Bonnie Prado Pino, Graduate Student, School of Bran Ferren, Co-Founder and Chief Creative Officer, Applied Aeronautics & Astronautics, Purdue University Minds, LLC Guillermo Jaramillo Pizarro, Ph.D. Candidate in Aeronautical Engineering, School of Aeronautics & Astronautics, Purdue 1330–1500 hrs Ballroom A-D University Panelists: System Needs in Propulsion and Energy David Bowles, Director, NASA Langley Research Center Moderator: Dan Dumbacher, Professor of Engineering Practice, Duane Cuttrell, Director, Operations Engineering and Technical School of Aeronautics and Astronautics, Purdue University Operations, Lockheed Martin Corporation Panelists: Rickey Shyne, Director, Research and Engineering, NASA Glenn Doug Blake, Director, Aerospace Systems Directorate, Air Force Research Center Research Laboratory Julie Van Kleeck, Vice President, Advanced Space and Launch Dennis Andrucyk, Deputy Associate Administrator, Space Business Unit, Aerojet Rocketdyne Technology Mission Directorate, NASA Wednesday, 27 July Tuesday, 26 July 0800–0900 hrs Ballroom A-D 0800–0900 hrs Ballroom A-D Keynote Address Game Changing Developments in Propulsion and e Impact of Additive Manufacturing on the Energy Design Process Moderator: Janet Kavandi, Director, NASA Glenn Research Center Elizabeth Robertson, Team Lead, Liquid Engine Systems Panelists: Branch, NASA Marshall Space Flight Center Jay Littles, Director, Advanced Launch Vehicle Propulsion, Aerojet Rocketdyne 1330–1500 hrs Ballroom A-D Tom Markusic, Co-Founder and Chief Executive Officer, Firefly Space Systems The Strategic Challenges and Opportunities in the James Maughan, Technical Director, Aero Thermal and Power and Propulsion Markets Mechanical Systems, GE Global Research Pierre Chao, Founding Partner, Renaissance Strategic Advisors

1300–1430 hrs Ballroom A-D High Power Systems for Aerospace Applications Moderator: Graham Warwick, Managing Editor, Technology, Aviation Week and Space Technology Panelists: Randy Furnas, Chief, Power Division, NASA Glenn Research Center John “Rick” Hooker, Design Engineer, Lockheed Martin Aeronautics John Nairus, Chief Engineer, Power & Control Division, Air Force Research Laboratory John H. Scott, Chief Technologist, Propulsion and Power (continued) Division, NASA Johnson Space Center www.aiaa-propulsionenergy.org 8 #aiaaPropEnergy The engine of change will come from the company that can build it. GE is bringing together best-in-class analytics and deep domain expertise to help our customers solve their toughest challenges. See how we’re changing the way we  y at geaviation.com.

85064_GEAV_DI_Print Ad_P+E.indd 1 7/5/16 3:55 PM ForumIntro 360 Tuesday, 26 July

0930–1200 hrs Ballroom F Liquid Rocket Propulsion: Lessons Learned Chair: T. Kent Pugmire, Retired Eric Besnard, Professor of Mechanical and Aerospace Engineering, California State University, Long Beach “Making Rocket Programs a Success in Universities” These conversations will cover a spectrum of Stephen Heister, Raisbeck Distinguished Professor, Director of timely topics including programs, systems, policy, the Maurice J. Zucrow Laboratory, Purdue University operations, applications, platforms and more! “History of the Maurice Zucrow Lab at Purdue University” John Steinmeyer, Business Development Director, Orbital ATK Monday, 25 July “International Cooperation on the Delta, Sea Launch and Antares Programs” 0930–1200 hrs Ballroom F Michael Kelly, Chief Engineer, FAA Office of Commercial Space Transportation, Federal Aviation Administration NRC Low-Carbon Aviation Report and “Lessons learned from industry, private venture, and federal Recommendations government” Moderator: Marty Bradley, Technical Fellow, Boeing Allan McDonald, Aerospace Consultant and Author of Truth, Commercial Airplanes Lies, and O-Rings: Inside the Space Shuttle Challenger Disaster “30 Years after Challenger - Ethics Lessons Learned but Panelists: Forgotten” Alan Angleman, Senior Program Officer, National Research Council Mike Benzakein, Wright Brothers Institute Professor, Assistant Vice President for Aerospace and Aviation, Office of Research, 1500 – 1800 hrs Ballroom F The Ohio State University Steve Csonka, Executive Director, Commercial Aviation Nuclear Power for Distant Solar System Alternative Fuels Initiative Destinations Alan Epstein, Vice President, Technology and Environment, Moderator: Lee Mason, Chief, Thermal Energy Conversions Pratt & Whitney Branch, NASA Glenn Research Center Karen Thole, Department Head and Professor, Mechanical and Panelists: Nuclear Engineering, Pennsylvania State University John Casani, NASA Jet Propulsion Laboratory (ret.) Leonard Dudzinski, Science Mission Directorate, NASA 1530–1800 hrs Ballroom F Rex Geveden, Chief Operating Officer, BWX Technologies, Inc. Patrick McClure, Los Alamos National Laboratory Launch Vehicle Reusability: Holy Grail, Chasing Susan Voss, President, Global Nuclear Network Analysis, LLC Our Tail, or Somewhere in Between? Moderator: Dan Dumbacher, Professor of Engineering Practice, School of Aeronautics and Astronautics, Purdue University Wednesday, 27 July Panelists: Ben Goldberg, Senior Director, Science and Engineering, 0930–1200 hrs Ballroom F Propulsions Systems Division, Orbital ATK Tom Markusic, Co-Founder and Chief Executive Officer, Firefly Rising Leaders in Aerospace — Forum 360 Space Systems Combined Session Jim Paulsen, Vice President Program Execution, Advanced This session will begin with Rex Geveden speaking about “Seven Space & Launch Programs, Aerojet Rocketdyne Career Hacks for Professional Success.” After that, there will be Gary Payton, Distinguished Visiting Professor, United States Air a round table of persons talking about their own and colleagues’ Force Academy professional success. Mr. Geveden will moderate and coordinate the question and answer period. www.aiaa-propulsionenergy.org 10 #aiaaPropEnergy ForumIntro 360

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

Sponsored by:

Monday, 25 July Wednesday, 27 July

1930–2100 hrs Ballroom H 0930–1200 hrs Ballroom F Dessert Reception Rising Leaders in Aerospace — Forum 360 This reception, which kicks off the Rising Leaders in Aerospace Combined Session events, is a perfect opportunity for young leaders to mingle This session will begin with Rex Geveden speaking about “Seven with others who will be participating at Propulsion and Energy Career Hacks for Professional Success.” After that, there will be 2016 as an attendee, presenter, or veteran professional. After the a round table of persons talking about their own and colleagues’ Exposition Hall Reception stop by for a little dessert with your professional success. Mr. Geveden will moderate and coordinate fellow young professionals. the question and answer period. Come meet other participants in a casual environment. You’re bound to see them again at the Speaker, Networking, Panel Events, or passing by in the hallways. Tuesday, 26 July

1000–1130 hrs Ballroom H Leadership Exchange/Speed Mentoring Senior members of corporations and AIAA will be taking time to meet with the Rising Leaders in Aerospace participants and share their experiences. This event is a great way to get insight from top-level officials and make some great new contacts. Spend 10 minutes speaking with a mentor, then rotate and spend 10 minutes with another mentor. Repeat until the end of the session. And who knows, maybe one or more will end up being a mentor for more than just the 10 minutes at this event. Don’t miss a terrific opportunity. Mentors include: Todd Barber, Jet Propulsion Laboratory John Casani, Jet Propulsion Laboratory Janet Convery, GE Aviation Mary Beth Koelbl, NASA Marshall Space Flight Center Robert Hancock, United States Air Force Sandy Magnus, AIAA Jimmy Tai, Georgia Institute of Technology Karen Thole, Pennsylvania State University

www.aiaa-propulsionenergy.org 11 #aiaaPropEnergy IntroNetworking and Special 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, 25 July, new contacts, continuing discussions from sessions, visiting 1800–1900 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 included in the registration fee the following times and locations: where indicated. Additional tickets may be purchased on site, as space is available. Monday, 25 July 0730–0800 hrs Foyer 0845–0930 hrs Exposition Hall AIAA Student Welcome Reception 1500–1530 hrs Exposition Hall Sunday, 24 July 2016, 1730–1900 hrs Ballroom H Tuesday, 26 July Mingle with your peers and hear from AIAA Executive Director Sandy Magnus. This reception provides you with the 0730–0800 hrs Foyer opportunity to meet your fellow students and learn more about 0845–0930 hrs Exposition Hall the opportunities available to you as an AIAA student member. 1430–1500 hrs Exposition Hall Sponsored by Sponsored by

Wednesday, 27 July 0730–0800 hrs Exposition Hall 0845–0930 hrs Exposition Hall Generation STEM AIAA Undergraduate Engine Design Competition Monday, 25 July, 1000–1430 hrs Exposition Hall Hosted by the AIAA Foundation and Lockheed Martin Wednesday, 27 July, 0930–1200 hrs Room 251B Corporation, Generation STEM will be a day filled with fun The AIAA Foundation and the GTE, ABPSI, and HSABP and interactive educational STEM experiences for middle Technical Committees have worked together to sponsor a school students. design competition. Undergraduate students from universities Generation STEM is designed to engage and stimulate students around the world were asked to prepare a design report to by allowing them to participate in mini design competitions respond to a Request for Proposal (RFP). This RFP asked and challenges, view engaging demonstrations from various students to design a candidate engine for a next-generation aerospace companies, learn more about aerospace careers, and trainer. discover aerospace findings that are impacting everyday life. All of the reports have been reviewed and scored by technical Conference attendees and exhibitors are encouraged to stop by experts, and this session features the top three proposal during the program to inspire and excite the next generation of winners, who have been invited to AIAA Propulsion and aerospace professionals. Or just come to observe the activities Energy 2016 to make an oral presentation to a panel of judges. and take ideas back to your section. Stop in for a few minutes These judges will assess the design, presentation, and responses or hang out for the afternoon. to questions. They will add their scores to those provided by the technical judges to come up with a 1st–3rd place ranking. Sponsored by: The final rankings will be announced at the conclusion of the session.

www.aiaa-propulsionenergy.org 12 #aiaaPropEnergy Recognition Event

AIAA celebrates our industry’s discoveries and achievements from the small but brilliantly simple innovations that affect everyday life to the major discoveries and missions that fuel our collective human drive to explore and accomplish amazing things. Wednesday, 27 July Energy Systems Award Ronald K. Hanson 1200–1330 hrs Ballroom G-J Clarence J. and Patricia R. Woodard Professor of Mechanical Engineering Recognition Luncheon—Celebrating Achievements Stanford University in Propulsion and Energy Stanford, California “For pioneering contributions on fundamental data provided A ticket for the luncheon is required and included in the from renewable and alternative fuels for applications to registration fee where indicated. Additional tickets for guests combustion engines, gasifiers and fluidized bed combustors for may be purchased upon registration or on site, as space is promoting fuel flexibility and performance of terrestrial energy systems.” available.

The following awards will be presented: Propellants and Combustion Award Aerospace Power Systems Award Ahmed F. Ghoniem Ronald C. Crane (1972) Professor, Mechanical Engineering Henry Brandhorst Massachusetts Institute of Technology Managing Director Cambridge, Massachusetts Aliquippa Holdings, LLC and CHZ Technologies, LLC Auburn, Alabama “For pioneering research and practical contributions to propulsion and power systems in Computational Fluid Dynamics “For over 55 years of developing aerospace power systems with and its application to turbulent combustion and combustion both space and terrestrial application, for providing exceptional dynamics.” leadership and innovation to the aerospace power system community and academia, and for significant contributions to AIAA.” Sustained Service Award Sanjay Garg Air Breathing Propulsion Award Chief, Intelligent Control and Autonomy Branch NASA Glenn Research Center Wesley Lord Cleveland, Ohio Technical Fellow, System Architecture Functional Design Pratt & Whitney “For three decades of significant and sustained contributions East Hartford, Connecticut advancing AIAA’s technical activities as an active member of multiple technical committees and standing committees.” “For 40 years of technical contributions advancing the state- of-the-art propulsors for commercial aircraft engines, reducing noise and improving fuel burn.” Wyld Propulsion Award Gary A. Flandro Engineer of the Year Award Boling Chair of Excellence in Mechanical and Aerospace Engineering (Emeritus), University of Tennessee Space Institute Robin J. Osborne Chief Engineer, Gloyer-Taylor Laboratories Senior Mechanical Engineer Tullahoma, Tennessee ERC, Inc./Jacobs-ESSSA Group Combustion Devices Design and Development Branch “For exceptional contributions to the knowledge base NASA Marshall Space Flight Center and technology implementation of rocket propulsion and Huntsville, Alabama astronautics, especially in solid and liquid propellant rocket combustion instability and interior ballistics.” “For increasing the aerospace industry’s understanding of spark torch ignition systems and building a low-cost ignition test facility.”

www.aiaa-propulsionenergy.org 13 #aiaaPropEnergy IntroRecognition Event

Certificates of Merit Liquid Propulsion Best Paper Air Breathing Propulsion Systems Integration Best Paper AIAA 2015-3769, “CFD Modeling of the Multipurpose AIAA 2016-0011, “Turbine Powered Simulator Calibration and Hydrogen Test Bed (MHTB) Self-Pressurization and Spray Testing for Hybrid Wing Body Powered Airframe Integration,” Bar Mixing Experiments in Normal Gravity: Effect of the Patrick Shea and Jeffrey Flamm, NASA Langley Research Accommodation Coefficient on the Tank Pressure,” Olga Center; Kurtis Long and Kevin James, NASA Ames Research Kartuzova and Mohammad Kassemi, NASA Glenn Research Center; and Daniel Tompkins and Michael Beyar, The Boeing Center. Company. Nuclear and Future Flight Propulsion Best Paper Electric Propulsion Best Paper AIAA 2015-3774, “Affordable Development and AIAA 2015-4005, “Non-Invasive Hall Current Distribution Demonstration of a Small NTR Engine and Stage: A Measurement in a Hall Effect Thruster,” Carl Mullins, Rafael Preliminary NASA, DOE and Industry Assessment,” Stanley K. Martinez, and John Williams, Colorado State University; Casey Borowski and Robert J. Sefcik, NASA Glenn Research Center; Farnell and Cody Farnell, Plasma Control LLC; David Liu, Air James E. Fittje and David R. McCurdy, Vantage Partners LLC; Force Institute of Technology; and Richard Branam, University Arthur L. Qualls and Bruce G. Schnitzler, Oak Ridge National of Alabama Tuscaloosa. Laboratory; James E. Werner, Idaho National Laboratory; Abraham Weitzberg, DOE Consultant; and Claude R. Joyner, Aerojet Rocketdyne. Energetic Components and Systems Best Paper AIAA 2015-3708, “Analysis of Dissipation Induced by Successive Planar Shock Loading of Granular Explosive,” Propellants and Combustion Best Paper Pratap Thamanna Rao and Keith A. Gonthier, Louisiana State AIAA 2015-3972, “Multi-Injector Impinging Jet Studies University. of Ignition Delay for Hydrogen Peroxide and Gelled Hydrocarbon Fuel Containing Reactive or Catalytic Particles,” Terrence L. Connell, Grant A. Risha, and Richard A. Yetter, Gas Turbine Engines Best Paper The Pennsylvania State University; and Benveniste Natan, AIAA 2015-4028, “A Composite Cycle Engine Concept with Technion—Israel Institute of Technology. Hecto-Pressure Ratio,” Sascha Kaiser, Bauhaus Luftfahrt e.V.; Stefan Donnerhack, MTU Aero Engines AG; Anders Lundbladh, GKN Aerospace Engine Systems; and Arne Seitz, Solid Rockets Best Papers Bauhaus Luftfahrt e.V. AIAA 2014-4016, “Improved Mean Flow Solution for Solid Rocket Motors with a Naturally Developing Swirling Motion,” Joseph Majdalani, Auburn University and Andrew Fist, Green Engineering Best Paper University of Tennessee. AIAA 2016-0267, “Impact of Ultra-High Bypass/Hybrid Wing Body Integration on Propulsion System Performance AIAA 2015-4107, “Time-Temperature Superposition Principle and Operability,” Wesley Lord, Gavin Hendricks, and Michael Applied to Thermally Aged Composite Propellant,” Luciene D. Kirby, Pratt & Whitney; and Stuart Ochs, Ray-Sing Lin, and Villar and Luis C. Rezende, Institute of Aeronautics and Space. Larry Hardin, United Technologies Research Center. Terrestrial Energy Best Paper High Speed Air Breathing Propulsion Best Paper AIAA 2016-0990, “Component and System Modeling of a AIAA 2016-0658, “Establishing the Controlling Parameters Direct Power Extraction System,” Omar D. Vidaña, Mariana of Ignition in High-Speed Flow,” Timothy Ombrello, Ez Chaidez, Brian Lovich, Jad Aboud, Manuel J. Hernandez, A. Hassan, and Campbell D. Carter, Air Force Research Luisa A. Cabrer, Ahsan Choudhuri, and Norman Love, The Laboratory; Brendan McGann, University of Notre Dame; University of Texas at El Paso. Hyungrok Do, Seoul National University; David M Peterson, Innovative Scientific Solutions, Inc.; and Philip Ivancic and Edward A Luke, Mississippi State University

www.aiaa-propulsionenergy.org 14 #aiaaPropEnergy The Partner You Can Count On™ Orbital ATK – Your Partner for Reliable and Affordable Propulsion Systems Orbital ATK provides reliable and flight-proven propulsion for the civil, defense and commercial markets. Through robust investments in advanced technology and sustained commitment to execution excellence, we are dedicated to providing leading edge technology solutions.

To learn more about Orbital ATK visit our website at OrbitalATK.com IntroITAR Information

A limited number of papers will be presented in “U.S. Only” technical sessions during the conference. In addition to your forum registration, a separate registration process is required to attend these restricted ITAR sessions. All individuals must bring the required documentation with them to the ITAR registration desk, most important is proof of U.S. Citizenship or Resident Alien Status. (Please note that a CAC card IS NOT official proof of U.S. Citizenship.) Please see the detailed information on the ITAR Registration Grid Information below to determine your individual requirements.

Access to ITAR Sessions: Presenting a Paper, Chairing a Availability of Manuscripts from ITAR-Restricted Sessions Session, or Attending an ITAR-Restricted Presentation For those who are registered to attend the ITAR sessions, a DVD Admittance to the restricted technical program is controlled by the containing the papers from the ITAR sessions will be available for U.S. International Traffic in Arms Regulations (ITAR). All attendees, purchase on site at the forum for $25. Those purchasing the DVD presenters, and session chairs will need to register for the conference, must be available to pick it up on Wednesday, 27 July 2016, between and then visit the ITAR registration desk to complete the additional 0900–1230 hrs at the ITAR Registration Desk. All DVDs must be processes. Anyone wishing to enter the restricted session room picked up in person. There will be no sale or distribution of these MUST abide by the procedures and submission of verified documents papers after the event. mandated by the DoD. No Exceptions! ITAR Badges must be worn during the sessions. Security will be checking photo IDs upon ITAR Electronics Policy entrance to the ITAR session rooms. No phones, computers (other than the presenter), iPads, cameras, Fitbits, or other electronic devices with cameras, recording or two- way transmission capabilities will be permitted into the ITAR session room. There will be a check-in desk in front of the room where you can check these devices. Large briefcases and bags will also need to be checked at the desk. Important session information for all attendees wishing to present or attend ITAR papers

AIAA Restricted Papers – ITAR Regulations Session Admittance Policy Several papers scheduled to be presented at this conference will be restricted DD Form 2345 individual certification credentials (required for U.S. & papers governed by ITAR (U.S. International Tra c in Arms Regulations). If Resident Aliens) MUST be from one of the following: you plan to attend any presentations restricted by ITAR, you must bring proof of 1. Copy of an approved and active DD2345 for the individual, OR citizenship PLUS the other verification documents as shown below. Please note that only U.S. Citizens and U.S. Resident Aliens can be considered for attendance 2. Copy of an approved and active DD2345 for the individual’s employer at these restricted presentations. Admittance to restricted sessions and access to PLUS evidence of current employment status with that employer restricted technical papers is implemented and controlled by ITAR . (corporate ID, business card, etc.), OR All restricted session attendees (including speakers and session chairs for 3. A listing of the individual’s employer in the most recent DoD quarterly these sessions) MUST abide by the procedures and submittal of verification Qualified U.S. Contractor Access List PLUS evidence of current documents as noted below – NO EXCEPTIONS: employment status with that employer (corporate ID, business card, etc.). DD Form 2345 may be downloaded and completed online in order to apply ATTENDEE CLASSIFICATION IDENTIFICATION & PROOF OF EMPLOYMENT for approval to be listed on the Qualified U.S. Contractor List, www.dlis. REQUIREMENTS dla.mil/jcp. Allow at least 4–6 weeks (or longer) prior to the AIAA technical conference dates for you to receive the approval and be listed on the Qualified U.S. Contractor List. U.S. Government Employees 1. Proof of U.S. Citizenship (for example, passport, birth certificate, naturalization papers), AND How to get your ITAR Clearance: NOTE: CAC Cards 2. Personal photographic identification: U.S. Bring all of the above listed identification, proof of employment and are NOT proof of Government/Military Photo ID badge, such as CAC card certification credentials to the AIAA ITAR Registration Desk in the AIAA citizenship. Registration area. Your documents will be verified and you will be provided with a stamp U.S. Citizens 1. Proof of U.S. Citizenship (for example, passport, indicating your ITAR clearance. Photo ID will be checked against your ITAR birth certificate, naturalization papers), AND badge before admittance is granted to any ITAR presentation. 2. Personal photographic identification (passport, Please be advised that all policies and procedures MUST be followed or driver’s license, etc.), AND 3. Certification credentials based on DD Form 2345 admittance to restricted sessions will not be permitted. (see below for details) Please see the ITAR Registration Desk Resident Aliens (U.S.) 1. Resident Alien Card, AND 2. Personal photographic identification (passport, with any questions. driver’s license, etc.), AND 3. Certification credentials based on DD Form 2345 (see below for details) www.aiaa-propulsionenergy.org 16 #aiaaPropEnergy Get Your Conference Info on the Go!

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My Itinerary For optimal use, we recommend • For optimal use, we recommend: iPhone 3GS, iPod Touch (3rd generation), s iPhone 3GS, iPod Touch (3rd Create your own conference iPad iOS 4.0, or later generation), iPad iOS 4.0, or later schedule Download the MyItinerary app by s Most mobile devices using Android searching for “ScholarOne” in the App 2.2 or later with the default browser Conference Info Store directly from your mobile device. Or, Including special events access the link below or scan the QR code s BlackBerry Torch or later device to access the iTunes page for the app. using BlackBerry OS 7.0 with the default browser Take Notes http://itunes.apple.com/us/ Take notes during sessions app/scholarone-my-itinerary/ • Download the MyItinerary app by id497884329?mt=8 scanning the QR code or accessing http://download. City Map Select the meeting “AIAA Propulsion and abstractcentral.com/aiaa- Energy 2016” See the surrounding area and the mpe16/index.htm Salt Palace Convention Center • Once downloaded, you can bookmark the site to access it later or add a link Connect to Twitter to your home screen. Tweet about what you’re doing and who you’re meeting with #aiaaPropEnergy IntroExposition Hall

EXITSEXITS

AIAA Sales Office AIAA Pavilion Tecplot, Inc. Exhibitor/ Corporate AEDC Valcor

BETA CAE PCB Pointwise Piezotronics Systems USA

CD-adapco Marotta

Cambridge University Press Vacco Industries Keystone Magellan Engineering Aerospace Company

General Rolls- Cobham Intelligent Dynamics Light OTS Royce

JASC Army Controls Research Rocketdyne Lab Orbital ATK Worthington Industries Graphite UTEP UCRI

ENTRANCE Exhibitors by Booth Number (êindicates AIAA Corporate Members)

319 Aerion Technologies ê 421 MTU Aero Engines AG 401 Aerojet Rocketdyne ê 520 MTU Aero Engines North America Inc. 602 Army Research Lab 407 NASA ê 417 Arnold Engineering Development Complex (AEDC) 301 Orbital ATK 609 Barber-Nichols Inc. 314 PCB Piezotronics 514 BETA CAE Systems 501 Poco Graphite 311 Cambridge University Press 415 Pointwise, Inc. ê 213 CD-adapco 406 Rolls-Royce Corporation ê 215 CF Turbo Software and Engineering GmbH 418 Tecplot, Inc. ê 110 Cobham 601 University of Cincinnati Research Institute (UCRI) 107 ESTECO 104 University of Notre Dame Turbomachinery ê 201 GE Aviation Laboratory 307 General Dynamics — OTS 600 University of Texas at El Paso Department of 206 Intelligent Light ê Mechanical Engineering (UTEP) 502 Jansens Aircraft Systems Controls 408 VACCO Industries 309 Keystone Engineering Company 516 Valcor Engineering Corporation 208 Magellan Aerospace 500 Worthington Industries (SCI) 312 Marotta Controls, Inc. 101 Moog www.aiaa-propulsionenergy.org 18 #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, 25 July 0845–1600 hrs Stop by the AIAA Pavilion, located in the Exposition Hall, Networking Coffee Breaks 0845–0930 hrs to browse publications and merchandise, learn about your membership benefits, and meet AIAA staff. 1500–1530 hrs Generation STEM 1000–1430 hrs 30% off All Books at AIAA Propulsion and Energy 2016 Reception* 1800–1930 hrs AIAA is offering a special discount on all titles featured at AIAA Tuesday, 26 July 0845–1600 hrs Propulsion and Energy 2016. Attendees can take advantage of a 30% discount off the list price of all books for sale at the AIAA Networking Coffee Breaks 0845–0930 hrs Bookstore located in the AIAA Pavilion. This special offer will 1430–1500 hrs only be available during the forum! Take advantage of these Networking Luncheon* 1200–1300 hrs super savings and visit the AIAA Bookstore! Wednesday, 27 July 0845–1200 hrs Networking Coffee Break 0845–0930 hrs AIAA Foundation Silent Auction Come visit us in the AIAA Pavilion. Did you know that the *A ticket is required to attend the reception and the networking AIAA Foundation is celebrating its 20th anniversary? To raise luncheon funds for our STEM programming, we are hosting a Silent Auction with some cool aerospace items for bid. Stop by and check it out! With your help and donation, we can reach our goal and continue to inspire and support the next generation of aerospace professionals.

Quadcopter Raffle Enter to win one of two quadcopters! Complete the raffle ticket (behind your registration badge) and drop it in the boxes in the Exposition Hall by 1200 hrs, Wednesday, 27 July. Winner will be notified by email and does not need to be present to win.

Go To The Movies Courtesy of Orbital ATK! Visit their booth (#301) for a pass to the nearby Clark Planetarium. The pass gets you in to any show at the Orbital ATK IMAX Theatre or the Hansen Dome Theatre, 24–27 July. http://clarkplanetarium.org/

www.aiaa-propulsionenergy.org 19 #aiaaPropEnergy Exhibitors Aerion Technologies 319 Barber-Nichols Inc. 609 1900 Embarcadero Rd. #101 6325 West 55th Avenue Palo Alto, CA 94303 Avenue Arvada, CO 80002 www.aerion-tech.com www.barber-nichols.com [email protected] [email protected] Aerion Technologies (formerly Desktop Aeronautics) creates Celebrating our 50th year in business, Barber-Nichols is tools for aerodynamic design and analysis of aerospace the industry leader in the rapid design and manufacture of vehicles. Our flagship product, GoCart, is an intuitive aerial specialty, state-of-the-art, rotating machinery including Rocket vehicle design tool built around NASA’s renowned Cartesian Engine Turbopumps and Prototype Power Systems. Our fully Euler CFD solver, Cart3D. Our customer list includes the integrated engineering and production facilities allow our major players from the aerospace and defense industry. highly experienced team to quickly transition our customers’ dreams to validated products.” Aerojet Rocketdyne 401 2001 Aerojet Road BETA CAE Systems 514 Rancho Cordova, CA 95742 29800 Middlebelt Road, Suite 100 www.aerojet.com Farmington Hills, MI 48334 [email protected] www.ansa-usa.com Aerojet Rocketdyne, is a world-recognized aerospace and [email protected] defense leader providing propulsion and energetics to BETA CAE Systems is an engineering services company that the space, missile defense, strategic, tactical missile, and distributes & supports the industry leading ANSA & META armaments areas in support of domestic and international software. ANSA is a CAE pre-processing tool for FE & CFD markets. Additional information about Aerojet Rocketdyne is Analysis, for full-model build, from CAD to solver input file, available online at www.Rocket.com. in one integrated environment. META is a post-processor for analyzing results from ANSYS, NASTRAN, ABAQUS, LS- DYNA, PAMCRASH, RADIOSS, MADYMO & other solvers. Army Research Lab 602 RDRL-WM Cambridge University Press 311 Aberdeen Proving Ground, MD 21005 www.arl.army.mil 32 Avenue of the Americas [email protected] New York, NY 10013-2473 The U.S. Army Research Laboratory is The Nation’s Premier www.cambridge.org/us Laboratory for Land Forces. ARL conducts basic and [email protected] exploratory research and advanced technology development in Cambridge’s publishing in books and journals combines state- a wide variety of areas, including vehicle propulsion,energetic of-the-art content with the highest standards of scholarship, materials, functional materials, power and energy, and writing and production. Visit our stand to browse new titles, manufacturing science. Specifically, ARL manages three available at a 20% discount, and to pick up sample issues of our of its seven primary S&T campaigns related to propulsion journals. Visit our website to see everything we do: and energy: Sciences for Maneuver, Materials Research,and www.cambridge.org/engineering Sciences for Lethality and Protection. CD-adapco 213 Arnold Engineering 417 60 Broadhollow Rd Development Complex (AEDC) Melville, NY 11747 100 Kindel Dr. Suite A242 www.cd-adapco.com [email protected] Arnold AFB, TN 37389 www.arnold.af.mil CD-adapco (http://www.cd-adapco.com) is a global [email protected] engineering simulation company with a unique vision for Arnold Engineering Development Complex develops, Multidisciplinary Design eXploration (MDX). Engineering tests and evaluates weapon, propulsion, aerodynamic and simulation provides the most reliable flow of information space systems at realistic conditions for the nation through into the design process, which drives innovation and lowers modeling, simulation and ground test facilities. We operate product development costs. CD-adapco simulation tools, led 28 aerodynamic and propulsion wind tunnels, rocket and by the flagship product STAR-CCM+®, allow customers to turbine engine test cells, space environmental chambers, arc discover better designs, faster. heaters, ballistic ranges and other specialized units - many are unmatched in the United States; some are unique in the world. AEDC is part of the Air Force Test Center, one of six centers of the Air Force Materiel Command. www.aiaa-propulsionenergy.org 20 #aiaaPropEnergy Exhibitors

CF Turbo Software & Engineering GmbH 215 General Dynamics —OTS 307 Unterer Kreuzweg 1 4300 Industrial Avenue Dresden Deutschland 01097 Lincoln, NE 68504 http://en.cfturbo.com/home.html www.gd-ots.com [email protected] [email protected] CFturbo Software & Engineering GmbH founded in 2008 General Dynamics Ordnance and Tactical Systems provides offers sophisticated design software and engineering reliable and affordable composite products to the defense and solutions especially for conceptual design of Turbomachinery commercial aerospace markets. With more than 50 years of components whereas today CFturbo® can be used to expertise, General Dynamics designs, develops, manufactures create axial, radial and mixed- flow pumps, blowers, fans, and tests a full range of composite missile and space structures, compressors and turbines. Additionally our company offers a including rocket motors, pressure vessels, launch tubes, drive wide range of consulting and engineering services including shafts and fuel tanks. design, simulation, optimization, prototyping and testing. Intelligent Light 206 Cobham 110 301 Route 17 N. 7th Floor 10 Cobham Drive Rutherford, NJ 07070 Orchard Park, NY 14127 www.ilight.com www.cobham.com [email protected] [email protected] Intelligent Light provides post-processing, data management Cobham builds on extensive space flight heritage with and big data visualization capability for CFD. Thousands of innovative propulsion solutions that support chemical, electric users rely on the industry leading FieldView software and our and cold gas systems. Leveraging decades of component custom engineering services to maximize their productivity design, Cobham has developed a variety of integrated pressure and effectiveness. Let us help you eliminate bottlenecks and control assemblies for propulsion applications for the launch achieve breakthrough results. vehicle and satellite market. Cobham has expanded beyond our standard propulsion offerings for the dynamic small sat market with integrated propulsion modules optimized for Jansens Aircraft Systems Controls 502 individual customer requirements. (JASC-Controls) 2303 W. Alameda Drive Tempe, AZ 85282 ESTECO 107 www.jasc-controls.com 39555 Orchard Hill Place #457 [email protected] Novi, MI 48375 www.esteco.com JASC is a custom engineering, design and manufacturing [email protected] company located in Tempe, AZ. Our expertise in flow controls has allowed us to achieve great success in the most demanding ESTECO is a pioneer in numerical optimization aerospace, aviation, gas turbine and military projects. Whether solutions, specializing in the research and development the challenge is cryogenic, high temperature, high pressure of engineering software for all stages of the simulation- or thermal cycling in nature, our control technology brings driven design process. ESTECO’s top-class products, customer performance ideas to reality. modeFRONTIER and SOMO, are used worldwide, helping companies increase efficiency in design simulation and accelerate product innovation. Keystone Engineering Company 309 4401 Donald Douglas Drive Long Beach, CA 90808 GE Aviation 201 www.keyengco.com One Neumann Way, MD G414 [email protected] Cincinnati, OH 45215 Keystone is a world leader in the design and fabrication of www.ge.com/aviation engineered products used in critical flight-weight aerospace GE Aviation, an operating unit of GE (NYSE: GE), is a world- and defense applications. Keystone core competencies include leading provider of jet and turboprop engines, components, the design, analysis, and production of light-weight propellant integrated digital, avionics, electrical power and mechanical and pressure storage tanks, spun domes for satellites and systems for commercial, military, business and general aviation launch vehicles, spun liners and jackets for launch vehicles, aircraft. GE Aviation has a global service network to support large diameter aircraft bearing systems and other specialized these offerings and is part of the world’s Digital Industrial engineered products for various defense and aerospace Company with software-defined machines and solutions. For applications. more information, visit us at www.ge.com/aviation. www.aiaa-propulsionenergy.org 21 #aiaaPropEnergy ExhibitorsIntro

Magellan Aerospace 208 MTU North America 520 2320 Wedekind Drive 795 Brook Street, Bldg. 5 Middletown, OH 45042 Rocky Hill, CT 06067 www.magellan.aero www.mtuusa.com [email protected] [email protected] Magellan Aerospace, Middletown, Inc. designs, analyzes and MTU Aero Engines North America (MTU AENA), a U.S. manufactures high temperature capable structures for the company, is a subsidiary of MTU Aero Engines. We provide a aerospace industry. By integrating the internal honeycomb full range of engineering services to customers in the aerospace manufactured products into brazed structural panels, high and power generation industries. Our core competencies focus temperature light weight components are delivered. Structural on program management and engineering services (design, applications for these components include control surfaces, analytics, project and repair engineering) for gas turbines. exhaust systems (acoustic and non-acoustic), fairings and heat Innovation backed by precision engineering stands behind the shields. The Middletown facility utilizes Inconel, stainless company’s reputation for solutions tailored to each customer’s steel, and titanium alloys for these applications while also individual needs. producing complex aluminum assemblies. NASA 407 Marotta Controls, Inc. 312 300 E Street Southwest 78 Boonton Avenue, PO Box 427 Washington, DC 20546 Montville, NJ 07045 www.nasa.gov www.marotta.com [email protected] [email protected] Since its inception in 1958, the National Aeronautics and Space Simplify your system and save up to 50% weight and cost with Administration (NASA) has sought to reach for new heights Marotta’s advanced satellite propulsion controls. Discover and reveal the unknown so that what we do and learn will how our flight qualified, TRL9, ITAR-free technology can benefit all humankind. NASA’s priorities are: Earth Right Now significantly reduce the number of components in your Xenon – Your Planet is Changing. We’re on It; Aeronautics– We’re feed system. Stop by Booth #312 to meet our team and learn with You When You Fly; International Space Station – Off more. the Earth, For the Earth; Journey to Mars; Solar System and Beyond; and Technology Powering Exploration. For more information, visit us at: www.nasa.gov. Moog 101 500 Jamison Rd., PO Box 18 East Aurora, NY 14052 Orbital ATK 301 www.moog.com/space PO Box 707 [email protected] Brigham City, UT 84302 Moog supplies critical components, subsystems and systems www.atk.com for access to and operation in space, including: thrust vector [email protected] control, avionics, propulsion components, subsystems ATK is on the forefront of R&D and manufacture of solid rocket and systems, spacecraft thrusters, antenna and solar array propulsion, aircraft structures, missile components, small sats, positioners, and vibration isolation. Moog is making solar arrays, satellite components, and flares and decoys. ATK significant investments this year in propulsion facilities, provides affordable solutions to meet emerging needs. metal additive manufacturing, avionics, and in-space payload dispensing systems. PCB Piezotronics 314 3425 Walden Ave MTU Aero Engines AG 421 Depew, NY 14043 Dachauerstrasse 665 www.pcb.com Munich, Germany 80995 [email protected] www.mtu.de/brushseals PCB PIEZOTRONICS, INC. is a designer, manufacturer, MTU Aero Engines North America (MTU AENA), a U.S. and global supplier of accelerometers, microphones, force, company, is a subsidiary of MTU Aero Engines. We provide a torque, load, strain, and pressure sensors, as well as the full range of engineering services to customers in the aerospace pioneer of ICP® technology. This instrumentation is used for and power generation industries. Our core competencies focus test, measurement, monitoring, and control requirements in on program management and engineering services (design, automotive, aerospace, industrial, R&D, military, educational, analytics, project and repair engineering) for gas turbines. commercial, OEM applications, and more. PCB® proudly stands behind their products with services such as 24- hour technical support, a global distribution network, and commitment to Total Customer Satisfaction. www.pcb.com. www.aiaa-propulsionenergy.org 22 #aiaaPropEnergy IntroExhibitors

Poco Graphite 501 Univ. of Cincinnati Research Institute (UCRI) 601 300 Old Greenwood Road 260 Stetson Street Suite 5300 Decatur, TX 76234 Cincinnati, OH 45219 UNIVERSITY of CINCINNATI www.poco.com www.ucri.org/[email protected] RESEARCH INSTITUTE Poco Graphite is a leading manufacturer of Graphite, SiC, In our rapid-fire, knowledge-driven economy, smarts rule. Carbon Foam, and Coating Materials for use in Propulsion That’s why UCRI helps businesses tap into the world–class and Turbine applications. POCO materials are used in extreme expertise and resources found in virtually every hallway on environments, including systems that require precision & high the UC campus. We’re a separate organization from UC, but performance. Typical applications are bushings, thrust washers, closely affiliated and well connected. We’re business people rings, seals, and thermal management systems. 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. Pointwise 415 213 South Jennings Avenue Fort Worth, TX 76104 University of Notre Dame 104 www.pointwise.com Turbomachinery Laboratory [email protected] 1165 Franklin Street, Suite 200 Pointwise, Inc. is solving the top problem facing engineering South Bend, IN 46601 analysts today: mesh generation for computational fluid www.turbo.nd.edu [email protected] dynamics. The Pointwise software cuts time spent to generate The Notre Dame Turbomachinery Laboratory in South high-quality meshes. Multiple-level undo and redo and a Bend, IN focuses on research, testing, and development of modern, flat graphical interface make it even easier to use. applications that involve turbomachinery technology. With Come by for a quick demo! shaft powers from 700-12,000 hp, the 28,000-square-foot lab facility offers capabilities for the development of high power level rotating machinery in a secured, export-controlled Rolls-Royce Corporation 406 environment. Computational capabilities include in-house and 450 S. Meridian Street, commercial software for structural and fluid-flow analysis and Indianapolis, IN 46225 a large-scale HPC cluster. www.Rolls-Royce.com At Rolls-Royce LibertyWorks, we develop solutions for everything from advanced VTOL technology to high-speed University of Texas at El Paso 600 flight. We provide technology the US warfighter needs Department of Mechanical Engineering to perform the mission. We value our relationships with 500 W. University Ave airframers, Army Advanced Technology Division, DARPA, El Paso, TX 79968 NASA, AFRL, Naval Research Laboratory, and advanced research.utep.edu/Default.aspx?alias=research.utep.edu/csetr technology consortiums. [email protected] The MIRO Center for Space Exploration and Technology Tecplot, Inc. 418 Research (cSETR) was established at The University of Texas at El Paso (UTEP) to promote research and education in the 3535 Factoria Blvd SE, Ste 550 areas of Aerospace and Defense Systems, Energy Engineering, Bellevue, WA 98006 and Crosscutting Technologies. The MIRO cSETR vision is www.tecplot.com to establish a sustainable minority serving university center of [email protected] excellence in advanced propulsion research through strategic Tecplot software empowers engineers and scientists working partnerships and to educate a diverse future aerospace with computational fluid dynamics (CFD) to discover, analyze, workforce. and understand information in complex data, and to effectively communicate their results to others via brilliant images and compelling animations. Tecplot products are used by more than 47,000 technical professionals around the world.

www.aiaa-propulsionenergy.org 23 #aiaaPropEnergy IntroExhibitors

VACCO Industries 408 Worthington Industries 500 10350 Vacco Street 336 Enterprise Place South El Monte, CA 91733 Pomona, CA 91768 www.vacco.com www.worthingtoncylinders.com [email protected] [email protected] VACCO® specializes in design and production of engineered Manufacturer of Composite Overwrapped Pressure Vessels fluid controls for human-rated, long duration and expendable and Structures. space applications. Proven Valves, Regulators, Filters, Couplings, Refueling Mechanisms, Welded Manifolds, and highly-integrated ChEMS™ Modules are available for applications ranging from cryogenic to high pressure and hazardous propellants. Reliable heritage products for Intelligent solutions. Valcor Engineering Corporation 516

2 Lawrence Road ® Springfield, NJ 07081 VALCOR www.valcor.com [email protected] Valcor Aerospace specializes in the design and manufacture of custom valves and control components (solenoid, relief, check, fill & drain valves, pressure regulators, accumulators, actuators) for liquids (propellants, fuel, hydraulic fluid) and gases in critical aerospace (aircraft, launch vehicle, missile, spacecraft, etc.) applications.

www.aiaa-propulsionenergy.org 24 #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 at the Salt Palace Convention Center. Hours are as follows: is included in the registration fee where indicated. Online proceedings will be available on Monday, 25 July. Attendees Sunday, 24 July 1500–1900 hrs who register in advance for the online proceedings will be Monday, 25 July 0700–1800 hrs provided with instructions on how to access them. Those registering on site will be provided with instructions at that Tuesday, 26 July 0700–1800 hrs time. Wednesday, 27 July 0700–1800 hrs Proceedings: 1. To view proceedings, visit Wi-Fi Internet Access On Site www.aiaa.org >ARC>Meeting Papers. AIAA is providing limited Wi-Fi service for attendees to use a. Log in with the link at the top right of the page. while on site. To keep this service available and optimized for b. Select the appropriate conference from the list. all attendees, please do not download files larger than 2MB, create multiple sessions across multiple devices, or download c. Search for individual papers with the Quick Search toolbar multiple files in one session. If you receive an error message in the upper-right corner of the page: that an AIAA server is blocking your current IP address, please i. By paper number: Click the Paper Number link, select inform the AIAA registration desk. the conference year, and enter the paper number. Network Name: AIAA Password: propenergy ii. Use the Search textbox to find papers by author, title, or keyword. The Advanced Search link provides additional search information and options. AIAA Livestream Channel 2. All manuscript files submitted by four days prior to the Visit livestream.com/aiaavideo/PropEnergy2016 to view conference are currently in the proceedings. Files submitted selected keynotes, plenaries, and Forum 360 sessions. Share the after that date, both original and revised manuscripts, will link with colleagues who couldn’t attend the forum, so they can not be available until the final proceedings update, which watch live or view later. may take up to 15 business days after the last day of the conference. 3. Direct any questions concerning access to proceedings and/ Social Media Kiosks or ARC to [email protected]. Throughout the forum, social media kiosks will display content shared by forum attendees! Look for your tweets or Instagram photos to be displayed on the screens if you’ve Manuscript Revisions used our hashtag #aiaaPropEnergy. AIAA is also hosting a competition where the user who has posted the most tweets 1. Manuscript revision is open for all presenting authors during the forum will win a prize. from 0900 hrs Eastern Time, Monday, 25 July, through 2000 hrs Eastern Time, Friday, 5 August. 2. Revisions submitted for manuscripts already online will ITAR Registration Hours not refresh until after the proceedings have been updated, which may take up to 15 business days after the last day Monday, 25 July 0700–1800 hrs of the conference. Located in Ballroom Foyer Tuesday, 26 July 0700–1800 hrs Certificate of Attendance Located outside Room 151 DE Certificates of Attendance are available for attendees who Wednesday, 27 July 0700–1800 hrs request documentation at the forum itself. The Certificates of Attendance will be available for attendees to print at a Located outside Room 151 DE self-service station at the registration desk starting Tuesday, 26 July. AIAA offers this service to better serve the needs of DVD pickup for those ITAR attendees purchasing a the professional community. Claims of hours or applicability DVD is Wednesday, 27 July, 0900–1500 hrs at the ITAR toward professional education requirements are the Registration Desk. responsibility of the participant.

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

Employment Opportunities Young Professional Guide for Gaining AIAA members can post and browse resumes, browse job Management Support listings, and access other online employment resources by Young professionals have the unique opportunity to meet and visiting the AIAA Career Center at http://careercenter.aiaa.org. learn from some of the most important people in the business Additionally, a message board will be available for postings in by attending conferences and participating in AIAA activities. the Exposition Hall. A detailed online guide, published by the AIAA Young Professional Committee, is available to help you gain support and financial backing from your company. The guide explains Membership the benefits of participation, offers recommendations, and provides an example letter for seeking management support AIAA is your vital lifelong link to the collective creativity and and funding, and shows you how to get the most out of your brainpower of the aerospace profession and a champion for its participation. The online guide can be found on the AIAA achievements – and nonmembers who pay the full conference website at www.aiaa.org/YPGuide. registration fee will receive their first year’s AIAA membership at no additional cost! Students who are not yet members may apply their registration fee toward their first year’s student member dues. (Free membership is not included in discounted Nondiscriminatory Practices group-rate registration.) AIAA accepts registrations irrespective of race, creed, sex, color, physical handicap, and national or ethnic origin. AIAA Foundation In celebration of the AIAA Foundation’s 20th anniversary, we Restrictions have challenged AIAA members to donate at least $20 to the Photos, video, or audio recording of sessions or exhibits, as foundation. To date, we have raised more than $99,000 on our well as the unauthorized sale of AIAA-copyrighted material, is way to the goal of $200,000! With your gift, we can continue prohibited. to enhance and create K–12 STEM programs, including classroom grants and hands-on activities, university design competitions, student conferences and recognition awards. To show support of our programming and goal, the Institute International Traffic in Arms Regulations (ITAR) will match individual and corporate donations up to one AIAA speakers and attendees are reminded that some million dollars of unrestricted funds. Your gift will be matched, topics discussed in the conference could be controlled doubling the impact of your donation, so please consider by the International Traffic in Arms Regulations (ITAR). donating today. For more information and to make a tax- U.S. nationals (U.S. citizens and permanent residents) are deductible donation, please visit www.aiaafoundation.org. responsible for ensuring that technical data they present in open sessions to non-U.S. nationals in attendance or in conference proceedings are not export restricted by the ITAR. U.S. nationals are likewise responsible for ensuring that they do not discuss ITAR export-restricted information with non-U.S. nationals in attendance.

www.aiaa-propulsionenergy.org 26 #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. that AIAA does not provide security in the session rooms and Speakers’ Briefing schedule is as follows: recommends that items of value not be left unattended. Monday, 25 July – Wednesday, 27 July: 0730 hrs “No Paper, No Podium” and “No Podium, No Speakers’ Practice Room Paper” Policy Speakers who wish to practice their presentations may do so If a written paper is not submitted by the final manuscript in the Convention Office #4 room located at the Salt Palace deadline, authors will not be permitted to present the paper at Convention Center. A sign-up sheet will be posted on the the forum. Also, if the paper is not presented at the forum, it door. In consideration of others, please limit practice time to will be withdrawn from the proceedings. It is the responsibility 30-minute increments. of those authors whose papers or presentations are accepted to ensure that a representative attends the conference to present Session Chair Reports the paper. These policies are intended to improve the quality 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 Session Chair Report form. You can download the FREE Authors of appropriate papers are encouraged to mobile app in your App Store, AppWorld, or Marketplace submit them for possible publication in one of the Institute’s by searching for “Canvas Solutions, Inc.” The mobile app is archival journals: AIAA Journal; Journal of Aerospace free, so please be sure to download it. Detailed instructions Information Systems; Journal of Air Transportation; Journal will be provided in the session rooms. If you do not have of Aircraft; Journal of Guidance, Control, and Dynamics; a tablet or a smartphone, simply use the report form as a Journal of Propulsion and Power; Journal of Spacecraft and guide and enter your session chair report information at the Rockets; or Journal of Thermophysics and Heat Transfer. You session chair reporting computer station located on site near may now submit your paper online at the AIAA registration area. Report data will be collected and http://mc.manuscriptcentral.com/aiaa. used for future planning purposes, including session topics and room allocations. Please submit your session chair report electronically by Wednesday, 27 July 2016.

You Innovate. AIAA Helps You Communicate. Learn more and register for KUDOS at AIAA has partnered with KUDOS to help our authors www.growkudos.com bring their work to the attention of their peers, the media, and broader audiences both in and outside the aerospace community. You have done the important research – now you can increase its visibility. KUDOS is a web-based service that allows authors to claim, explain and share their work. Doing so increases the downloads of full-text articles by 23%.

www.aiaa-propulsionenergy.org 27 #aiaaPropEnergy IntroCommittee Meetings Time Title Location Saturday, 23 July 2016 0800-1700 hrs Advanced High-Speed Air-Breathing Propulsion Technology Course Room 254B 0800-1700 hrs Electric Propulsion for Space Systems Course Room 254A 0800-1700 hrs Hybrid Rocket Propulsion Course Room 254C 0800-1700 hrs Fundamentals of Liquid Chemical Propellants Room 255A 0800-1700 hrs Propulsion Aerodynamics Workshop Room 255E/F Sunday, 24 July 2016 0800-1700 hrs Advanced High-Speed Air-Breathing Propulsion Technology Course Room 254B 0800-1700 hrs Electric Propulsion for Space Systems Course Room 254A 0800-1700 hrs Hybrid Rocket Propulsion Course Room 254C 0800-1700 hrs Fundamentals of Liquid Chemical Propellants Room 255A 0800-1700 hrs Propulsion Aerodynamics Workshop Room 255E/F 1400-1900 hrs Electric Propulsion Discussion Room 150DE 1700-2000 hrs TAC Propulsion and Energy Group Meeting Room 255B 1730-1900 hrs AIAA Student Welcome Reception East Lobby Monday, 25 July 2016 0800-0900 hrs HSABPTC Prep Committee Room 355A 0900-1000 hrs ABPTCs Steering Committee Room 355A 1000-1100 hrs HSABPTC Steering Committee Room 355A 1000-1030 hrs ABPTCs New Member Orientation Room 355D 1030-1100 hrs GTETC Membership Upgrade Room 355D 1100-1200 hrs ABPSI TC Meeting Room 355A 1100-1200 hrs GTE TC Meeting Room 355D 1100-1200 hrs HSABP TC Meeting Room 355C 1200-1500 hrs Nuclear and Future Flight Propulsion TC Room 355E 1300-1400 hrs HyTASP PC Steering Committee Meeting Room 355A 1300-1400 hrs ABPTCs Conference Subcommittee Room 355C 1400-1600 hrs HyTASP PC Room 355F 1400-1500 hrs ABPTCs Honors and Awards Subcommittee Room 355A 1500-1600 hrs TAC P&E Group Coordination Room 355A 1500-1600 Hrs ABP Student Engine Design Competitiion Room 355C 1600-1700 hrs ABPTCs Communications Subcommittee Room 355A 1700-1800 hrs ABP Working Groups Room 355E 1700-1900 hrs GEPC Leadership & Conference Team Room 355D 1900-2200 hrs Terrestrial Energy Systems TC Room 355A 1900-2130 hrs Propellants and Combustion TC Room 355B 1900-2200 hrs Energetic Components and Systems TC Room 355C 1900-2200 hrs Solid Rockets TC Room 355E 1900-2200 hrs ABPTCs Group Meeting Room 355F 1930-2100 hrs RLA Dessert Reception Ballroom H

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Time Title Location Tuesday, 26 July 2016 0900-1100 hrs TAC Rocket, Space and Advanced Propulsion Group Room 355A 1000-1130 hrs 2017 Technical Program Committee Room 355F 1500-1600 hrs TAC P&E Group Tag-up Room 355A 1700-1930 hrs Green Engineering PC Room 355A 1800-2000 hrs Pressure Gain Combustion PC Room 355D 1830-2100 hrs Electric Propulsion TC Room 355E 1800-2200 hrs Aerospace Power Systems TC Room 355C 1900-2200 hrs Hybrid Rockets TC Room 355F Wednesday, 27 July 2016 1400-1500 hrs TAC P&E Energy TC Leadership Group Room 150C 1900-2200 hrs Liquid Propulsion TC Room 355F

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Sessions at a Glance Overview

Energy-Focused Topic Areas Propulsion-Focused Topic Areas Advanced Power Systems (APS) Air Breathing Propulsion Systems Integration (ABPSI) Energy Conversion Device Technology (ECD) Additive Manufacturing (ADP) Electricity Delivery, Grid and Energy Storage Technologies (EDES) Advanced Engine Control (AEC) Energy Efficiency (EE) Aircraft Electric Propulsion (AEP) Energy Optimized Aircraft and Equipment Systems (EOA) Energetic Components and Systems (ECS) Fossil-Fuel Power (FFP) Propulsion Education (EDU) Green Engineering (GEPC) Energy Optimized Aircraft and Equipment Systems (EOA) Thermal Managent (TM) Electric Propulsion (EP) Thermal Management Technology (TM) Gas Turbine Engines (GTE) Green Engineering (GEPC) Hybrid Rockets (HR) High Speed Air Breathing Propulsion (HSABP) Liquid Propulsion (LP) Nuclear and Future Flight (NFF) Propellants and Combustion (PC) Propulsion and Power Systems (PP) Satellites (SATS) Solid Rockets (SR) Vehicle Systems (VS)

Abbreviation Title Date Start Time Location Air Breathing Propulsion Systems Integration (ABPSI) 3-ABPSI-1 Nozzles and Exhaust 25-Jul 0930 hrs 255 F 32-ABPSI-2 High-Speed Inlets 25-Jul 1530 hrs 255 F 64-ABPSI-3 Supersonic and Hypersonic Inlets 26-Jul 0930 hrs 255 F 93-ABPSI-4 Subsonic Inlets & Aerodynamic Interaction 26-Jul 1500 hrs 255 F 150-ABPSI-5 Propulsion Systems Integration 27-Jul 1500 hrs 255 F 137-GTE-15/ Undergraduate Engine Design Competition 27-Jul 0930 hrs 251 B ABPSI-6/HSABP-11 Additive Manfacturing (ADP) 4-ADP-1 Additive Manufacturing for Propulsion Systems 25-Jul 0930 hrs 255 E 124-ADP-2 Seal Material Advancements and Advanced Seal Technology 27-Jul 0930 hrs 255 E Advanced Engine Control (AEC) 5-AEC-1 Advanced Engine Control & Intelligent Systems I 25-Jul 0930 hrs 150 G 94-AEC-2 Advanced Engine Control & Intelligent Systems II 26-Jul 1500 hrs 150 DE Aircraft Electric Propulsion (AEP) 33-AEP-1 Aircraft Electric Propulsion I 25-Jul 1530 hrs 250 E 65-AEP-2 Aircraft Electric Propulsion II 26-Jul 0930 hrs 150 DE Advanced Propulsion Concepts (APC) 6-APC-1 Advanced In-Space Concepts 25-Jul 0930 hrs 251 C 95-APC-2 Advanced Propulsion Concepts I 26-Jul 1500 hrs 251 D 125-APC-3 Advanced Propulsion Concepts II 27-Jul 0930 hrs 251 C www.aiaa-propulsionenergy.org 30 #aiaaPropEnergy IntroSessions at a Glance

Abbreviation Title Date Start Time Location Advanced Power Systems (APS) 7-APS-1 Space Power Generation, Processing and Performance 25-Jul 0930 hrs 150 DE 34-APS-2 Space Transportation Development and Progress 25-Jul 1530 hrs 151 G 96-APS-3 Space Nuclear Power Generation 26-Jul 1500 hrs 151 G 126-APS-4 Space and Aircraft Power Generation, Processing and Performance 27-Jul 0930 hrs 151 G Energy Conversion Device Technology (ECD) 8-ECD-1 Magnetohydrodynamic, Brayton, and CO2 Cycle Systems 25-Jul 0930 hrs 151 DE 66-ECD-2 Thermoelectric, Fuel Cell, and Photovoltaic Conversion Systems 26-Jul 0930 hrs 151 G 151-ECD-3 Stirling Components and Systems 27-Jul 1500 hrs 151 AB Energetic Components and Systems (ECS) 35-ECS-1 Energetic Material, Detonation Transition and Ignition of Components 25-Jul 1530 hrs 251 C 67-ECS-2 Updates to Acceptance Methodologies for Energetic Components 26-Jul 0930 hrs 251 C 127-ECS-3 Energetic Systems and Component Developments 27-Jul 0930 hrs 254 C 152-ECS-4 Young Professionals and Energetic Components & Systems - An 27-Jul 1500 hrs 254 B Educational Series Panel Session Electricity Delivery, Grid and Energy Storage Technologies (EDES) 9-EDES-1 Waste Heat Recovery and Submerged Offshore Nuclear Power Stations: 25-Jul 0930 hrs 151 G Technology, Opportunities and Challenges 36-EDES-2 Energy Technologies for Aerospace and Terrestrial Applications 25-Jul 1530 hrs 151 DE Energy Optimized Aircraft and Equipment Systems (EOS) 135-GEPC-2/EOA-1 Low Carbon Aviation- Electric Propulsion and Technologies 27-Jul 0930 hrs 254 B Propulsion Education (EDU) 10-EDU-1 Propulsion Education I 25-Jul 0930 hrs 253 AB 68-EDU-2 Propulsion Education II 26-Jul 0930 hrs 251 B 128-EDU-3 Propulsion Education III 27-Jul 0930 hrs 253 AB Energy Efficiency (EE) 97-EE-1 Systems-Level Analysis of Energy Efficiency and Renewable Energy 26-Jul 1500 hrs 150 G 153-EE-2 Renewable Fuel Generation And Processing 27-Jul 1500 hrs 150 G Electric Propulsion (EP) 11-EP-1 Hall Thruster Physics & Modeling I 25-Jul 0930 hrs 250 A 12-EP-2 Lorentz Force Accelerators 25-Jul 0930 hrs 250 B 13-EP-3 EP Flight Programs & Missions 25-Jul 0930 hrs 250 C 14-EP-4 Ion Thruster Development 25-Jul 0930 hrs 250 D 15-EP-5 Electrospray I 25-Jul 0930 hrs 250 E 37-EP-6 Hall Thruster Physics & Modeling II 25-Jul 1530 hrs 250 A 38-EP-7 Hall Thruster Development 25-Jul 1530 hrs 250 B 39-EP-8 Hollow Cathode Physics & Modeling 25-Jul 1530 hrs 250 C 40-EP-9 NEXT Ion Thruster Development 25-Jul 1530 hrs 250 D 69-EP-10 Hall Thruster Physics & Modeling III 26-Jul 0930 hrs 250 A 70-EP-11 Hall Thruster Alternative Propellants 26-Jul 0930 hrs 250 B 71-EP-12 Hollow Cathode Development 26-Jul 0930 hrs 250 C

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Abbreviation Title Date Start Time Location Electric Propulsion (EP) (continued) 72-EP-13 Helicon Thruster 26-Jul 0930 hrs 250 D 73-EP-14 Electrospray II 26-Jul 0930 hrs 250 E 98-EP-15 HERMeS Hall Thruster I 26-Jul 1500 hrs 250 A 99-EP-16 Low Power Hall Thruster Development 26-Jul 1500 hrs 250 B 100-EP-17 LaB6 Hollow Cathodes 26-Jul 1500 hrs 250 C 101-EP-18 Sputtering & Erosion Physics 26-Jul 1500 hrs 250 D 102-EP-19 Pulsed Plasma Thruster 26-Jul 1500 hrs 250 E 129-EP-20 Plasma Plume Modeling 27-Jul 0930 hrs 250 A 130-EP-21 Mid Power Hall Thruster Development 27-Jul 0930 hrs 250 B 131-EP-22 Cathodes & Neutralizers 27-Jul 0930 hrs 250 C 132-EP-23 Advanced EP Concepts 27-Jul 0930 hrs 250 D 154-EP-24 HERMeS Hall Thruster II 27-Jul 1500 hrs 250 A 155-EP-25 High Power Hall Thruster & PPU Development 27-Jul 1500 hrs 250 B 156-EP-26 Magnetoplasmadynamics and EP Diagnostics 27-Jul 1500 hrs 250 C 157-EP-28 Micropropulsion 27-Jul 1500 hrs 250 E Forum 360 (F360) 16-F360-1 NRC Low-Carbon Aviation Report and Recommendations 25-Jul 0930 hrs Ballroom F 41-F360-2 Launch Vehicle Reusability: Holy Grail, Chasing Our Tail, or Somewhere 25-Jul 1530 hrs Ballroom F in Between 74-F360-3/LP-11 Liquid Propulsion History Session Lessons Learned 26-Jul 0930 hrs Ballroom F 103-F360-4 Nuclear Power for Distant Solar System Destinations 26-Jul 1500 hrs Ballroom F 133-F360-5 Seven Career Hacks for Professional Success 27-Jul 0930 hrs Ballroom F Fossil-Fuel Power (FFP) 42-FFP-1 Fossil-Fuel Power Technologies I 25-Jul 1530 hrs 150 DE 134-FFP-2 Fossil-Fuel Power Technologies II 27-Jul 0930 hrs 150 DE Green Energy (GEPC) 75-GEPC-1 Low Carbon Aviation-Propulsion Integration, Gas Turbines, and Fuels 26-Jul 0930 hrs 254 B 135-GEPC-2/EOA-1 Low Carbon Aviation- Electric Propulsion and Technologies 27-Jul 0930 hrs 254 B Gas Turbine Engines (GTE) 17-GTE-1 Turbines I 25-Jul 0930 hrs 250 F 18-GTE-2 Air-Breathing Combustors I 25-Jul 0930 hrs 251 A 43-GTE-4 Thermodynamic Topics of Gas Turbine Engines 25-Jul 1530 hrs 250 F 44-GTE-5 Compressors I 25-Jul 1530 hrs 251 A 45-GTE-6 Air-Breathing Combustors II 25-Jul 1530 hrs 251 B 76-GTE-7 Turbines II 26-Jul 0930 hrs 250 F 77-GTE-8 Compressors II 26-Jul 0930 hrs 251 A 46-GTE-9 Engine Control Systems 25-Jul 1530 hrs 254 B 104-GTE-10 Advanced Materials and Technology for Gas Turbine Engines 26-Jul 1500 hrs 251 A 105-GTE-11 Turbines III 26-Jul 1500 hrs 251 B 106-GTE-12 Gas Turbine Engine Testing Techniques 26-Jul 1500 hrs 251 C

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Abbreviation Title Date Start Time Location Gas Turbine Engines (GTE) (continued) 136-GTE-14 Compressors III 27-Jul 0930 hrs 251 A 137-GTE-15/ Undergraduate Engine Design Competition 27-Jul 0930 hrs 251 B ABPSI-6/HSABP-11 158-GTE-16 Turbines IV 27-Jul 1500 hrs 250 F 159-GTE-17 Aerodynamic Flows in Gas Turbine Engines 27-Jul 1500 hrs 251 A 160-GTE-18 Gas Turbine Inlets 27-Jul 1500 hrs 251 B 161-GTE-19 Gas Turbine Engine Modeling 27-Jul 1500 hrs 251 C Hybrid Rockets (HR) 19-HR-1 Combustion Dynamics and Mixing Efficiencies I 25-Jul 0930 hrs 255 B 47-HR-2 Design and Development of Novel Hybrid Rocket Motor Concepts I 25-Jul 1530 hrs 255 B 78-HR-3 Internal Ballistics Modeling I 26-Jul 0930 hrs 253 AB 79-HR-4 Combustion Dynamics and Mixing Efficiencies II 26-Jul 0930 hrs 255 B 107-HR-5 Development and Evaluation of Novel O/F Formulations and 26-Jul 1500 hrs 253 AB Combinations 108-HR-6 Combustion Stability, Motor Performance, and Related Issues 26-Jul 1500 hrs 255 B 138-HR-7 Design and Development of Novel Hybrid Rocket Motor Concepts II 27-Jul 0930 hrs 255 B 162-HR-8 Internal Ballistics Modeling II 27-Jul 1500 hrs 255 B High Speed Air Breathing Propulsion (HSABP) 20-HSABP-1 Special/Invited Panel on HSABP: Special Session: Persistence Issues In 25-Jul 0930 hrs 254 B CFD of Hypersonic Air-Breathing Propulsion 21-HSABP-2 Computational Analysis of Supersonic Combustion Flow Paths, 25-Jul 0930 hrs 255 A Components, and Processes 22-HSABP-3 Design and Optimization of High Speed Propulsion Flow Paths 25-Jul 0930 hrs 254 C 48-HSABP-4 Advances in Hypersonic Air-Breathing Propulsion Systems 25-Jul 1530 hrs 255 A 80-HSABP-5 Numerical Analysis of Supersonic Combustion Flow Paths, 26-Jul 0930 hrs 254 C Components, and Processes 81-HSABP-6 High Fidelity Simulations of High-Speed Air-Breathing Systems 26-Jul 0930 hrs 255 A 109-HSABP-7 Numerical Analysis of High-Speed Air-Breathing Propulsion and Their 26-Jul 1500 hrs 254 C Integration 110-HSABP-8 Pulse Detonation Physics, and/or Combined Cycle with Other Utility to 26-Jul 1500 hrs 255 A High-Speed Propulsion 139-HSABP-9 Experimental and Numerical Analysis of High Speed Propulsion 27-Jul 0930 hrs 255 A Systems 163-HSABP-10 Experimental Developments in High-Speed Air-Breathing Systems 27-Jul 1500 hrs 255 A 137-GTE-15/ Undergraduate Engine Design Competition 27-Jul 0930 hrs 251 B ABPSI-6/HSABP-11 ITAR 82-ITAR-1 Gas Turbines and Associated Equipment (CAT-XIX) 26-Jul 0930 hrs 151 DE 111-ITAR-2 Launch Vehicles I (CAT-IV) 26-Jul 1500 hrs 151 DE 140-ITAR-3 Explosives and Energetic Materials (CAT-V) 27-Jul 0930 hrs 151 DE 164-ITAR-4 Launch Vehicles II (CAT-IV) 27-Jul 1500 hrs 151 DE

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Abbreviation Title Date Start Time Location Liquid Propulsion (LP) 23-LP-1 Green Propellants I 25-Jul 0930 hrs 251 D 24-LP-2 Combustors I 25-Jul 0930 hrs 251 E 25-LP-3 Propellant Storage & Transfer I 25-Jul 0930 hrs 251 F 49-LP-4 Green Propellants II 25-Jul 1530 hrs 251 D 50-LP-5 Nozzles I 25-Jul 1530 hrs 251 E 51-LP-6 Propellant Storage & Transfer II 25-Jul 1530 hrs 251 F 52-LP-7 Propulsion Systems - Design & Test I 25-Jul 1530 hrs 253 AB 74-F360-3/LP-11 Liquid Propulsion History Session: Lessons Learned 26-Jul 0930 hrs Ballroom F 83-LP-8 Nozzles II 26-Jul 0930 hrs 251 D 84-LP-9 Propellant Storage & Transfer III 26-Jul 0930 hrs 251 E 141-LP-12 Rocket Engine Components 27-Jul 0930 hrs 251 D 142-LP-13 Propulsion Systems - Design & Test II 27-Jul 0930 hrs 251 E 143-LP-14 Turbomachinery 27-Jul 0930 hrs 251 F 165-LP-15 Injectors 27-Jul 1500 hrs 251 D 166-LP-16 Combustion Stability 27-Jul 1500 hrs 251 E 167-LP-17 Combustors II 27-Jul 1500 hrs 251 F 168-LP-18 Green Propellants III 27-Jul 1500 hrs 253 AB Nuclear and Future Flight (NFF) 53-NFF-1 Fusion and Alternative Nuclear Concepts I 25-Jul 1530 hrs 150 G 61-NFF-2 Open Forum: Nuclear Propulsion in the 21st Century 25-Jul 1930 hrs 150 G 85-NFF-3 Fusion and Alternative Nuclear Concepts II 26-Jul 0930 hrs 150 G 113-NFF-4 Nuclear Thermal Propulsion: Engines and Missions 26-Jul 1500 hrs 251 E 121-NFF-5 Future Flight Propulsion Systems I 26-Jul 1900 hrs 150 G 144-NFF-6 Future Flight Propulsion Systems II 27-Jul 0930 hrs 150 G Propellants and Combustion (PC) 26-PC-1 Combustion Dynamics I 25-Jul 0930 hrs 255 C 27-PC-2 Propellant Development - Solid Fuel 25-Jul 0930 hrs 255 D 54-PC-3 Ignition 25-Jul 1530 hrs 255 C 55-PC-4 Spray Combustion 25-Jul 1530 hrs 255 D 56-PC-5 Advanced Concepts 25-Jul 1530 hrs 255 E 86-PC-6 Combustion Chemistry 26-Jul 0930 hrs 255 C 87-PC-7 Air-Breathing Combustion Modeling 26-Jul 0930 hrs 255 D 88-PC-8 Cryogenic Sprays 26-Jul 0930 hrs 255 E 114-PC-9 Advanced Combustor Concepts 26-Jul 1500 hrs 255 C 115-PC-10 Combustion Instability 26-Jul 1500 hrs 255 D 116-PC-11 Combustion Diagnostics 26-Jul 1500 hrs 255 E 145-PC-12 Green Propulsion 27-Jul 0930 hrs 255 C 146-PC-13 Single Injector Test Case Modeling 27-Jul 0930 hrs 255 D 169-PC-14 Combustion Modeling 27-Jul 1500 hrs 255 C 170-PC-15 Rotating Detonation Concepts 27-Jul 1500 hrs 255 D 171-PC-16 Combustion Dynamics II 27-Jul 1500 hrs 255 E

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Abbreviation Title Date Start Time Location Plenary Sessions (PLNRY) 1-PLNRY-1 Innovate Or Die! (Note: Dying Is Easier) 25-Jul 0800 hrs Ballroom A-D 30-PLNRY-2 System Needs in Propulsion and Energy 25-Jul 1330 hrs Ballroom A-D 62-PLNRY-3 Game Changing Developments in Propulsion and Energy 26-Jul 0800 hrs Ballroom A-D 91-PLNRY-4 High Power Systems for Aerospace Applications 26-Jul 1300 hrs Ballroom A-D 120-PLNRY-5 Formula for Success and Longevity in the Aerospace Business 26-Jul 1800 hrs Ballroom A-D 122-PLNRY-6 The Impact of Additive Manufacturing on the Design Process 27-Jul 0800 hrs Ballroom A-D 149-PLNRY-7 The Strategic Challenges and Opportunities in the Power and 27-Jul 1330 hrs Ballroom A-D Propulsion Markets Propulsion and Power Systems (PP) 172-PP-1 Propulsion and Power Systems of Unmanned Systems 27-Jul 1500 hrs 150 DE Satellites (SATS) 117-SATS-1 Small Satellites I 26-Jul 1500 hrs 251 F 173-SATS-2 Small Satellites II 27-Jul 1500 hrs 254 C Solid Rockets (SR) 28-SR-1 Solid Rocket Grain Design and Ballistics 25-Jul 0930 hrs 254 A 57-SR-2 Solid Rocket Modeling and Simulation 25-Jul 1530 hrs 254 A 89-SR-3 Solid Rocket Combustion Instability 26-Jul 0930 hrs 254 A 118-SR-4 Advanced Solid Rockets (Nozzles, Cases, and Controllable) 26-Jul 1500 hrs 254 A 147-SR-5 Solid Rocket Developments Past and Present 27-Jul 0930 hrs 254 A 174-SR-6 Solid Propellant Developments 27-Jul 1500 hrs 254 A Thermal Management (TM ) 29-TM-1 Thermal System Applications and Unique Environments I 25-Jul 0930 hrs 151 AB 58-TM-2 Thermal System Applications and Unique Environments II 25-Jul 1530 hrs 151 AB 90-TM-3 Thermal System Applications and Unique Environments III 26-Jul 0930 hrs 151 AB 119-TM-4 Heat Transfer and Transport Modeling and Analysis I 26-Jul 1500 hrs 151 AB 148-TM-5 Heat Transfer and Transport Modeling and Analysis II 27-Jul 0930 hrs 151 AB 175-TM-6 Nano-Technology for Thermal Management (Panel) 27-Jul 1500 hrs 151 G 176-TM-7 Heat Transfer and Transport Modeling and Analysis III 27-Jul 1500 hrs 151 G Vehicle Systems (VS) 59-VS-1 Advanced Vehicle Systems Concepts 25-Jul 1530 hrs 254 C

www.aiaa-propulsionenergy.org 35 #aiaaPropEnergy Monday Monday, 25 July 2016 1-PLNRY-1 INNOVATE OR DIE! (Note: Dying is easier) Ballroom A-D 0800 - 0900 hrs Bran Ferren Co-Founder & Chief Creative Officer Applied Minds, LLC Monday, 25 July 2016 2-NW-1 Networking Coffee Break Exhibit Hall C 0845 - 0930 hrs Monday, 25 July 2016 3-ABPSI-1 Nozzles and Exhaust 255 F Chaired by: C. CHUCK, Boeing Commercial Airplanes and D. SANDERS, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4500 AIAA-2016-4501 AIAA-2016-4502 AIAA-2016-4503 AIAA-2016-4504

Reducing residue in aluminized fuel-rich Prediction of NOx Emissions Using a Hot Streak Characterization in Serpentine Propulsion AerodynamicWorkshop II, Open and Closed-Loop Responses of a propellant for Ramjets. Stirred Reactor Modelling Approach for an Exhaust Nozzles Summary of Participant Results for a Dual Dual-Throat Nozzle during Fluidic Thrust N. Rathi, P. Ramakrishna, Indian Institute of Aero-Engine with RQL Combustor D. Crowe, Air Force Institute of Technology, Wright- Separate Flow Reference Nozzle, Including Vectoring Technology Madras, Chennai, India A. Prakash, Teesside University, Middlesbrough, Patterson AFB, OH; C. Martin, Air Force Research Some Experimental Results M. Ferlauto, R. Marsilio, Technical University of United Kingdom Laboratory, Eglin AFB, FL R. Thornock, Self, Seattle, WA Turin, Turin, Italy Monday, 25 July 2016 4-ADP-1 Additive Manufacturing for Propulsion Systems 255 E 36 Chaired by: E. JENS, Stanford Univ and C. GATTO, Jet Propulsion Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4505 AIAA-2016-4506 AIAA-2016-4507 AIAA-2016-4508 AIAA-2016-4509 Thin film deposition using rarefied gas jet Use of Additive Manufacturing to Develop Additive Manufacturing of Small Scale Design of an Additive Manufactured Additively Manufactured Low NOx S. Pradhan, Indian Institute of Science, Bengaluru, India Advanced Hybrid Rocket Designs Rocket Grain Cartridges with Uniformly Compressor Vane with Multi-Hole Pressure Multipoint Lean Direct Injection Fuel J. Catina, B. Nellis, D. Grigsby, K. Castonguay, U.S. Distributed Aluminum Particles Probes for the Application in a Twin-Spool Atomizer Concepts Naval Academy, Annapolis, MD T. Elliott, B. Jenkins, R. Zeineldin, J. Johnson, Turbofan Engine G. Zink, S. Pack, J. Ryon, J. Short, United M. Simons, J. Godfey, University of Tennessee, F. Kern, University of the German Federal Armed Technologies Corporation, West Des Moines, IA Chattanooga, Chattanooga, TN; et al. Forces, Neubiberg, Germany; S. Bindl, Electro- Optical Systems, Krailling, Germany; M. Strasser, R. Niehuis, University of the German Federal Armed Forces, Neubiberg, Germany Monday, 25 July 2016 5-AEC-1 Advanced Engine Control & Intelligent Systems I 150 G Chaired by: A. BEHBAHANI, AFRL/RQT and R. MILLAR, Naval Postgraduate School 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4510 AIAA-2016-4511 AIAA-2016-4512 G2 ISHM Autonomous Control System for Heat Transfer Analysis for Servo Valve in Technical Opportunities for High Cryogenics Operation Hydraulic Servo Actuator of Aero Engine Temperature Smart P3 Sensors and J. Toro Medina, NASA Kennedy Space Center, Cape Vectoring Nozzle Electronics for Distributed Engine Control Canaveral, FL Y. Ding, Y. Liu, Y. Luo, L. Du, Beihang University, O. Watts, Watts International, LLC, Indianapolis, Beijing, China IN; L. Frediani, M. Usrey, Sporian Microsystems, Inc., Lafayette, CO Monday, 25 July 2016 6-APC-1 Advanced In-Space Concepts 251 C Chaired by: A. REISZ, Reisz Engineers and J. ROBINSON, Retired f/Boeing 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4513 AIAA-2016-4514 AIAA-2016-4515 AIAA-2016-4516 Roadmap for Long Term Sustainable Performance of a High Power Hall Proposed Lunar Mission to Commemorate Space Tug Propellant Options Space Exploration and Habitation Thruster for a Manned Mission to Mars Apollo 11 Moon Landing J. Robinson, Propellant Supply Technology, Seal Alternate Basing Concepts M. Gonzalez, San Jose State University, San D. Thorpe, Space Propulsion Synergy Team, Seal Beach, CA J. Robinson, Propellant Supply Technology, Seal Jose, CA Beach, CA; E. Henderson, NASA Johnson Space Beach, CA; R. Rhodes, Self, Cape Canaveral, FL; E. Center, Houston, TX Henderson, Self, Houston, TX Monday, 25 July 2016 7-APS-1 Space Power Generation, Processing and Performance 150 DE Chaired by: M. PATEL, US Merchant Marine Academy and A. BAISDEN, Johns Hopkins University Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4517 AIAA-2016-4518 AIAA-2016-4519 AIAA-2016-4520 AIAA-2016-4521 The Van Allan Probes Power System Stability Analysis of Spacecraft Power Status of the Development of Flight Power Solar Array Design For The Mars InSight Planetary Object Geophysical Observer Mission Performance Systems and Power Processing Units Processing Units for the NASA’s Evolutionary Lander Mission (POGO) and Its Unique Power System M. Butler, Johns Hopkins University Applied Physics J. Lee, The Aerospace Corporation, El Segundo, CA Xenon Thruster - Commercial (NEXT-C) Project G. Lam, S. Billets, T. Norick, R. Warwick, Lockheed E. Adams, E. Hohlfeld, J. Neville, C. Vigil Lopez, B. Laboratory, Laurel, MD M. Aulisio, NASA Glenn Research Center, Cleveland, Martin Corporation, Sunnyvale, CA Wilhelm, Johns Hopkins University Applied Physics OH; J. Bontempo, ZIN Technologies, Inc., Cleveland, Laboratory, Laurel, MD OH; L. Pinero, NASA Glenn Research Center, Cleveland, OH; A. Birchenough, Vantage Partners, LLC, Cleveland, OH; T. Hertel, Aerojet Rocketdyne, Canoga Park, CA; B. White, NASA Glenn Research Center, Cleveland, OH; et al. 37 Monday, 25 July 2016 8-ECD-1 Magnetohydrodynamic, Brayton, and CO2 Cycle Systems 151 DE Chaired by: M. PISZCZOR, NASA Glenn Research Center and S. GENG, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4522 AIAA-2016-4523 AIAA-2016-4524 AIAA-2016-4525 AIAA-2016-4526 Fundamental Studies of Radio-Frequency Numerical Simulation of Frozen Inert Gas Numerical Analysis of Non-equilibrium Sensitivity Study of a VHTR Powered Two Types of Analytical Methods for a Preionization for Frozen Inert Gas Plasma Plasma MHD Generator with Collisional- Disk MHD Generator with Swirl Vanes Brayton Cycle as a Topping Unit for a Centrifugal Compressor Impeller for D. Ichinokiyama, F. Takayasu, University of Magnetohydrodynamic Electrical Power Radiative Model Steam Cycle Supercritical CO 2 Power Cycles Generation R. Takahashi, F. Takayasu, University of Tsukuba, Tsukuba, Tsukuba, Japan W. Freitas, D. Wilson, University of Texas, L. Blanchette, A. Khadse, M. Mohagheghi, J. M. Tanaka, Y. Hitotsubashi, Y. Okuno, Tokyo Tsukuba, Japan; Y. Okuno, Tokyo Institute of Arlington, Arlington, TX Kapat, University of Central Florida, Orlando, FL Institute of Technology, Yokohama, Japan Technology, Yokohama, Japan Monday, 25 July 2016 9-EDES-1 Waste Heat Recovery and Submerged Offshore Nuclear Power Stations: Technology, Opportunities and Challenges 151 G 0930 - 1200 hrs This is a discussion panel where the panel members will talk about technologies for waste heat recovery and modular submerged offshore nuclear power stations for power generation and energy conversion, and with emphasis on challenges and opportunities. Each panel member will also make a short presentation to highlight his/her scope of involvement in and view of the future demands for these technologies.

Panelists: Stephen Heister Terry J. Hendricks Ji-Cheng (JC) Zhao J. Stephen Herring Raisbeck Engineering Distinguished Professor for Engineering and Technical Group Supervisor, Thermal Energy Conversion Program Director, Advanced Research Projects Agency - Energy Director Technology Integration Applications & Systems, MMRTG Pyroshock Project Manager/JPL (ARPA-E) Center for Space Nuclear Research Director, Maurice J. Zucrow Laboratories MATRIX Technical Manager U.S. Department of Energy Purdue University NASA Jet Propulsion Laboratory, California Institute of Technology Monday, 25 July 2016 10-EDU-1 Propulsion Education I 253 AB Chaired by: E. FLEEMAN and M. HITT, The University of Alabama in Huntsville 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4527 AIAA-2016-4528 AIAA-2016-4529 AIAA-2016-4530 AIAA-2016-4531 Practical Techniques for Modeling Gas Teaching Risk Analysis for Use in an Aircraft The Gas Dynamic Brayton Cycle Power Overview of Vortex Injected Hybrid Rocket Development of a Vortex Hybrid Upper Turbine Engine Performance Gas Turbine Engine Capstone Design Course Conversion Test Bed as an Educational Engines-Regression Rate Modeling Stage Engine J. Chapman, T. Lavelle, J. Litt, NASA Glenn A. Byerley, C. Cooper, D. O’Dowd, U.S. Air Force Device for Workforce Development B. Roy, R. Frederick, University of Alabama, A. Parlett, University of Alabama, Huntsville, Research Center, Cleveland, OH Academy, Colorado Springs, CO J. Herdy, Government Energy Solutions, Huntsville, AL Huntsville, Huntsville, AL Huntsville, AL Monday, 25 July 2016 11-EP-1 Hall Thruster Physics & Modeling I 250 A Chaired by: H. KAMHAWI, NASA Glenn Research Center and M. PATINO, University of California, Los Angeles 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4532 AIAA-2016-4533 AIAA-2016-4534 AIAA-2016-4535 Measurements and theory of driven PRINCE: A Software Tool for Characterizing Growth and Saturation of Ion Acoustic Hall Thruster Thermal Modeling and Test breathing oscillations in a Hall effect Waves and Instabilities in Plasma Thrusters Waves in Hall Thrusters Data Correlation thruster S. Rojas Mata, E. Choueiri, Princeton University, I. Katz, A. Lopez Ortega, B. Jorns, I. Mikellides, J. Myers, Vantage Partners, LLC, Cleveland, OH; K. Hara, S. Keller, Y. Raitses, Princeton Plasma Princeton, NJ; B. Jorns, Jet Propulsion Laboratory, Jet Propulsion Laboratory, California Institute of H. Kamhawi, J. Yim, L. Clayman, NASA Glenn Physics Laboratory, Princeton, NJ California Institute of Technology, Pasadena, CA; R. Technology, Pasadena, CA Research Center, Cleveland, OH Spektor, The Aerospace Corporation, El Segundo, CA Monday, 25 July 2016 12-EP-2 Lorentz Force Accelerators 250 B Chaired by: M. KEIDAR, The George Washington University and N. YANES 0930 hrs 1000 hrs 1030 hrs

38 AIAA-2016-4536 AIAA-2016-4537 AIAA-2016-4538 Liquid Metal Mass Flow Measurement Measurement of the Applied-Field Parametric Optimization of the Fusion Using a JxB Pump for a Lithium Lorentz Component of the Thrust of a Lithium Driven Rocket Liner Compression Driver Force Accelerator Lorentz Force Accelerator A. Shimazu, University of Washingtion, Seattle, M. Hepler, W. Coogan, B. Ilardi, E. Choueiri, W. Coogan, M. Hepler, E. Choueiri, Princeton WA; A. Pancotti, B. Cornella, J. Slough, MSNW, Princeton University, Princeton, NJ University, Princeton, NJ LLC, Redmond, WA Monday, 25 July 2016 13-EP-3 EP Flight Programs & Missions 250 C Chaired by: T. SWANSON, AEDC and B. JORNS 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4539 AIAA-2016-4540 AIAA-2016-4541 AIAA-2016-4542 AIAA-2016-4543 In-Flight Operation of the Dawn Ion The Iodine Satellite (iSat) Project Psyche: Journey to a Metal World Adaptability of the SSL SPT-140 Performance and Plume Characterization Propulsion System Through Operations in Development through Critical Design D. Oh, D. Goebel, Jet Propulsion Laboratory, Subsystem for use on a NASA Discovery of the PPS 1350-G Hall Thruster the LAMO Orbit at Ceres Review (CDR) California Institute of Technology, Pasadena, CA; Class Missions: Psyche K. Diamant, The Aerospace Corporation, El C. Garner, M. Rayman, Jet Propulsion Laboratory, J. Dankanich, NASA Marshall Space Flight Center, L. Elkins-Tanton, Arizona State University, Tempe, J. Delgado, P. Lord, L. Rotlisberger, Space Segundo, CA; T. Lee, R. Liang, J. Noland, Space California Institute of Technology, Pasadena, CA Huntsville, AL; H. Kamhawi, NASA Glenn Research AZ; C. Polanskey, Jet Propulsion Laboratory, Systems/Loral, LLC, Palo Alto, CA Systems/Loral, LLC, Palo Alto, CA; V. Vial, N. Center, Cleveland, OH; M. Selby, NASA Marshall California Institute of Technology, Pasadena, CA; Cornu, Safran Group, Vernon, France Space Flight Center, Huntsville, AL; L. Byrne, Busek P. Lord, S. Tilley, Space Systems/Loral, LLC, Palo Company, Inc., Natick, MA Alto, CA; et al. Monday, 25 July 2016 14-EP-4 Ion Thruster Development 250 D Chaired by: R. WIRZ, UCLA and J. FOSTER, University of Michigan 0930 hrs 1000 hrs AIAA-2016-4544 AIAA-2016-4545 Maturation of Iodine Fueled BIT-3 RF Ion Discharge EEDF for a Miniature DC Ring- Thruster and RF Neutralizer Cusp Ion Thruster M. Tsay, J. Frongillo, J. Zwahlen, Busek Company, B. Dankongkakul, R. Wirz, University of California, Inc., Natick, MA Los Angeles, Los Angeles, CA Monday, 25 July 2016 15-EP-5 Electrospray I 250 E Chaired by: B. PRINCE, Air Force Research Laboratory and S. BERG, Missouri University of Science and Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4547 AIAA-2016-4548 AIAA-2016-4549 AIAA-2016-4550 AIAA-2016-4551 Silicon Emitter Needle and Array Design Simulation and Imaging of Ferrofluid Measuring the Effects of Magnetic Surface Species Measurements in the Beam Measurement of the Fragmentation for Indium Electrospray Arrays for Meniscus Deformation and Spray Onset Stress During Electrospray of an Ionic of an Ionic Liquid Ferrofluid Capillary Rates of Solvated Ions in Ion Electrospray Spacecraft Propulsion under Electric and Magnetic Stresse Liquid Ferrofluid Electrospray Source Thrusters C. Marrese-Reading, J. Anderson, Jet Propulsion B. Jackson, L. King, Michigan Technological K. Terhune, L. King, Michigan Technological K. Terhune, L. King, Michigan Technological C. Miller, P. Lozano, Massachusetts Institute of Laboratory, California Institute of Technology, University, Houghton, MI University, Houghton, MI University, Houghton, MI; B. Prince, Air Force Technology, Cambridge, MA Pasadena, CA Research Laboratory, Kirtland AFB, NM; B. Hawkett, University of Sydney, Sydney, Australia Monday, 25 July 2016 16-F360-1 NRC Low-Carbon Aviation Report and Recommendations Ballroom F 0930 - 1200 hrs Moderator: Marty Bradley, Technical Fellow, Boeing Commercial Airplanes 39 Panelists: Alan Angleman Karen Thole Alan Epstein Mike Benzakein Steve Csonka Senior Program Officer Department Head and Professor, Mechanical and Vice President, Technology and Environment Wright Brothers Institute Professor Executive Director National Research Council Nuclear Engineering Pratt & Whitney Assistant Vice President for Aerospace and Aviation, Commercial Aviation Alternative Fuels Initiative Pennsylvania State University Office of Research The Ohio State University

Monday, 25 July 2016 17-GTE-1 Turbines I 250 F Chaired by: G. PANIAGUA, Purdue University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4552 AIAA-2016-4553 AIAA-2016-4554 AIAA-2016-4555 AIAA-2016-4556 Influence of Laminar-Turbulent Transition Secondary Flows and Losses in a Highly Secondary Loss Production Mechanisms in Probabilistic CFD-Analysis of Integration of a Turbine Stage Optimizer on 3D Flow Pattern in Subsonic Turbine Loaded Low Aspect Ratio Transonic Axial a Low Pressure Turbine Cascade Regeneration-Induced Geometry into Engine Simulation Utilizing Numerical Cascade Flow Turbine Stage P. Bear, M. Wolff, Wright State University, Dayton, Variances in a Low-Pressure Turbine Propulsion System Simulation S. Yershov, V. Yakovlev, National Academy of A. Kaliyaperumal, M. Govardhan, Indian Institute OH; A. Gross, New Mexico State University, Las B. Ernst, J. Seume, F. Herbst, Leibniz University, C. Thorn, R. Hartfield, Auburn University, Auburn, AL Sciences of Ukraine, Kharkiv, Ukraine of Technology Madras, Chennai, India Cruces, NM; C. Marks, R. Sondergaard, Air Force Hannover, Germany Research Laboratory, Wright-Patterson AFB, OH Monday, 25 July 2016 18-GTE-2 Air-Breathing Combustors I 251 A Chaired by: M. NALIM, Indiana University Purdue University Indianapolis 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4557 AIAA-2016-4558 AIAA-2016-4559 AIAA-2016-4560 AIAA-2016-4561 Assessment of the Boundary Layer within Computational Analysis of Flame Numerical Evaluation of an Ejector-Enhanced Optical Diagnostics in a High-g A CFD Investigation of Multiple Burner a Rotating Detonation Combustor Stabilization Using Strong Swirl for Resonant Pulse Combustor with a Poppet Inlet Combustion Cavity Ignition and Flame Propagation with J. Braun, J. Sousa, G. Paniagua, Purdue University, Afterburner Applications Valve and a Converging Exhaust Nozzle A. Cottle, N. Gilbert, M. Polanka, Air Force Institute Detailed Chemistry and Automatic West Lafayette, IN K. Parammasivam, D. D, S. Gunasekar, A. Basidh, S. Yungster, Ohio Aerospace Institute, Cleveland, OH; of Technology, Wright-Patterson AFB, OH; L. Goss, Meshing Anna University, Chennai, India D. Paxson, H. Perkins, NASA Glenn Research Center, C. Goss, Innovative Scientific Solutions, Inc., G. Kumar, S. Drennan, Convergent Science, Inc., Cleveland, OH Dayton, OH Madison, WI Monday, 25 July 2016 19-HR-1 Combustion Dynamics and Mixing Efficiencies I 255 B Chaired by: S. CLAFLIN, Aerojet Rocketdyne and D. PASTRONE, Politecnico di Torino 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4562 AIAA-2016-4563 AIAA-2016-4564 AIAA-2016-4565 Vortex Combustion in a Lab-Scale Hybrid Thermal Cycling for Development of Hybrid Flame Emission Spectroscopy in a Bipolar Combustion Response Model for Rocket Motor Fuel for a Notional Mars Ascent Vehicle Paraffin-Based Hybrid Rocket Hybrid Rocket Internal Ballistic Simulation C. Paravan, J. Glowacki, S. Carlotti, F. Maggi, L. E. Farias, M. Redmond, A. Karp, R. Shotwell, Jet K. Stober, P. Narsai, K. Venkataraman, A. Thomas, D. Greatrix, Ryerson University, Toronto, Canada Galfetti, Technical University of Milan, Milan, Italy Propulsion Laboratory, California Institute of Technology, B. Cantwell, Stanford University, Stanford, CA Pasadena, CA; F. Mechentel, Stanford University, Palo Alto, CA; G. Story, NASA Marshall Space Flight Center, Huntsville, AL Monday, 25 July 2016 20-HSABP-1 Special/Invited Panel on HSABP: Special Session: Persistence Issues In CFD of Hypersonic Air-Breathing Propulsion 254 B 40 Chaired by: F. MALO-MOLINA, Raytheon Missile Systems and S. BECKEL 0930 hrs 1100 hrs 1130 hrs Panel Discussion AIAA-2016-4566 AIAA-2016-4567 Reacting Hybrid Reynolds-Averaged Scaling for Flamelet Calculation of Navier-Stokes/Large-Eddy Simulation of a Turbulent Supersonic Combustion Supersonic Cavity Flameholder F. Ladeinde, Z. Lou, Stony Brook University, Stony E. Hassan, D. Peterson, M. Hagenmaier, Air Force Brook, NY Research Laboratory, Wright-Patterson AFB, OH Monday, 25 July 2016 21-HSABP-2 Computational Analysis of Supersonic Combustion Flow Paths, Components, and Processes 255 A Chaired by: C. BRUNO, United Technologies Research Center and R. MOEHLENKAMP, Aerojet Rocketdyne 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4568 AIAA-2016-4569 AIAA-2016-4570 AIAA-2016-4571 Performance comparisons, RAM and A Quasi-One-Dimensional Analysis of Quasi-One-Dimensional Analysis of A computational and experimental study

SCRAM Hydrogen-Fueled Scramjet Combustors Supersonic Combustor Performance of injection structure effect on H2-air J. Tegner, Swedish Defense Research Agency R. Seleznev, S. Surzhikov, Russian Academy of Y. Zhao, Q. Shen, F. Guan, China Academy of rotating detonation engine (FOI), Stockholm, Sweden Sciences, Moscow, Russia Aerospace Aerodynamics, Beijing, China C. Yang, H. Ma, X. Wu, X. Xu, Nanjing University of Science and Technology, Nanjing, China Monday, 25 July 2016 22-HSABP-3 Design and Optimization of High Speed Propulsion Flow Paths 254 C Chaired by: R. HARTFIELD, Auburn University and D. PAXSON, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4572 AIAA-2016-4573 AIAA-2016-4574 AIAA-2016-4575 Investigation of a variable geometry 2D Analysis of Mode Transition Performance Analyzing the flow pattern of inward turning Research on a Novel Internal waverider inlet for combined cycle engine. for a Tandem TBCC Engine inlet combined with variable-geometry TBCC Inlet for Ramjet Mode X. Liu, L. Shi, P. Liu, G. He, Northwestern M. Zhang, Z. Wang, Z. Liu, X. Zhang, Z. Fengyuan, G. Huang, H. Huihui, C. Xia, Nanjing H. Huihui, G. Huang, Z. Fengyuan, C. Xia, Nanjing Polytechnical University, Xi’an, China Northwestern Polytechnical University, Xi’an, China University of Aeronautics and Astronautics, Nanjing, University of Aeronautics and Astronautics, China Nanjing, China Monday, 25 July 2016 23-LP-1 Green Propellants I 251 D Chaired by: M. DEANS, NASA Glenn Research Ctr and J. MOORE 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4576 AIAA-2016-4577 AIAA-2016-4578 AIAA-2016-4579 Green Propellant Loading Demonstration AF-M315E Propulsion System Advances Decomposition of a Double Salt Ionic Liquid Linear Burn Rates of Monopropellants for at U.S. Range and Improvements Monopropellant on Heated Metallic Surfaces Multi-Mode Micropropulsion H. Mulkey, J. Miller, C. Bacha, NASA Goddard R. Masse, M. Allen, R. Spores, E. Driscoll, Aerojet S. Berg, J. Rovey, Missouri University of Science and A. Mundahl, S. Berg, J. Rovey, Missouri University Space Flight Center, Greenbelt, MD Rocketdyne, Redmond, WA Technology, Rolla, MO of Science and Technology, Rolla, MO Monday, 25 July 2016 24-LP-2 Combustors I 251 E Chaired by: D. LINEBERRY, UAH Propusion Research Center and M. MASQUELET, GE Global Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4580 AIAA-2016-4581 AIAA-2016-4582 AIAA-2016-4583

41 Exact Euler Solution of the Beltramian Effect of Injector Variation on the Experimental Investigation of Continuous Validation of Damage Parameter Based and Trkalian Bidirectional Vortex in a Bidirectional Vortex Detonation Rocket Engines for In-Space Finite Element Fatigue Life Analysis Cylindrical Annulus B. Maicke, G. Talamantes, Pennsylvania State Propulsion Results to Combustion Chamber Type TMF T. Barber, J. Majdalani, Auburn University, Auburn, AL University, Middletown, PA R. Smith, GHKN Engineering, LLC, Redmond, WA; Panel Test Results S. Stanley, Aerojet Rocketdyne,, Redmond, WA G. Thiede, J. Riccius, German Aerospace Center (DLR), Lampoldshausen, Germany; S. Reese, RWTH Aachen University, Aachen, Germany Monday, 25 July 2016 25-LP-3 Propellant Storage & Transfer I 251 F Chaired by: J. MOLINSKY, Orbital ATK and M. MEYER, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4584 AIAA-2016-4585 AIAA-2016-4586 AIAA-2016-4587 AIAA-2016-4588 Experimental, Numerical and Analytical New CFD Method for Simulation of Slosh Coupling sloshing, GNC and rigid body Validation of High-Resolution CFD Method Numerical calculation and reduced gravity Study of Cyrogenic Slosh Dynamics in a & Microgravity Fluid Dynamics motions during ballistic flight phases for Slosh Damping Extraction of Baffled experiment for dynamic wetting behavior Spherical Tank R. Manning, I. Ballinger, M. Dowdy, Keystone P. Behruzi, F. De Rose, F. Cirillo, M. Konopka, Tanks in liquid container J. Storey, J. Poothokaran, D. Kirk, H. Gutierrez, Engineering Company, Long Beach, CA Airbus, Bremen, Germany H. Yang, CFD Research Corporation, Huntsville, R. Imai, Muroran Institute of Technology, Muroran, Florida Institute of Technology, Melbourne, FL; M. AL; J. West, NASA Marshall Spaceflight Center, Japan de Natris, Avans University of Applied Sciences, Huntsville, AL Hertogenbosch, The Netherlands; B. Marsell, NASA Kennedy Space Center, Cape Canaveral, FL; et al. Monday, 25 July 2016 26-PC-1 Combustion Dynamics I 255 C Chaired by: W. ANDERSON, Purdue University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4589 AIAA-2016-4590 AIAA-2016-4591 AIAA-2016-4592 Experimental Combustion Dynamics Computation of Combustion Noise from a Assessing Computational Fluid Dynamics A structural variation of the methane-air Behavior Of A Multi-Element Lean Direct Premixed and Pressurized Propane Flame Turbulence Models for Rocket Exhaust premixed flame affected by an ultrasonic Injection (LDI) Gas Turbine Combustor Using Statistical Noise Modeling Plume Simulation standing wave W. Acosta, Army Research Laboratory, Cleveland, W. Ullrich, C. Hirsch, T. Sattelmayer, Technical D. Watts, QinetiQ, Sevenoaks, United Kingdom J. Kim, M. Kim, S. Bae, D. Bae, Pukyong National OH; C. Chang, NASA Glenn Research Center, University of Munich, Garching, Germany University, Busan, South Korea; H. Seo, Hanwha Cleveland, OH Corporation, Daejeon, South Korea Monday, 25 July 2016 27-PC-2 Propellant Development - Solid Fuel 255 D Chaired by: T. NGUYEN, Aerojet Rocketdyne and C. PARAVAN, Politecnico di Milano 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4593 AIAA-2016-4594 AIAA-2016-4595 AIAA-2016-4596 AIAA-2016-4597 Measurements of Dielectric Properties of Modern Scanning Electron Microscopy in the Pyrotechnic Dispersion and Ignition of Novel Activated Metal Powders for Improved Numerical Method to Estimate Thermal Condensed Phase Aluminized Composite Study of Solid Propellant Combustion: Surface Boron Particles in Gels Hybrid Fuels and Green Solid Propellants Conductivity of a Model Composite Propellants structure and Elemental Identification Via EDS Y. Solomon, Israel Military Industries, Ramat S. Dossi, C. Paravan, F. Maggi, M. Di Lorenzo, J. Propellant S. Barkley, K. Zhu, M. Ballestero, J. Michael, T. G. Morrow, A. Demko, E. Petersen, Texas A&M Hasharon, Israel; D. Grinstein, B. Natan, Technion-- Ardalic, L. Galfetti, Technical University of Milan, G. Rajoriya, C. Vijay, P. Ramakrishna, Indian Sippel, Iowa State University, Ames, IA University, College Station, TX Israel Institute of Technology, Haifa, Israel Milan, Italy Institute of Technology Madras, Chennai, India Monday, 25 July 2016 28-SR-1 Solid Rocket Grain Design and Ballistics 254 A Chaired by: M. BERDOYES, Herakles and S. MCHENRY, OrbitalATK

42 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4598 AIAA-2016-4599 AIAA-2016-4600 3D Flame Spread and Starting Transient in Burning Rate and Temperature Application of the Universal Expression Dual-thrust Solid Propellant Rocket Motors Measurements of HTPB/AP/Al Propellants for Erosive Burning to Nozzleless Solid S. Ajith, . Nichith , S. Vignesh, Kumaraguru College at Standard Rocket Motor Tests Propellant Rocket Motors of Technology, Coimbatore, India; S. Mani, Georgia R. de Araujo, P. Lacava, Technological Institute of A. Ozer, TUBITAK, Ankara, Turkey; Y. Özyörük, Institute of Technology, Atlanta, GA; T. Ramesh kumar, Aeronautics (ITA), São José dos Campos, Brazil; L. Middle East Technical University, Ankara, Turkey Auburn University, Auburn, AL; V. Sanal Kumar, de Almeida, F. Cunha, AVIBRAS aeroespacial, São Kumaraguru College of Technology, Coimbatore, India José dos Campos, Brazil

Monday, 25 July 2016 29-TM-1 Thermal System Applications and Unique Environments I 151 AB Chaired by: M. CHOI, NASA-Goddard Space Flight Center and C. TARAU, Advanced Cooling Technologies 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4601 AIAA-2016-4602 AIAA-2016-4603 AIAA-2016-4604 AIAA-2016-4605 Using Paraffin PCM to Make Optical Novel Multiphase Change Materials for Alkali Metal Heat Pipes for Kilopower Computational Investigation of Heat Pipe Embedded Thermoelectric Communication Type of Payloads Energy Storage Application in Buildings C. Tarau, W. Anderson, D. Beard, Advanced Cooling Impingement Cooling for Regeneratively Generator for Diesel Generator Set Waste Thermally Self-Sufficient for Operation in J. Darkwa, W. Su, University of Nottingham, Technologies, Inc., Lancaster, PA Cooled Rocket Nozzles Heat Recovery Orion Crew Module Nottingham, United Kingdom B. De Angelo, M. Ricklick, Embry-Riddle J. Schmidt, M. Ababneh, Advanced Cooling M. Choi, NASA Goddard Space Flight Center, Aeronautical University, Daytona Beach, FL Technologies, Inc., Lancaster, PA Greenbelt, MD Monday, 25 July 2016 30-PLNRY-2 System Needs in Propulsion and Energy Ballroom A-D 1330 - 1500 hrs Moderator: Dan Dumbacher, Professor Engineering Practice, School of Aeronautics and Astronautics, Purdue University Panelists: Doug Blake Dennis Andrucyk Director, Aerospace Systems Directorate Deputy Associate Administrator, Space Technology Mission Directorate Air Force Research Laboratory NASA

Monday, 25 July 2016 31-NW-2 Networking Coffee Break Exhibit Hall C 1500 - 1530 hrs Monday, 25 July 2016 32-ABPSI-2 High-Speed Inlets 255 F Chaired by: M. HASSAN, Georgia Institute of Technology 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4606 AIAA-2016-4607 AIAA-2016-4608 AIAA-2016-4609 Optimizing Probe Placement to Determine Design of Wave Derived Inlet for High Effects of Ridge Configuration on the Vortex Generators in a Two-Dimensional, Inlet Distortion Curvature Fuselage Performance of Integrated inlets External-Compression Supersonic Inlet S. Walter, J. Nabity, R. Starkey, University of E. Saheby, G. Huang, Nanjing University of G. Huang, E. Saheby, Nanjing University of E. Baydar, F. Lu, University of Texas, Arlington, Colorado, Boulder, Boulder, CO Aeronautics and Astronautics, Nanjing, China; A. Aeronautics and Astronautics, Nanjing, China; M. Arlington, TX; J. Slater, NASA Glenn Research Hays, California State University, Long Beach, CA Akhlaghi, University of Québec, Montréal, Canada; Center, Cleveland, OH Z. Yu, Nanjing University of Aeronautics and Astronautics, Nanjing, China

43 Monday, 25 July 2016 33-AEP-1 Aircraft Electric Propulsion I 250 E Chaired by: L. GEA, Boeing Engineering Operations & Technology and C. CHUCK, Boeing Commercial Airplanes 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4610 AIAA-2016-4611 AIAA-2016-4612 AIAA-2016-4613 Parallel Hybrid Gas-Electric Geared NASA Turbo-electric Distributed Propulsion Hybrid Regional Aircraft: A Comparative Airbus Group Electrical Aircraft Program, Turbofan Engine Conceptual Design and Bench Review of New Potentials Enabled by Electric The E-Fan Project Benefits Analysis K. Papathakis, K. Kloesel, Y. Lin, S. Clarke, J. Power L. Juvé, J. Fosse, E. Joubert, N. Fouquet, Airbus, C. Lents, L. Hardin, J. Rheaume, United Technologies Ediger, S. Ginn, NASA Armstrong Flight Research J. Thauvin, G. Barraud, Airbus, Toulouse, France; M. Suresnes, France Corporation, East Hartford, CT; L. Kohlman, NASA Glenn Center, Edwards, CA Budinger, Clément Ader Institute, Toulouse, France; Research Center, Cleveland, OH X. Roboam, University of Toulouse, Toulouse, France; D. Leray, Clément Ader Institute, Toulouse, France; B. Sareni, University of Toulouse, Toulouse, France Monday, 25 July 2016 34-APS-2 Space Transportation Development and Progress 151 G 1530 - 1800 hrs This panel will focus on future Mars exploration architectures and their transformation from vision to reality. Monday, 25 July 2016 35-ECS-1 Energetic Material, Detonation Transition and Ignition of Components 251 C Chaired by: J. BAGLINI, Exodynamics Technology Incorporated and S. SAWHILL, Systima Technologies, Inc. 1530 hrs 1600 hrs AIAA-2016-4614 AIAA-2016-4615 The Evolution of Retonation During DDT Multiscale Simulation of Shock to of Low Density HMX Detonation K. Gonthier, P. Rao, Louisiana State University, E. Fahrenthold, University of Texas, Austin, Baton Rouge, LA Austin, TX Monday, 25 July 2016 36-EDES-2 Energy Technologies for Aerospace and Terrestrial Applications 151 DE Chaired by: S. DUNCAN, Aerospace Systems Design Laboratory, Georgia Tech and L. MASON, NASA Glenn Research Center 1530 hrs 1600 hrs AIAA-2016-4616 AIAA-2016-4617 Improving the Simple Gas Turbine Cycle Efficient Liquid Fuel Consumption in with Compressed Air Energy Storage Household Cooking Appliances without (CAES) Back-flow Tendencies P. Lemieux, California Polytechnic State University, F. Ajibade, E. Ogedengbe, University of Lagos, San Luis Obispo, CA Akoka-Yaba, Nigeria Monday, 25 July 2016 37-EP-6 Hall Thruster Physics & Modeling II 250 A Chaired by: J. KOO and C. HUERTA 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4618 AIAA-2016-4619 AIAA-2016-4620 AIAA-2016-4621 Hall2De Simulations with a First-principles Continuum Kinetic Study of Magnetized Comparing Two-Dimensional, Development of a hybrid particle- Electron Transport Model Based on the Sheaths for Use in Hall Thrusters Axisymmetric, Hybrid-Direct Kinetic and continuum kinetic method for Hall Electron Cyclotron Drift Instability P. Cagas, B. Srinivasan, Virginia Polytechnic Hybrid-Particle-in-Cell Simulations of the thruster discharge plasmas I. Mikellides, B. Jorns, I. Katz, A. Lopez Ortega, Institute and State University, Blacksburg, VA; Discharge Plasma in a Hall Thruster K. Hara, Princeton Plasma Physics Laboratory, Jet Propulsion Laboratory, California Institute of A. Hakim, Princeton Plasma Physics Laboratory, A. Raisanen, University of Michigan, Ann Arbor, Princeton, NJ; S. Cho, Japan Aerospace Exploration Technology, Pasadena, CA Princeton, NJ Ann Arbor, MI; K. Hara, Princeton Plasma Physics Agency (JAXA), Chofu, Japan Laboratory, Princeton, NJ; I. Boyd, University of Michigan, Ann Arbor, Ann Arbor, MI Monday, 25 July 2016 38-EP-7 Hall Thruster Development 250 B 44 Chaired by: W. HARGUS, USAF/AFRL/RQRC and G. LI 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4622 AIAA-2016-4623 AIAA-2016-4624 AIAA-2016-4625 Parametric studies of velocity distribution Annular Hall Thruster with High Anode Laser Induced Fluorescence Measurements Operational Properties of UT-58 Anode functions for Xenon ions and neutrals in Efficiency in a Hall Thruster as a Function of Layer Hall Thruster with Modified cylindrical Hall thruster by laser-induced S. Lee, H. Kim, J. Kim, Y. Lim, W. Choe, Korea Background Pressure Magnetic Field and Guard-ring Material fluorescence Advanced Institute of Science and Technology, R. Spektor, W. Tighe, The Aerospace Corporation, J. Bak, Y. Hamada, Y. Hirano, K. Komurasaki, I. Romadanov, University of Saskatchewan, Saskatoon, Daejeon, South Korea El Segundo, CA T. Schönherr, H. Koizumi, University of Tokyo, Canada; P. Svarnas, University of Patras, Patras, Tokyo, Japan Greece; A. Diallo, Y. Raitses, Princeton Plasma Physics Laboratory, Princeton, NJ; A. Smolyakov, University of Saskatchewan, Saskatoon, Canada Monday, 25 July 2016 39-EP-8 Hollow Cathode Physics & Modeling 250 C Chaired by: W. HUANG, NASA Glenn Research Center and J. FRIEMAN 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4626 AIAA-2016-4627 AIAA-2016-4628 AIAA-2016-4629 First-principles Modelling of the IAT-driven First-principles modeling of the IAT-driven Numerical and Experimental Study on The High Frequency Potential Oscillations Anomalous Resistivity in Hollow Cathode anomalous resistivity in hollow cathode Discharge Characteristics of High-Current Near the Hollow Cathode in Ion Thrusters Discharges I: Theory discharges II: Numerical simulations and Hollow Cathode Y. Qin, K. Xie, Q. Xia, J. Ouyang, Beijing Institute B. Jorns, A. Lopez Ortega, I. Mikellides, Jet comparison with measurements K. Kubota, Japan Aerospace Exploration Agency (JAXA), of Technology, Beijing, China Propulsion Laboratory, California Institute of A. Lopez Ortega, I. Mikellides, B. Jorns, Jet Chofu, Japan; Y. Oshio, Tokyo University of Agriculture Technology, Pasadena, CA Propulsion Laboratory, California Institute of and Technology, Koganei, Japan; H. Watanabe, Technology, Pasadena, CA Tokyo Metropolitan University, Hino, Japan; S. Cho, Y. Ohkawa, I. Funaki, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Monday, 25 July 2016 40-EP-9 NEXT Ion Thruster Development 250 D Chaired by: E. CARDIFF, NASA and D. HERMAN, NASA Glenn Research Ctr 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4630 AIAA-2016-4631 AIAA-2016-4632 AIAA-2016-4633 Post-test Examination of NASA’s Evolutionary Post-test Examination of NASA’s Evolutionary Post-test Examination of NASA’s NEXT Thruster Performance Curve Xenon Thruster Long-Duration Test Hardware: Xenon Thruster Long-Duration Test Hardware: Evolutionary Xenon Thruster Long- Analysis And Validation Discharge Chamber Discharge and Neutralizer Cathodes Duration Test Hardware: Ion Optics P. Saripalli, University of Maryland, College Park, R. Shastry, G. Soulas, NASA Glenn Research Center, R. Shastry, G. Soulas, NASA Glenn Research Center, G. Soulas, R. Shastry, NASA Glenn Research College Park, MD; E. Cardiff, J. Englander, NASA Cleveland, OH Cleveland, OH Center, Cleveland, OH Goddard Space Flight Center, Greenbelt, MD Monday, 25 July 2016 41-F360-2 Launch Vehicle Reusability: Holy Grail, Chasing Our Tail, or Somewhere in Between Ballroom F 1530 - 1800 hrs Moderator: Dan Dumbacher, Professor Engineering Practice, School of Aeronautics and Astronautics, Purdue University Panelists: Gary Payton Jim Paulsen Ben Goldberg Tom Markusic Distinguished Visiting Professor Vice President Program Execution, Advanced Space & Launch Programs Vice President, Science and Engineering, Propulsions Systems Division Co-Founder and Chief Executive Officer United States Air Force Academy Aerojet Rocketdyne Orbital ATK Firefly Space Systems

Monday, 25 July 2016 42-FFP-1 Fossil-Fuel Power Technologies I 150 DE Chaired by: B. KHANDELWAL, The University of Sheffield and A. CHOUDHURI, University of Texas at El Paso 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4634 AIAA-2016-4635 AIAA-2016-4636 AIAA-2016-4637

45 Investigation on Flow-Flame Front Conceptual Study of Oxy-Methane Conceptual Design of a Supercritical Oxyfuel High Intensity Combustion of Methane Characteristics in a Backward Facing Step Flows in a Constant-Velocity Faraday Combustor Based on LOX/Methane Rocket and Propane using Oxygen Enhanced Air Combustor Using Laser Diagnostics Magnetohydrodynamic Generator Engine Technologies A. Said, A. Gupta, University of Maryland, College A. Acosta-Zamora, M. de la Torre, N. Love, A. M. Hernandez, L. Cabrera, A. Choudhuri, N. Love, A. Chowdhury, A. Badhan, L. Cabrera, A. Choudhuri, N. Park, College Park, MD Choudhuri, University of Texas, El Paso, El Paso, TX University of Texas, El Paso, El Paso, TX Love, University of Texas, El Paso, El Paso, TX Monday, 25 July 2016 43-GTE-4 Thermodynamic Topics of Gas Turbine Engines 250 F Chaired by: X. GAO, Colorado State Univ 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4638 AIAA-2016-4639 AIAA-2016-4640 AIAA-2016-4641 Exergy-Based Performance Analysis of a Gas Turbine Transient Response to Environmental Assessment of a Micro Turbojet Aerothermodynamic Benefits of Mixed Turbojet Engine Subsystem Architecture Secondary Power Engine with the Aid of Exergy Exhaust Turbofans M. Abbas, D. Riggins, Missouri University of Off-Takes K. Coban, Anadolu University, Eskisehir, Turkey; Y. S. Khalid, Gas Turbine Systems Solutions, LLC, Science and Technology, Rolla, MO M. Ozcan, I. Chakraborty, J. Tai, D. Mavris, Sohret, Suleyman Demirel University, Isparta, Turkey; Palm Beach Gardens, FL Georgia Institute of Technology, Atlanta, GA T. Karakoc, Anadolu University, Eskisehir, Turkey; C. Colpan, Dokuz Eylul University, Izmir, Turkey Monday, 25 July 2016 44-GTE-5 Compressors I 251 A Chaired by: M. ATTIA, Embry-Riddle Aeronautical University 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4642 AIAA-2016-4643 AIAA-2016-4644 AIAA-2016-4645 AIAA-2016-4646 Rotor Blade Fault Detection through Stationary Simulation of the Fluid- A Hybrid Vortex Solution for Surge Margin Stall and Surge Characteristics of a Two- Computational Study of the Effects of Statistical Analysis of Stationary Structure Interaction to Determine the Enhancement in Axial Compressors Volume Compression System Protruding Studs Casing Treatment on the Component Vibration Operating Geometry of a Blade in a M. Attia, D. Port, A. Rozendaal, Embry-Riddle A. Hickman, S. Morris, University of Notre Dame, Performance of an Axial Transonic Turbofan J. Cox, S. Arnold, P. Anusonti-Inthra, University of Transonic Axial Compressor Aeronautical University, Daytona Beach, FL Notre Dame, IN M. Collao, R. Webster, K. Sreenivas, W. Lin, University Tennessee, Tullahoma, Tullahoma, TN S. Aberle, R. Niehuis, University of the German of Tennessee, Chattanooga, Chattanooga, TN Federal Armed Forces, Neubiberg, Germany Monday, 25 July 2016 45-GTE-6 Air-Breathing Combustors II 251 B Chaired by: M. LIOU, NASA Glenn Research Center and A. CASWELL, USAF AFRL/RQTC 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4647 AIAA-2016-4648 AIAA-2016-4649 AIAA-2016-4650 AIAA-2016-4651 Investigation of differences in lean The Effect of Axial Spacing of Constant Precursors to blowout in a turbulent The Impact of Venturi Geometry on Enhancement of the Open National blowout of liquid single-component fuels and Variable Blockages on the combustor based on recurrence Reacting Flows in a Swirl-Venturi Lean Combustor Code (Open NCC) and Initial in a gas turbine model combustor Deflagration to Detonation Transition in a quantification Direct Injection Airblast Injector Simulation of Energy Efficient Engine J. Grohmann, B. Rauch, T. Kathrotia, W. Meier, M. Pulse Detonation Engine V. Unni, R. Sujith, Indian Institute of Technology X. Ren, X. Xue, C. Sung, University of Connecticut, K. Miki, J. Moder, M. Liou, NASA Glenn Research Aigner, German Aerospace Center (DLR), Stuttgart, N. Gagnon, M. Attia, Embry-Riddle Aeronautical Madras, Chennai, India Storrs, Storrs, CT; K. Brady, Innovative Scientific Center, Cleveland, OH Germany University, Daytona Beach, FL Solutions, Inc., Dayton, OH; H. Mongia, CSTI Associates, LLC, Yardley, PA; P. Lee, Woodward FST, Inc., Zeeland, MI Monday, 25 July 2016 46-GTE-9 Engine Control Systems 254 B Chaired by: D. FOUTCH, The Boeing Company 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4652 AIAA-2016-4653 AIAA-2016-4654 AIAA-2016-4655 A Network Scheduling Model for Advanced Control Considerations for The Application of Hardware in the Loop Aircraft Engine Advanced Controls Distributed Control Simulation Turbofan Engine Design Testing for Distributed Engine Control Research under NASA Aeronautics D. Culley, E. Aretskin-Hariton, G. Thomas, NASA J. Connolly, J. Csank, NASA Glenn Research Center, G. Thomas, N&R Engineering, Parma Heights, OH; D. Research Mission Programs Glenn Research Center, Cleveland, OH Cleveland, OH; A. Chicatelli, Vantage Partners, LLC, Culley, NASA Glenn Research Center, Cleveland, OH; A. S. Garg, NASA Glenn Research Center, Cleveland, Brook Park, OH Brand, Sporian Microsystems, Inc., Lafayette, CO OH Monday, 25 July 2016 47-HR-2 Design and Development of Novel Hybrid Rocket Motor Concepts I 255 B 46 Chaired by: M. KOBALD, DLR-German Aerospace Center and S. COOGAN, Southwest Research Institute 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4656 AIAA-2016-4657 AIAA-2016-4658 AIAA-2016-4659 Hybrid Propulsion In-Situ Resource Experimental Evaluation of a Throttled Launch-Assist Hybrid Rocket Investigation on Tri-propellant Hybrid Utilization Test Facility Results for Polyethylene/Nitrous Oxide Axial- Motor for an Airborne NanoSat Launch Rocket Performance Performance Characterization Injection, End-Burning Hybrid Platform. Y. Chen, National Space Organization, Hsinchu F. Mechentel, Stanford University, Stanford, CA; M. Hitt, R. Frederick, University of Alabama, S. Whitmore, Z. Spurrier, S. Walker, S. Merkley, Science Park, Taiwan; A. Lai, J. Lin, S. Wei, T. A. Karp, B. Nakazono, M. Parker, D. Vaughan, Huntsville, Huntsville, AL Utah State University, Logan, UT Chou, J. Wu, National Chiao Tung University, Jet Propulsion Laboratory, California Institute of Hsinchu, Taiwan Technology, Pasadena, CA Monday, 25 July 2016 48-HSABP-4 Advances in Hypersonic Air-Breathing Propulsion Systems 255 A Chaired by: E. AXDAHL, NASA Langley Research Center and G. PANIAGUA, Purdue University 1530 hrs 1600 hrs 1630 hrs AIAA-2016-4660 AIAA-2016-4661 AIAA-2016-4662 Experimental and Numerical Studies Characterization of the time-resolved Prediction of Mixing Efficiency between of Kerosene Fueled Scramjet Control starting process of supersonic diffusers Incoming Air and Embedded Rocket Exhaust Technology N. Thiry, University of Strathclyde, Glasgow, United within an RBCC Engine Q. Fu, Northwestern Polytechnical University, Kingdom; G. Paniagua, Purdue University, West T. Isono, R. Nakano, Tohoku University, Sendai, Japan; Xi’an, China Lafayette, IN S. Tomioka, K. Kudo, A. Murakami, S. Ueda, Japan Aerospace Exploration Agency (JAXA), Kakuda, Japan Monday, 25 July 2016 49-LP-4 Green Propellants II 251 D Chaired by: E. BESNARD, California State University–Long Beach and C. KIRCHBERGER, German Aerospace Center (DLR) 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4663 AIAA-2016-4664 AIAA-2016-4665 AIAA-2016-4666 AIAA-2016-4667 Predicting Flashing Phenomena: A Combustion Characteristics of GAP for Overview on the Gelled Propellants Long Duration Test Runs of a Highly Green Gelled Propellant Gas Generator Combined Approach of Numerical the Liquid Monopropellant -Effects of the Activities of DLR Lampoldshausen Throttleable Gelled Propellant Rocket Motor for High-Performance Divert- and Attitude Simulation and Experiments Spray Droplet Diameters- C. Kirchberger, P. Kröger, M. Negri, H. Ciezki, P. Pinto, J. Ramsel, K. Bauer, S. Risse, K. Control Systems C. Hendrich, German Aerospace Center (DLR), K. Hayashi, T. Kuwahara, Nihon University, German Aerospace Center (DLR), Lampoldshausen, Naumann, A. Thumann, Bayern-Chemie, Aschau K. Naumann, G. Tussiwand, Bayern-Chemie, Hardthausen, Germany; L. Gury, University of Funabashi, Japan Germany am Inn, Germany; et al. Aschau am Inn, Germany Applied Sciences, Wiener Neustadt, Austria; S. Schlechtriem, German Aerospace Center (DLR), Hardthausen, Germany Monday, 25 July 2016 50-LP-5 Nozzles I 251 E Chaired by: K. LOHNER, Stanford University 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4668 AIAA-2016-4669 AIAA-2016-4670 AIAA-2016-4671 AIAA-2016-4672 Experimental investigation of cold flow Scaling Effects on Side Load Generation in Hybrid RANS-LES Simulation of Separated A Numerical Model for Nozzle Flow CFD Analysis of Film Cooling and Heat TIC nozzles, a spectral analysis Subscale Rocket Nozzles Nozzle Flow Application under LOX/CH4 Hot Flow Transfer in a Bipropellant Rocket Nozzle, C. Genin, R. Stark, German Aerospace Center R. Stark, C. Genin, German Aerospace Center R. Larusson, N. Andersson, Chalmers University of Conditions Incorporating Chemically Reacting Flow (DLR), Lampoldshausen, Germany (DLR), Lampoldshausen, Germany Technology, Göteborg, Sweden; J. Östlund, GKN D. Schneider, C. Genin, German Aerospace Center N. Amato, J. Leylegian, M. Naraghi, Manhattan Aerospace Engine Systems, Trollhättan, Sweden (DLR), Lampoldshausen, Germany; S. Karl, V. College, Riverdale, NY Hannemann, German Aerospace Center (DLR), Göttingen, Germany

47 Monday, 25 July 2016 51-LP-6 Propellant Storage & Transfer II 251 F Chaired by: P. BEHRUZI, Airbus Defence & Space and S. BUSHMAN, Johns Hopkins University Applied Physics Laboratory 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4673 AIAA-2016-4674 AIAA-2016-4675 AIAA-2016-4676 AIAA-2016-4677 Modeling Droplet Heat and Mass Transfer Self-Pressurization of a Flightweight, Numerical Approach to Measure Numerical Modeling of Pressurization of Modeling Ullage Dynamics of Tank during Spray Bar Pressure Control of the Liquid Hydrogen Tank: Simulation and Accommodation Coefficients for Cryogenic Propellant Tank for Integrated Pressure Control Experiment during Jet Multipurpose Hydrogen Test Bed (MHTB) Comparison with Experiments Long-Duration Spaceflight Cryogenic Vehicle Fluid System Mixing in Microgravity Tank in Normal Gravity M. Stewart, Vantage Partners, LLC, Cleveland, Propellants A. Majumdar, A. LeClair, A. Hedayat, NASA O. Kartuzova, M. Kassemi, NASA Glenn Research O. Kartuzova, M. Kassemi, NASA Glenn Research OH; J. Moder, NASA Glenn Research Center, S. Alberts, P. Srikanth, S. Collicott, S. Heister, Marshall Space Flight Center, Huntsville, AL Center, Cleveland, OH Center, Cleveland, OH Cleveland, OH Purdue University, West Lafayette, IN Monday, 25 July 2016 52-LP-7 Propulsion Systems - Design & Test I 253 AB Chaired by: C. GATTO, Jet Propulsion Laboratory and R. BELL, Sierra Nevada 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4678 AIAA-2016-4679 AIAA-2016-4680 AIAA-2016-4681 AIAA-2016-4682 Vinci® propulsion system: Transition from Extending MESSENGER’s Low-Altitude Primary Mission Flight Performance of the Integrated Pressure-Fed Liquid Oxygen Cold Helium Pressurization for Liquid Ariane 5 ME to Ariane 6 Hover Campaign by Using Helium Van Allen Probes Propulsion Systems / Methane Propulsion Systems – Oxygen / Liquid Methane Propulsion J. Sannino, J. Delange, V. De Korver, Airbus, Paris, Pressurant as Cold-Gas Propellant J. John, S. Bushman, Johns Hopkins University Morpheus Experience, MARE, and Future Systems: Fully-Integrated Initial Hot-Fire France; A. Lekeux, B. Vieille, French Space Agency S. Bushman, C. Engelbrecht, S. Flanigan, M. Applied Physics Laboratory, Laurel, MD Applications Test Results (CNES), Paris, France Kirk, J. McAdams, D. Moessner, Johns Hopkins E. Hurlbert, M. Atwell, J. Melcher, R. Morehead, R. Morehead, M. Atwell, J. Melcher, E. Hurlbert, University Applied Physics Laboratory, Laurel, MD NASA Johnson Space Center, Houston, TX NASA Johnson Space Center, Houston, TX Monday, 25 July 2016 53-NFF-1 Fusion and Alternative Nuclear Concepts I 150 G Chaired by: J. CASSIBRY and G. WILLIAMS, Ohio Aerospace Institute 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4683 AIAA-2016-4684 AIAA-2016-4685 AIAA-2016-4686 Progress on Computational Modeling Development of a magnetic thrust On the Use of a Pulsed Nuclear Thermal Test Suite for Hydrodynamic Modeling for of Z-Pinch Nuclear Fusion Reactor chamber for a laser fusion rocket Rocket for Interplanetary Travel. Plasma Driven Magneto-Inertial Fusion Components for Spacecraft Propulsion M. Edamoto, N. Saito, T. Morita, N. Yamamoto, F. Arias, University of Catalonia, Barcelona, Spain K. Schillo, J. Cassibry, M. Rodriguez, University of M. Rodriguez, J. Cassibry, University of Alabama, Kyushu University, Kasuga, Japan; A. Sunahara, Alabama, Huntsville, Huntsville, AL Huntsville, Huntsville, AL Osaka University, Suita, Japan; R. Kawashima, Kyushu University, Kasuga, Japan; et al. Monday, 25 July 2016 54-PC-3 Ignition 255 C Chaired by: B. CHEHROUDHI, Advanced Technology Consultants and S. VASU, University of Central Florida 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4687 AIAA-2016-4689 AIAA-2016-4690 AIAA-2016-4691 AIAA-2016-4688 Ignition and Flame Propagation in a Alternative Jet Fuel Spray and Combustion Burning Rate and Ignition Delay Times of Shock Tube Ignition Studies of Advanced Design and Test of a Resonance Ignition Liquid-Fueled Swirling Combustor at Intermittent-Combustion Engine AP/HTPB-Based Solid Rocket Propellants Biofuels System for Green In-Orbit Propulsion M. Masquelet, S. Cao, M. Pai, General Electric Conditions Containing Graphene O. Pryor, G. Barari, B. Koroglu, J. Lopez, L. Nash, Systems Company, Niskayuna, NY J. Temme, M. Tess, C. Kweon, Army Research C. Dillier, A. Demko, T. Sammet, Texas A&M University, S. Vasu, University of Central Florida, Orlando, FL C. Bauer, O. Haidn, Technical University of Munich, Laboratory, Aberdeen Proving Ground, MD; V. College Station, TX; K. Grossman, S. Seal, University Munich, Germany Coburn, Engility, Aberdeen Proving Ground, MD of Central Florida, Orlando, FL; E. Petersen, Texas A&M University, College Station, TX Monday, 25 July 2016 55-PC-4 Spray Combustion 255 D 48 Chaired by: W. ANDERSON, Purdue University and G. LAMANNA, Universitaet Stuttgart 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4692 AIAA-2016-4693 AIAA-2016-4694 AIAA-2016-4695 Experimental Combustion Investigations Influence of Sleeve Angle on the LBO A Hybrid Eulerian-Eulerian/Eulerian- Crosswise Distribution of Kerosene Spray from Like-Impingement Sprays of Green Performance of TeLESS-II Combustor Lagrangian Method for Dense-to-Dilute in Crossflow Propellants B. Wang, C. Zhang, X. Hui, Y. Lin, Beihang Dispersed Multiphase Reacting Flows Y. Zhao, C. Zhang, Y. Lin, Y. Cheng, Beihang C. Indiana, M. Bellenoue, B. Boust, National Center for University, Beijing, China; J. Li, AVIC Commercial A. Panchal, G. Hannebique, M. Akiki, R. Ranjan, University, Beijing, China Scientific Research (CNRS), Futuroscope, France; S. Aircraft Engine Co., Ltd, Beijing, China S. Menon, Georgia Institute of Technology, Petitot, French Space Agency (CNES), Paris, France Atlanta, GA Monday, 25 July 2016 56-PC-5 Advanced Concepts 255 E Chaired by: R. HAUSEN, Honywell and A. STEINBERG, University of Toronto 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4696 AIAA-2016-4697 AIAA-2016-4698 AIAA-2016-4699 AIAA-2016-4700 Analysis of MHD Generators for use with Application of Additive manufacturing in Experimental and numerical investigation Experimental Investigation of Ignition Performance and Thermal Characteristics solid rocket motors Solid and Hybrid Grain Design of spray characteristics in a new FLOX® and Combustion Processes in a Constant- of Low-Power DC Arcjet Thrusters with Y. Metsker, J. Kugele, Technical University of C. Bauer, Y. Metsker, C. von Sethe, M. Mutschler, based combustor for liquid fuels for Micro Volume Combustion Chamber for Air- Radiation-Cooled Anodes for Green Munich, Munich, Germany; S. Nobbe, Ludwig M. Bambauer, P. Lungu, Technical University of Gas Turbine Range Extender (MGT-REX). Breathing Propulsion Propellants Maximilian University of Munich, Munich, Munich, Munich, Germany; et al. J. Gounder, A. Zizin, L. Oliver, M. Rachner, German B. Boust, Q. Michalski, M. Bellenoue, National S. Shiraki, H. Tahara, Osaka Institute of Germany; O. Haidn, Technical University of Aerospace Center (DLR), Stuttgart, Germany; S. Center for Scientific Research (CNRS), Poitiers, Technology, Osaka, Japan Munich, Munich, Germany Kulkarni, Delft University of Technology, Delft, The France Netherlands; M. Aigner, German Aerospace Center (DLR), Stuttgart, Germany Monday, 25 July 2016 57-SR-2 Solid Rocket Modeling and Simulation 254 A Chaired by: E. CAVALLINI, University of Roma “La Sapienza” and J. MAJDALANI, Auburn University 1530 hrs 1600 hrs 1630 hrs AIAA-2016-4701 AIAA-2016-4702 AIAA-2016-4703 Local Linear Stability Analysis of Non- Random Vibration Environment Standard VEGA Launch Vehicle Dynamic Loads due Circular Injection-Driven Channel Flows Deviation Variation Verification for Solid to Solid Propulsion Ignition Transients and M. Bouyges, F. Chedevergne, G. Casalis, ONERA, Rocket Motors Pressure Oscillations Toulouse, France R. Ott, Orbital ATK, Corinne, UT E. Cavallini, B. Favini, University of Rome “La Sapienza”, Rome, Italy; M. Castelli, A. Neri, ESA, Rome, Italy Monday, 25 July 2016 58-TM-2 Thermal System Applications and Unique Environments II 151 AB Chaired by: C. TARAU, Advanced Cooling Technologies and M. CHOI, NASA-Goddard Space Flight Center 1530 hrs 1600 hrs 1630 hrs Oral Presentation AIAA-2016-4704 AIAA-2016-4705 High Temperature Titanium-Water Heat Swift BAT Thermal Recovery After Loop Status of the Development of Low Cost Pipes for Kilopower Fission Power Systems Heat Pipe #0 Secondary Heater Controller Radiator for Surface Fission Power - III M. Ababneh, W. Anderson, D. Beard, C. Tarau, Failure in October 2015 C. Tarau, T. Maxwell, W. Anderson, C. Wagner, Advanced Cooling Technologies, Inc., Lancaster, PA M. Choi, NASA Goddard Space Flight Center, Advanced Cooling Technologies, Inc., Lancaster, PA; Greenbelt, MD M. Wrosch, Vanguard Space Technologies, Inc., San Diego, CA; M. Briggs, NASA Glenn Research Center, Cleveland, OH Monday, 25 July 2016 59-VS-1 Advanced Vehicle Systems Concepts 254 C 49 Chaired by: F. CHANDLER, Boeing Defense, Space & Security and T. CHEN, NASA 1530 hrs 1600 hrs AIAA-2016-4706 AIAA-2016-4707 Hypersonic Waverider Stream Surface Enabling Propulsion Technology Makes Actuation for Variable Design Point Operation Endo/Exoatmospheric Operating J. Maxwell, University of Maryland, College Park, Commercial Aircraft Possible College Park, MD B. Pande, iPropulsion, North Salt Lake, UT Monday, 25 July 2016 60-NW-3 Welcome Reception Exhibit Hall C 1800 - 1930 hrs Monday, 25 July 2016 61-NFF-2 Open Forum: Nuclear Propulsion in the 21st Century 150 G 1930 - 2130 hrs Tuesday Tuesday, 26 July 2016 62-PLNRY-3 Game Changing Developments in Propulsion and Energy Ballroom A-D 0800 - 0900 hrs Moderator: Janet Kavandi, Director, NASA Glenn Research Center Panelists: Jay Littles James Maughan Tom Markusic Director, Advanced Launch Vehicle Propulsion Global Technology Director Co-Founder and Chief Executive Officer Aerojet Rocketdyne GE Global Research Firefly Space Systems

Tuesday, 26 July 2016 63-NW-4 Networking Coffee Break Exhibit Hall C 0845- 0930 hrs Tuesday, 26 July 2016 64-ABPSI-3 Supersonic and Hypersonic Inlets 255 F Chaired by: J. SLATER, NASA Glenn Research Center and R. STARKEY, University of Colorado Boulder 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4708 AIAA-2016-4709 AIAA-2016-4710 Role of wall temperature on shock train in Computational experiments for improving the Investigation on Strut-based RBCC Engine a rectangular isolator performance of Fugine based on supermulti- Configuration to Improve Performance H. Lu, D. Wang, Z. Liu, China Academy of jets colliding working for a wide range of in M3-6 Aerospace Aerodynamics, Beijing, China; L. Yue, X. speeds from startup to hypersonic condition D. Yan, G. He, F. Qin, X. Wei, L. Shi, Northwestern Zhang, Institute of Mechanics, Chinese Academy of K. Tsuru, K. Naitoh, Waseda University, Tokyo, Japan Polytechnical University, Xi’an, China Sciences, Beijing, China 50 Tuesday, 26 July 2016 65-AEP-2 Aircraft Electric Propulsion II 150 DE Chaired by: L. GEA, Boeing Engineering Operations & Technology and C. CHUCK, Boeing Commercial Airplanes 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4711 AIAA-2016-4712 AIAA-2016-4713 Principles of High-efficiency Electric Flight Optimizing Power Density and Efficiency Potential of Aircraft Electric Propulsion with J. Barnes, Pelican Aero Group, San Pedro, CA of a Double-Halbach Permanent-Magnet SOFC/GT Hybrid Core Ironless Axial Flux Motor K. Okai, T. Himeno, T. Watanabe, University of K. Duffy, University of Toledo, Toledo, OH Tokyo, Bunkyo, Japan; H. Nomura, Nihon University, Narashino, Japan; T. Tagashira, A. Nishizawa, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Tuesday, 26 July 2016 66-ECD-2 Thermoelectric, Fuel Cell, and Photovoltaic Conversion Systems 151 G Chaired by: C. SANDIFER, NASA Glenn Research Center and S. WILSON, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4714 AIAA-2016-4715 AIAA-2016-4716 AIAA-2016-4717 AIAA-2016-4718 Development of Filled-Skutterudite Based Development of High Temperature Thermoelectric Generator Opportunity Optimal Thickness Analysis of the Dynamic Model of Solid Oxide Fuel Cell Thermopile for High Temperature Sensors Thermoelectric Device Technologies to Analysis for Commercial Gas Turbine Microporous Layer in an M.pudica Based Integrated with Fan and Exhaust Nozzle for Space and Terrestrial Applications Validated Materials Performance and Engines Photovoltaic Solar Cell V. Chakravarthula, R. Roberts, M. Wolff, Wright K. Smith, B. Li, S. Firdosy, S. Sujittosakul, M. Errico, Reliability for Advanced ThermoElectric J. Rheaume, D. Gerlach, United Technologies M. Shitta, E. Ogedengbe, I. Feyintola, University State University, Dayton, OH G. Nakatsukasa, Jet Propulsion Laboratory, California Couple (ATEC) Program Corporation, East Hartford, CT of Lagos, Akoka-Yaba, Nigeria Institute of Technology, Pasadena, CA; et al. B. Li, S. Firdosy, V. Ravi, K. Smith, D. Uhl, J. Ni, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; et al. Tuesday, 26 July 2016 67-ECS-2 Updates to Acceptance Methodologies for Energetic Components 251 C Chaired by: J. SCOTT, United Launch Alliance, LLC 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4719 AIAA-2016-4720 AIAA-2016-4721 Variations in the use of dynamics Methodology for Analyzing Non-Steady- Technical Evaluation and Proposed environments in the screening of State Thermal Transient Test (T3) Data Modifications for Ordnance Component ordnance components in LAT L. Yang, Self, La Canada Flintridge, CA Shock and Random Vibration Test J. Scott, K. Kostecka, United Launch Alliance, Requirements Centennial, CO J. Niehues, United Launch Alliance, Centennial, CO Tuesday, 26 July 2016 68-EDU-2 Propulsion Education II 251 B Chaired by: M. HITT, The University of Alabama in Huntsville and R. REZENDE 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4722 AIAA-2016-4723 AIAA-2016-4724 AIAA-2016-4725 UAH Propulsion Research Center - 25th K-12 Minority STEM Education Program: An Overview of Combustion Instabilities Overview of X-Ray Techniques for Anniversary Highlights MAA Southwest and Rocket Engine Injector Design Solid Rocket Propellant Regression R. Frederick, University of Alabama, Huntsville, H. Keerthi, P. Uptergrove, M. Everett, N. Love, A. C. Staschus, R. Frederick, University of Alabama, Measurements Huntsville, AL Choudhuri, University of Texas, El Paso, El Paso, TX Huntsville, Huntsville, AL D. Jones, R. Frederick, University of Alabama, Huntsville, Huntsville, AL Tuesday, 26 July 2016 69-EP-10 Hall Thruster Physics & Modeling III 250 A Chaired by: J. POLK, Jet Propulsion Laboratory and S. SAMPLES 0930 hrs 1000 hrs 1030 hrs

51 AIAA-2016-4726 AIAA-2016-4727 AIAA-2016-4728 A Unified Model for Axial-Radial and Influence of multiple factors on electron The Effects of Cathode Boundary Condition Axial-Azimuthal Hall Thruster Simulations behavior and transport process in a on Particle Simulation of a SPT-100-like Hall R. Kawashima, University of Tokyo, Tokyo, Japan; miniaturized hall thruster Thruster K. Hara, Princeton Plasma Physics Laboratory, Q. Liu, H. Tang, J. Ren, X. Shi, X. Lu, Beihang S. Cho, Japan Aerospace Exploration Agency (JAXA), Princeton, NJ; K. Komurasaki, H. Koizumi, University, Beijing, China Tokyo, Japan; H. Watanabe, Tokyo Metropolitan University of Tokyo, Tokyo, Japan University, Tokyo, Japan; K. Kubota, I. Funaki, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan Tuesday, 26 July 2016 70-EP-11 Hall Thruster Alternative Propellants 250 B Chaired by: L. KING, Michigan Technological University and B. DANKONGKAKUL 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4729 AIAA-2016-4730 AIAA-2016-4731 Overview of Iodine Propellant Hall Engineering Model Propellant Feed Condensable Propellant Hall Thruster for Thruster Development Activities at NASA System Development for an Iodine Hall Metallic Thin Film Deposition Glenn Research Center Thruster Demonstration Mission M. Hopkins, Riverside Research, Beavercreek, H. Kamhawi, T. Haag, G. Benavides, T. Hickman, K. Polzin, S. Peeples, A. Martinez, J. Seixal, OH; L. King, J. Drelich, J. Goldman, Michigan T. Smith, NASA Glenn Research Center, Cleveland, S. Mauro, A. Burt, NASA Marshall Space Flight Technological University, Houghton, MI; K. Baker, OH; G. Williams, Ohio Aerospace Institute, Center, Huntsville, AL; et al. William Beaumont Hospital, Royal Oak, MI Cleveland, OH; et al. Tuesday, 26 July 2016 71-EP-12 Hollow Cathode Development 250 C Chaired by: I. MIKELLIDES, Jet Propulsion Laboratory and C. DODSON 0930 hrs 1000 hrs AIAA-2016-4732 AIAA-2016-4733 Characterization and Qualification of a Advanced Dispenser-Type Cathode Low Current Heaterless Hollow Cathode Development for Electric Propulsion D. Lev, G. Alon, D. Mikitchuk, L. Appel, Rafael, W. Ohlinger, Self, Babson Park, FL; B. Vancil, eBeam, Haifa, Israel Inc., Beaverton, OR; J. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA Tuesday, 26 July 2016 72-EP-13 Helicon Thruster 250 D Chaired by: E. PENCIL, NASA Glenn Research Center and N. ARTHUR 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4734 AIAA-2016-4735 AIAA-2016-4736 AIAA-2016-4737 Current Status of the Helicon Injected Effects of Water Vapor Propellant on A Solid Propellant High Power Helicon Effects of Magnetic Nozzles and a Inertial Plasma Electrostatic Rocket Helicon Thruster Performance Thruster Downstream Antenna to the High Power D. Ahern, G. Miley, University of Illinois, Urbana- E. Petro, R. Sedwick, University of Maryland, I. Johnson, B. Roberson, R. Winglee, University Helicon Thruster Champaign, Urbana, IL College Park, College Park, MD of Washington, Seattle, Seattle, WA; I. Slobodov, B. Roberson, I. Johnson, I. Slobodov, R. Winglee, J. Prager, T. Ziemba, Eagle Harbor Technologies, University of Washington, Seattle, Seattle, WA; J. Inc., Seattle, WA Prager, T. Ziemba, Eagle Harbor Technologies, Inc., Seattle, WA Tuesday, 26 July 2016 73-EP-14 Electrospray II 250 E Chaired by: J. DANKANICH, NASA Marshall Space Flight Center and C. MILLER 52 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4738 AIAA-2016-4739 AIAA-2016-4740 Microfluidic Electrospray Propulsion(MEP) Electrospray Thruster Propellant Feedsystem Mass Spectrometry of Selected Ionic Thruster Performance with Microfabricated for a Gravity Wave Observatory Mission Liquids in Capillary Electrospray at Emitter Arrays for Indium Propellant N. Demmons, N. Lamarre, Busek Company, Inc., Nanoliter Volumetric Flow Rates C. Marrese-Reading, Jet Propulsion Laboratory, Natick, MA; J. Ziemer, M. Parker, Jet Propulsion S. Miller, Boston College, Chestnut Hill, MA; B. California Institute of Technology, Pasadena, CA Laboratory, California Institute of Technology, Pasadena, Prince, R. Bemish, Air Force Research Laboratory, CA; D. Spence, Busek Company, Inc., Natick, MA Kirtland AFB, NM; J. Rovey, Missouri University of Science and Technology, Rolla, MO Tuesday, 26 July 2016 74-F360-3/LP-11 Liquid Propulsion History Session: Lessons Learned Ballroom F 0930 - 1200 hrs Chaired by: T. Kent Pugmire (ret.)

Leaders in the liquid propulsion community share their personal experiences from working in academia, small and large aerospace companies, and government institutions. Topics covered range from dealing with technical and programmatic difficulties in system and organization evolutions to personal challenges encountered.

Making Rocket Programs a Success in Universities? History of the Maurice Zucrow Lab at Purdue University International Cooperation on the Delta, Sea Launch and Antares Programs Eric Besnard Stephen Heister John Steinmeyer Professor of Mechanical and Aerospace Engineering Raisbeck Distinguished Professor, Director of the Maurice J. Zucrow Laboratory Business Development Director California State University, Long Beach Purdue University Orbital ATK Lessons Learned from Industry, Private Venture, and Federal Government 30 Years after Challenger - Ethics Lessons Learned but Forgotten Michael Kelly Allan McDonald Chief Engineer, FAA Office of Commercial Space Transportation Aerospace Consultant and Author of Federal Aviation Administration Truth, Lies, and O-Rings: Inside the Space Shuttle Challenger Disaster Tuesday, 26 July 2016 75-GEPC-1 Low Carbon Aviation-Propulsion Integration, Gas Turbines, and Fuels 254 B Chaired by: M. BRADLEY, Boeing Commercial Airplanes and T. ABDEL-SALAM, East Carolina University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation National Research Council - Low Carbon Sustainable Alternative Jet Fuel Deployment The Role and Future of Gas Turbine Technologies and Innovation for Low Low Carbon Aviation: Fleet Level System Aviation: Study Background and for Low Carbon Aviation: Goals, Progress, and Propulsion in Low Carbon Aviation Carbon Aviation Studies Expectations Research Needs Remaining A. Epstein, Pratt & Whitney , Palm Beach, FL E. Ducharme , GE Aviation, Ashville, NC D. DeLaurentis, Purdue University, West Lafayette, IN B. Esker, NASA Headquarters, Wahington DC, D.C. S. Csonka, Commercial Aviation Alternative Fuels Initiative (CAAFI) , Washington, D.C. Tuesday, 26 July 2016 76-GTE-7 Turbines II 250 F Chaired by: M. RICKLICK, Embry Riddle Aeronautical University 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4741 AIAA-2016-4742 AIAA-2016-4743 Validation of Magnetic Resonance Experimental Analysis of an Axial Turbine A Detailed Experimental and Numerical Thermometry through Experimental and Driven by Periodic Pressure Pulses Investigation of Flow and Heat Transfer Computational Approaches M. Fernelius, S. Gorrell, Brigham Young University, in a Single Row Narrow Impingement J. Spirnak, M. Samland, B. Tremont, A. McQuirter, Provo, UT Channel Using PIV and LES E. Williams, M. Benson, U.S. Military Academy, J. Hossain, E. Fernandez, J. Kapat, University of West Point, NY; et al. Central Florida, Orlando, FL Tuesday, 26 July 2016 77-GTE-8 Compressors II 251 A Chaired by: K. MANI, Rolls-Royce Corporation

53 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4744 AIAA-2016-4745 AIAA-2016-4746 Design and Analysis of a High Pressure Validation of a Two-Equation VLES Implementation of Fourier methods in Ratio Mixed Flow Compressor Stage Turbulence Model Using a Transonic Axial CFD to analyze distortion transfer and A. Nassar, G. Giri, SoftInWay, Inc., Bengaluru, Compressor Stage generation through a transonic fan India; L. Moroz, A. Sherbina, I. Klimov, SoftInWay, R. Kelly, A. Hickman, K. Shi, S. Morris, A. Jemcov, M. Peterson, S. Gorrell, Brigham Young University, Inc., Burlington, MA University of Notre Dame, Notre Dame, IN Provo, UT; M. List, Air Force Research Laboratory, Wright-Patterson AFB, OH; C. Custer, CD-adapco, Northville, MI Tuesday, 26 July 2016 78-HR-3 Internal Ballistics Modeling I 253 AB Chaired by: B. EVANS, Stanford University and S. CLAFLIN, Aerojet Rocketdyne 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4747 AIAA-2016-4748 AIAA-2016-4749 AIAA-2016-4750 AIAA-2016-4751 Method for Determining Nozzle Throat Numerical analysis of grain port scale and Optimization of Hybrid Sounding Rockets Scaling of Hybrid Rocket Motors with Quasi 1-D Numerical Analysis of Erosion History in Hybrid Rockets firing test of long-time working hybrid Through Coupled Motor-Trajectory Swirling Oxidizer Injection - Part 2 Combustion Instability in Hybrid Rocket L. Kamps, Y. Saito, R. Kawabata, Y. Takahashi, H. motor Simulation E. Paccagnella, F. Barato, D. Pavarin, University Motor Incorporating Boundary Layer Lags Nagata, Hokkaido University, Sapporo, Japan X. Sun, H. Tian, Y. Zhang, H. Zhu, Beihang M. Ghilardi, F. Barato, D. Pavarin, University of of Padova, Padova, Italy; A. Karabeyoglu, Space G. Karthikeyan, T. Shimada, Japan Aerospace University, Beijing, China Padua, Padua, Italy Propulsion Group, Inc., Palo Alto, CA Exploration Agency (JAXA), Sagamihara, Japan Tuesday, 26 July 2016 79-HR-4 Combustion Dynamics and Mixing Efficiencies II 255 B Chaired by: B. CANTWELL, Stanford University and Y. CHEN, National Space Organization Taiwan 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4752 AIAA-2016-4753 AIAA-2016-4754 AIAA-2016-4755 Experimental and Analytical Investigation Measuring Nozzle Erosion in a Hybrid Development of a Hybrid Rocket Slab Fuel Regression Behavior of a Swirling- of Effect of Pressure on Regression Rate of Rocket Motor with Ultrasound Motor Injection End-Burning Hybrid Rocket Axial-Injection End-Burning Hybrid Rockets P. Narsai, K. Venkataraman, K. Stober, B. Cantwell, R. Theba, K. Veale, C. Bemont, University of Engine using Paraffin-based Fuels Y. Saito, T. Yokoi, H. Nagata, Hokkaido University, Stanford University, Stanford, CA KwaZulu-Natal, Durban, South Africa Y. Oishige, D. Hayashi, T. Sakurai, Tokyo Sapporo, Japan; H. Yasukochi, K. Soeda, University of Metropolitan University, Hino, Japan Tokyo, Tokyo, Japan; T. Totani, Hokkaido University, Sapporo, Japan; et al. Tuesday, 26 July 2016 80-HSABP-5 Numerical Analysis of Supersonic Combustion Flow Paths, Components, and Processes 254 C Chaired by: F. MALO-MOLINA, Raytheon Missile Systems and F. LADEINDE, TTC Technologies Inc 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4756 AIAA-2016-4757 AIAA-2016-4758 AIAA-2016-4759 AIAA-2016-4760 Combustion Performance of Hydrocarbon Research on Mixing Control by Injection Performance Prediction of Diverging Dual- Asymmetric Combustion Characteristics Supersonic Mixing and Combustion studies Fuel in a Dual-Mode Combustor Scheme in Dual-Mode Combustor mode Combustors at Ramjet-mode Operation of Transverse Ethylene Injection in a using Decoupling Strategy K. Nojima, M. Soejima, T. Arakawa, Tohoku T. Arakawa, S. Ishizaki, K. Nojima, Tohoku S. Tomioka, M. Takahashi, K. Kobayashi, K. Tani, Rectangular Supersonic Combustor with Y. Wang, W. Song, Northwestern Polytechnical University, Sendai, Japan; S. Tomioka, N. University, Sendai, Japan; S. Tomioka, N. Japan Aerospace Exploration Agency (JAXA), Kakuda, Single-side Expansion University, Xi’an, China; H. Bai, China Sakuranaka, Japan Aerospace Exploration Agency Sakuranaka, Japan Aerospace Exploration Agency Japan; K. Nojima, T. Arakawa, Tohoku University, M. Sun, National University of Defense Technology, Aerodynamics Research and Development Center (JAXA), Kakuda, Japan (JAXA), Kakuda, Japan Sendai, Japan Changsha, China (CARDC), Mianyang, China Tuesday, 26 July 2016 81-HSABP-6 High Fidelity Simulations of High-Speed Air-Breathing Systems 255 A 54 Chaired by: V. TANGIRALA, General Electric and R. SPRINGER, Johns Hopkins University Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4761 AIAA-2016-4762 AIAA-2016-4763 AIAA-2016-4764 Detached Eddy Simulation of a high-Ma Computational Analysis of Flow Control of Shock-Induced Boundary Layer CFD Analysis of Mixing Characteristics of regenerative-cooled scramjet combustor Phenomena in a Back-Pressured Separation by High Momentum Blowing Several Fuel Injectors at Hypervelocity based on skeletal kerosene mechanism Supersonic Isolator D. Cuppoletti, C. Saucier, C. Harris, Northrop Flow Conditions W. Yao, Y. Lu, X. Li, J. Wang, X. Fan, Chinese M. Hagenmaier, E. Hassan, Air Force Research Grumman Corporation, El Segundo, CA T. Drozda, R. Baurle, NASA Langley Research Academy of Sciences, Beijing, China Laboratory, Wright-Patterson AFB, OH Center, Hampton, VA Tuesday, 26 July 2016 82-ITAR-1 Gas Turbines and Associated Equipment (CAT-XIX) 151 DE Chaired by: C. LI, Air Force Office of Scientific Research and K. MILLSAPS, Naval Postgraduate School 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4765 Oral Presentation AIAA-2016-4766 AIAA-2016-4767 Initial Comparison of Experimental and NRL Simulations of a Rotating-Detonation- Integrated Fiber Optic Sensor (IFOS) Thermodynamics of RDE Flow with Axial Numeric Premixed Rotating Detonation Wave Engine Concept System Flow Turbine Engines K. Kailasanath, D. Schwer, Naval Research N. Ma, Physical Optics Corporation, Torrance, CA; C. Nordeen, University of Connecticut, Storrs, I. Andrus, P. King, M. Polanka, Air Force Institute of Laboratory, Washington, D.C. A. Ghoshal, Army Research Laboratory, Aberdeen Storrs, CT; R. Munipalli, Z. Liu, HyPerComp, Inc., Technology, Wright-Patterson AFB, OH; F. Schauer, Proving Ground, MD; T. Nielsen, V. Romanov , Westlake Village, CA; B. Cetegen, University of Air Force Research Laboratory, Wright-Patterson Physical Optics Corporation, Torrance, CA Connecticut, Storrs, Storrs, CT AFB, OH; J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH Tuesday, 26 July 2016 83-LP-8 Nozzles II 251 D Chaired by: S. FORDE, Aerojet Rocketdyne and S. MILLER, Aerojet Rocketdyne 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4768 AIAA-2016-4769 AIAA-2016-4770 AIAA-2016-4771 Performance Evaluation of Aerospike Nozzles 3D Numerical Studies on Thrust Vectoring Diagnostic Investigation of Nozzle Flow Rapid Fabrication Techniques for Liquid for Lucrative Thrust Vector Control using Shock Induced Self Impinging Choking Time and Stage Separation Rocket Channel Wall Nozzles S. Ajith, A. S, M. Raj, R. S, Kumaraguru College of Secondary Jets Sequence of a Multi-stage Rocket P. Gradl, NASA Marshall Space Flight Center, Technology, Coimbatore, India; T. Ramesh kumar, N. Vishnu, S. Vigneshwaran , S. Vignesh, . Nichith V. Sanal Kumar, . Nichith , S. Vigneshwaran , Huntsville, AL Auburn University, AL, AL; V. Sanal Kumar, Kumaraguru , S. Sharan, V. Sanal Kumar, Kumaraguru College A. S, A. Kumar, S. Ajith, Kumaraguru College of College of Technology, Coimbatore, India of Technology, Coimbatore, India Technology, Coimbatore, India; et al. Tuesday, 26 July 2016 84-LP-9 Propellant Storage & Transfer III 251 E Chaired by: M. MEYER, NASA Glenn Research Center and D. KIRK, Florida Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4772 AIAA-2016-4773 AIAA-2016-4774 AIAA-2016-4775 A Detailed Historical Review of Propellant Experimental Investigation on Liquid Analytical Prediction of Peak Pressure Design and Operation of a Calorimeter for Management Devices for Low Gravity Acquisition Devices by Mesh-type Baffles Transients Occurring During The Priming Advanced Multilayer Insulation Testing Propellant Acquisition S. Hamajima, T. Himeno, Y. Sakuma, University of a Spacecraft Propulsion System D. Chato, W. Johnson, NASA Glenn Research J. Hartwig, NASA Glenn Research Center, of Tokyo, Tokyo, Japan; Y. Umemura, H. Negishi, J. Flynn, Orbital ATK, Dulles, VA Center, Cleveland, OH; N. Van Dresar, Self, Cleveland, OH Japan Aerospace Exploration Agency (JAXA), Driggs, ID Tsukuba, Japan; K. Ishikawa, Mitsubishi Group, Nagoya, Japan; et al. Tuesday, 26 July 2016 85-NFF-3 Fusion and Alternative Nuclear Concepts II 150 G 55 Chaired by: M. RODRIGUEZ and B. PALASZEWSKI, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4776 AIAA-2016-4777 AIAA-2016-4778 Inertial Electrostatic Confinement Fusion Novel Inertial Electrostatic Confinement A Hybrid Solid/Gas Core Nuclear Thermal Simulation and a Statistical Treatment of Fusion with Buckyball Shaped Grids Rocket Engine for Future Solar System Coulomb Collisions J. Wulfkuehler, M. Tajmar, Technical University of Exploration. A. Chap, R. Sedwick, University of Maryland, Dresden, Dresden, Germany L. Beveridge, Idaho State University, Pocatello, ID College Park, College Park, MD Tuesday, 26 July 2016 86-PC-6 Combustion Chemistry 255 C Chaired by: T. JACKSON, University of Florida and N. SLAVINSKAYA, DLR - German Aerospace Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4779 AIAA-2016-4780 AIAA-2016-4781 AIAA-2016-4782 Characterizing NOx Emissions for Air- Density Functional Theory Investigations Skeletal Mechanism of the Methane Ignition Delay Testing of Various Hypergolic Breathing Rotating Detonation Engines on Bulk Iridium Structures for ReaxFF Oxidation for Space Propulsion Ionic liquids and Oxidizers D. Schwer, K. Kailasanath, Naval Research Catalysis Parameterization Applications A. Thomas, K. Stober, Stanford University, Stanford, CA; Laboratory, Washington, D.C. D. Depew, J. Wang, University of Southern N. Slavinskaya, German Aerospace Center (DLR), R. Al Otaibi, M. Alotaibi, N. Almuqati, King Abdulaziz California, Los Angeles, CA Stuttgart, Germany; O. Haidn, Technical University City for Science and Technology, Riyadh, Saudi Arabia; of Munich, Munich, Germany B. Evans, Stanford University, Stanford, CA; et al. Tuesday, 26 July 2016 87-PC-7 Air-Breathing Combustion Modeling 255 D Chaired by: S. MENON, Georgia Institute of Technology and L. SMITH, United Technologies Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4783 AIAA-2016-4784 AIAA-2016-4785 AIAA-2016-4786 CFD Based Design of a Filming Injector for Effect of Radiation on Gas Turbine LES validation practices in a model aero- Large-Eddy Simulation of a Full Annular N+3 Combustors Combustor Liner Temperature with engine combustor at engine relevant RQL Combustion Chamber & Fuel K. Ajmani, Vantage Partners, LLC, Cleveland, OH; Conjugate Heat Transfer (CHT) conditions Distribution Effects on the Combustor Exit H. Mongia, Purdue University, West Lafayette, IN; Methodology S. Yellapantula, K. Venkatesan, General Electric Temperature Profile P. Lee, Woodward FST, Inc., Zeeland, MI Y. Saygin, S. UsLu, TOBB University of Economics Company, Niskayuna, NY; A. Pratt, C. Slabaugh, R. O. Kocaman, T. Aksu, S. UsLu, TOBB University of and Technology, Ankara, Turkey Lucht, Purdue University, West Lafayette, IN Economics and Technology, Ankara, Turkey Tuesday, 26 July 2016 88-PC-8 Cryogenic Sprays 255 E Chaired by: V. SANKARAN, US Air Force/AFRL/RQRC and H. TERASHIMA, Hokkaido University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4787 AIAA-2016-4788 AIAA-2016-4789 AIAA-2016-4790 AIAA-2016-4791 Cryogenic Flashing Jets: A Review (Invited Trajectory and Breakup of Cryogenic Jets Sub- or Supercritical? A flamelet analysis Injection of Cryogenic Propellants under High Fidelity Large Eddy Simulation of Paper) in Crossflow of high pressure rocket propellant Low Pressure Conditions Reacting Supercritical Fuel Jet-in-Cross- G. Lamanna, University of Stuttgart, Stuttgart, W. Richards, A. Steinberg, University of Toronto, injection M. Luo, O. Haidn, Technical University of Munich, Flow using GPU acceleration Germany Toronto, Canada D. Banuti, Stanford University, Stanford, CA; J. Munich, Germany K. Gottiparthi, R. Sankaran, Oak Ridge National Hickey, University of Waterloo, Waterloo, Canada; Laboratory, Oak Ridge, TN; J. Oefelein, Sandia M. Ihme, Stanford University, Stanford, CA National Laboratories, Livermore, CA Tuesday, 26 July 2016 89-SR-3 Solid Rocket Combustion Instability 254 A Chaired by: A. SPURLING, Naval Air Warfare Center Weapons Division and C. ROUSSEAU, Denel (Pty) Ltd. 56 0930 hrs 1000 hrs AIAA-2016-4792 AIAA-2016-4793 Biglobal Instability of the Compressible Motor Scale and Propellant Geometry Taylor-Culick Solution in Cylindrical Effects on Pressure Oscillations in Aft- Rockets Finocyl Solid Rocket Motors M. Akiki, Georgia Institute of Technology, Atlanta, E. Cavallini, B. Favini, University of Rome “La GA; J. Majdalani, Auburn University, Auburn, AL Sapienza”, Rome, Italy; A. Neri, ESA, Rome, Italy Tuesday, 26 July 2016 90-TM-3 Thermal System Applications and Unique Environments III 151 AB Chaired by: J. MEHTA, Belcan AETD and C. TARAU, Advanced Cooling Technologies 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4794 AIAA-2016-4795 AIAA-2016-4796 AIAA-2016-4797 AIAA-2016-4798 Investigations into the thermal Development of a radiative heating Copper-Methanol Heat Pipes Development A novel spiral regenerator suitable Investigation of Insulation Effect on performance of a helically coiled closed system for studies of heat transfer in for Electronics Cooling of Surveillance for MICSE and the study on its hybrid Spacecraft Thermal Control System loop oscillating heat pipe fuel-cooled structures Equipment thermodynamic cycle A. Farag, Egyptian Armed Forces, Cairo, Egypt; A. S. Yeboah, University of Nottingham, Ningbo, D. Dong, Y. Lu, Y. Yuan, X. Fan, Chinese Academy R. Riehl, National Institute for Space Research Z. Zhang, G. Huang, C. Xia, Y. Xu, Nanjing Elzahaby, Tanta University, Cairo, Egypt; M. Khalil, China; J. Darkwa, University of Nottingham, of Sciences, Beijing, China (INPE), São José dos Campos, Brazil University of Aeronautics and Astronautics, T. Wafi, Egyptian Armed Forces, Cairo, Egypt; E. Nottingham, United Kingdom Nanjing, China Khalil, Cairo University, Giza, Egypt Tuesday, 26 July 2016 91-PLNRY-4 High Power Systems for Aerospace Applications Ballroom A-D 1300 - 1430 hrs Moderator: Graham Warwick, Managing Editor, Technology, Aviation Week and Space Technology Panelists: John Nairus John “Rick” Hooker John H. Scott Randy Furnas Chief Engineer, Power & Control Division Design Engineer Chief Technologist, Propulsion and Power Division Chief, Power Division Air Force Research Laboratory Lockheed Martin Aeronautics NASA Johnson Space Center NASA Glenn Research Center

Tuesday, 26 July 2016 92-NW-5 Networking Coffee Break Exhibit Hall C 1430 - 1500 hrs Tuesday, 26 July 2016 93-ABPSI-4 Subsonic Inlets & Aerodynamic Interaction 255 F Chaired by: T. BERENS, AIRBUS Defence and Space and M. HAGEMAN 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4799 AIAA-2016-4800 AIAA-2016-4801 AIAA-2016-4802 AIAA-2016-4803 Design point analysis of a distributed Installed Performance Assessment of a Numerical Investigation of the Effect of Three Dimensional Design Optimization Studies on Boundarylayer Blockage and propulsion system with boundary layer Boundary Layer Ingesting Distributed Wing Position on the Aeroacoustic Field of Using Adjoint Method with Newton Krylov External Flow Choking at Moving Wing in ingestion implemented in UAV’s for Propulsion System at Design Point a Propeller Solver Ground Effect agriculture in the Andean region C. Goldberg, D. Nalianda, P. Pilidis, D. MacManus, D. Boots, D. Feszty, Carleton University, Ottawa, A. Yıldırım, S. Eyi, Middle East Technical University, S. Vignesh, S. Ganesh Shankar, S. Ajith, S. Vivek, E. Valencia, National Polytechnic School, Quito, Cranfield University, Cranfield, United Kingdom; J. Canada Ankara, Turkey S. Mani, V. Sanal Kumar, Kumaraguru College of Ecuador; V. Hidalgo, Tsinghua University, Beijing, China; Felder, NASA Glenn Research Center, Cleveland, Technology, Coimbatore, India J. Cisneros, National Polytechnic School, Quito, Ecuador OH

57 Tuesday, 26 July 2016 94-AEC-2 Advanced Engine Control & Intelligent Systems II 150 DE Chaired by: R. MILLAR, Naval Postgraduate School and A. BEHBAHANI, AFRL/RQT 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4804 AIAA-2016-4805 AIAA-2016-4806 AIAA-2016-4807 AIAA-2016-4808 AIAA-2016-4809 Intelligent Nodal-Based Controls Technologies Development of Distributed Control Modeling of a Gas Turbine Using Performing Diagnostics & Prognostics On Reconfigurable Distributed Control Integrated Robust and Resilient Control of for Integrated Propulsion Energy / Power / Systems for Aircraft Turbofan Engines Distributed Networks with Smart Nodes Simulated Engine Failures Using Neural Systems for Turbine Engine Operation Propulsion Systems Thermal Management Systems T. Seitz, Ohio State University, Columbus, OH; and Multiple Time Delays Networks Uncertainties A. Behbahani, Air Force Research Laboratory, A. Behbahani, Air Force Research Laboratory, Wright- O. Macmann, University of Cincinnati, Cincinnati, T. Seitz, R. Yedavalli, Ohio State University, O. Macmann, University of Cincinnati, Cincinnati, S. Zein-Sabatto, M. Bodruzzaman, C. McCurry, Wright-Patterson AFB, OH; O. Macmann, University Patterson AFB, OH; R. Roberts, Wright State University, OH; A. Behbahani, Air Force Research Laboratory, Columbus, OH; O. Macman, University of OH; T. Seitz, Ohio State University, Columbus, Tennessee State University, Nashville, TN; A. of Cincinnati, Cincinnati, OH; T. Seitz, Ohio State Dayton, OH; A. Chandoke, Air Force Research Wright-Patterson AFB, OH; F. Khoury, Purdue Cincinnati, Cincinnati, OH; A. Behbahani, Air Force OH; A. Behbahani, Air Force Research Laboratory, Behbahani, Air Force Research Laboratory, Wright- University, Columbus, OH; R. Buettner, Wright Laboratory, Wright-Patterson AFB, OH University, Lafayette, IN Research Laboratory, Wright-Patterson AFB, OH Wright-Patterson AFB, OH; K. Cohen, University of Patterson AFB, OH State University, Dayton, OH Cincinnati, Cincinnati, OH Tuesday, 26 July 2016 95-APC-2 Advanced Propulsion Concepts I 251 D Chaired by: A. REISZ, Reisz Engineers and J. ROBINSON, Retired f/Boeing 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-4810 AIAA-2016-4811 AIAA-2016-4812 AIAA-2016-4813 Parametric Cycle Analysis of a Computational Fluid Dynamics Simulations Aerodynamic Design and Analysis of the Experimental Investigation of a Baffled- Turbofan with Core Engine Replaced by and Validation of a Novel Constant Volume Hyperloop Pod Tube Ram Accelerator Revolutionary Innovative Turbine Engine Combustion Jet Engine J. Braun, J. Sousa, C. Pekardan, Purdue University, C. Knowlen, J. Glusman, R. Grist, A. Bruckner, F. Yang, Z. Wang, Z. Liu, L. Zhou, X. Zhang, J. Travis, A. Kuznetsov, North Carolina State University, West Lafayette, IN University of Washington, Seattle, Seattle, WA; A. Northwestern Polytechnical University, Xi’an, China Raleigh, NC; W. Roberts, King Abdullah University of Higgins, McGill University, Montréal, Canada Science and Technology, Thuwal, Saudi Arabia Tuesday, 26 July 2016 96-APS-3 Space Nuclear Power Generation 151 G Chaired by: J. HAINES, Retired - formerly ESA/ESTEC and M. PATEL, US Merchant Marine Academy 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-4814 AIAA-2016-4815 AIAA-2016-4816 AIAA-2016-4817 Performance Testing of the EU/QU The Selenide Saga: A Contribution Advanced Stirling Radioisotope Generator Enhancement of the Multi-Mission MMRTG Toward a History of the Selenide Isotope EU2 Anomaly Investigation Radioisotope Thermoelectric Generator C. Barklay, University of Dayton Research Institute, Generator E. Lewandowski, S. Oriti, NASA Glenn Research with Efficient Skutterudite Thermoelectric Dayton, OH; B. Tolson, UES, Inc., Dayton, OH; G. Bennett, Metaspace Enterprises, Boise, ID Center, Cleveland, OH Couples: Current Status of the Skutterudite G. Bolotin, N. Keyawa, W. David, Jet Propulsion Technology Maturation Program Laboratory, California Institute of Technology, T. Holgate, Y. Song, D. Shi, R. Utz, T. Chung, R. Pasadena, CA Bennett, Teledyne, Hunt Valley, MD; et al. Tuesday, 26 July 2016 97-EE-1 Systems-Level Analysis of Energy Efficiency and Renewable Energy 150 G Chaired by: E. OGEDENGBE, ENERGHX Consulting/University of Lagos and S. DUNCAN, Aerospace Systems Design Laboratory, Georgia Tech 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4818 AIAA-2016-4819 AIAA-2016-4820 AIAA-2016-4821 AIAA-2016-4822 AIAA-2016-4823 A Building Thermal Demand Model for a A Parametric Modeling of Water-to-air “Synthetic shroud” concept for wind Air Craft Winglet Design and Performance: Separation analysis in a high-speed A Center for Aviation Systems Efficiency District Energy System Heat Exchanger Based on CFD Analysis turbine performance optimization Cant Angle Effect rotating cylinder for a binary gas mixture D. Erbschloe, Self, Caseyville, IL; W. Harrison, J. Lewe, S. Oh, H. Solano, D. Mavris, Georgia S. Wojnarska, Procter & Gamble Company, Zabki, D. Feszty, Carleton University, Ottawa, Canada; E. Khalil, E. AbdelGhany, G. ElHarriri, Cairo S. Pradhan, Indian Institute of Science, Bengaluru, Air Force Research Laboratory, Wright-Patterson Institute of Technology, Atlanta, GA Poland; J. Lewe, K. Song, S. Duncan, Georgia S. McTavish, National Research Council Canada, University, Cairo, Egypt; O. Abdellatif, Benha India AFB, OH Institute of Technology, Atlanta, GA Ottawa, Canada; I. Bodnya, D. Jee, Carleton University, Cairo, Egypt University, Ottawa, Canada Tuesday, 26 July 2016 98-EP-15 HERMeS Hall Thruster I 250 A 58 Chaired by: M. WALKER, Georgia Institute of Technology and K. TERHUNE 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4824 AIAA-2016-4825 AIAA-2016-4826 AIAA-2016-4827 AIAA-2016-4828 AIAA-2016-4829 The Ion Propulsion System for the Asteroid Development Status of the 12.5 kW HERMeS Performance, Facility Pressure Effects, and Performance Comparison of the 12.5 Facility Effect Characterization Test of Plasma Oscillation Characterization of Redirect Robotic Mission Hall Thruster for the Solar Electric Propulsion Stability Characterization Tests of NASA’s kW HERMeS Hall Thruster Technology NASA’s HERMeS Hall Thruster NASA’s HERMeS Hall Thruster via High D. Herman, W. Santiago, H. Kamhawi, NASA Technology Demonstration Mission 12.5-kW Hall Effect Rocket with Magnetic Demonstration Units W. Huang, H. Kamhawi, T. Haag, NASA Glenn Speed Imaging Glenn Research Center, Cleveland, OH; J. Polk, R. Hofer, Jet Propulsion Laboratory, California Institute Shielding Thruster R. Conversano, R. Hofer, M. Sekerak, Jet Propulsion Research Center, Cleveland, OH W. Huang, H. Kamhawi, T. Haag, NASA Glenn J. Snyder, R. Hofer, Jet Propulsion Laboratory, of Technology, Pasadena, CA; H. Kamhawi, NASA Glenn H. Kamhawi, T. Haag, W. Huang, J. Yim, D. Herman, Laboratory, California Institute of Technology, Pasadena, Research Center, Cleveland, OH California Institute of Technology, Pasadena, CA; Research Center, Cleveland, OH NASA Glenn Research Center, Cleveland, OH; P. CA; H. Kamhawi, P. Peterson, NASA Glenn Research et al. Peterson, Vantage Partners, LLC, Cleveland, OH; et al. Center, Cleveland, OH Tuesday, 26 July 2016 99-EP-16 Low Power Hall Thruster Development 250 B Chaired by: D. OH, Jet Propulsion Laboratory and J. SZABO, Busek Co., Inc. 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4830 AIAA-2016-4831 AIAA-2016-4832 AIAA-2016-4833 AIAA-2016-4834 High Throughput 600 Watt Hall Effect Characterization and Qualification of the Design and characterization of a 200W Performance Evaluation of the T-40 Low- Experimental Study of the Effects of the Thruster for Space Exploration CAM200 Low Power Hall Thruster Hall thruster in “magnetic shielding’’ Power Hall Current Thruster Cathode Position and the Electrical Circuit J. Szabo, B. Pote, R. Tedrake, S. Paintal, L. Byrne, D. Lev, R. Eytan, D. Katz-Franco, L. Appel, Rafael, configuration J. Frieman, T. Liu, M. Walker, Georgia Institute of Configuration on the Operation of HK40 Hall V. Hruby, Busek Company, Inc., Natick, MA; et al. Haifa, Israel L. Grimaud, J. Vaudolon, S. Mazouffre, National Technology, Atlanta, GA; J. Makela, A. Mathers, P. Thruster and BUSTLab Hollow Cathode Center for Scientific Research (CNRS), Orléans, Peterson, Aerojet Rocketdyne, Redmond, WA N. Turan, U. Kokal, M. Celik, Bogazici University, France; C. Boniface, French Space Agency (CNES), Istanbul, Turkey; H. Kurt, Istanbul Medeniyet University, Toulouse, France Istanbul, Turkey Tuesday, 26 July 2016 100-EP-17 LaB6 Hollow Cathodes 250 C Chaired by: R. SPEKTOR, The Aerospace Corporation and B. JACKSON 1500 hrs 1530 hrs 1600 hrs AIAA-2016-4835 AIAA-2016-4836 AIAA-2016-4838 Lanthanum Hexaboride Hollow Cathode Wear Test Demonstration of a Technique Laser-induced Fluorescence Measurements

Performance and Wear Testing for the to Mitigate Keeper Erosion in a High- of Energetic Ions in a 100-A LaB6 Hollow Asteroid Redirect Mission Hall Thruster Current LaB 6 Hollow Cathode Cathode D. Goebel, J. Polk, Jet Propulsion Laboratory, A. Ho, B. Jorns, I. Mikellides, D. Goebel, A. Lopez C. Dodson, University of California, Los Angeles, Los California Institute of Technology, Pasadena, CA Ortega, Jet Propulsion Laboratory, California Angeles, CA; D. Perez-Grande, Charles III University Institute of Technology, Pasadena, CA of Madrid, Madrid, Spain; B. Jorns, D. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; R. Wirz, University of California, Los Angeles, Los Angeles, CA Tuesday, 26 July 2016 101-EP-18 Sputtering & Erosion Physics 250 D Chaired by: K. POLZIN, NASA Marshall Space Flight Center and N. MACDONALD, AFRL 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4839 AIAA-2016-4840 AIAA-2016-4841 AIAA-2016-4842 AIAA-2016-4843 Mechanisms for Pole Piece Erosion in a Surface Geometry Effects on Secondary Multi-diagnostic Measurements of Sputter Search for Anomalous Ridge Growth A Parametric Computational Study of 6-kW Magnetically-Shielded Hall Thruster Electron Emission Via Monte Carlo Yield of Molybdenum under Argon Plasma during Stressed Material Plasma Erosion Boron Transport in Hall Thrusters B. Jorns, Jet Propulsion Laboratory, California Modeling Bombardment A. Schinder, M. Walker, J. Rimoli, Georgia Institute B. Smith, I. Boyd, University of Michigan, Ann Institute of Technology, Pasadena, CA; C. Dodson, C. Huerta, R. Wirz, University of California, Los G. Li, T. Matlock, University of California, Los of Technology, Atlanta, GA Arbor, Ann Arbor, MI University of California, Los Angeles, Los Angeles, Angeles, Los Angeles, CA Angeles, Los Angeles, CA; D. Goebel, Jet Propulsion CA; J. Anderson, D. Goebel, R. Hofer, M. Sekerak, Laboratory, California Institute of Technology, Jet Propulsion Laboratory, California Institute of Pasadena, CA; R. Wirz, University of California, Los 59 Technology, Pasadena, CA; et al. Angeles, Los Angeles, CA Tuesday, 26 July 2016 102-EP-19 Pulsed Plasma Thruster 250 E Chaired by: R. KAWASHIMA, The University of Tokyo and J. CARDIN, VACCO 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4844 AIAA-2016-4845 AIAA-2016-4846 AIAA-2016-4847 AIAA-2016-4848 Research and Development of a High-Power Observation of Late-Time Ablation in Electric Pulsed Plasma Thruster Development Characteristics of a Coaxial Pulsed Plasma Development and Testing of Electric Electrothermal Pulsed Plasma Thruster System Solid Propellant Pulsed Microthrusters Using A Novel HAN-Based Green Electric Thruster Using Liquid Propellant Propulsion Systems at TU Dresden onboard Osaka Institute of Technology 2nd M. Glascock, J. Rovey, Missouri University of Science Monopropellant K. Miyagi, Kyushu Institute of Technology, D. Bock, F. Nürmberger, C. Drobny, P. Laufer, M. PROITERES Nano-Satellite and Technology, Rolla, MO; S. Williams, J. Thrasher, J. Thrasher, S. Williams, P. Takahashi, J. Sousa, Kitakyushu, Japan; A. Kakami, University of Tajmar, Technical University of Dresden, Dresden, K. Kanaoka, H. Tahara, Osaka Institute of Technology, Digital Solid State Propulsion, Inc., Reno, NV Digital Solid State Propulsion, Inc., Reno, NV Miyazaki, Miyazaki, Japan; T. Tachibana, Kyushu Germany Osaka, Japan Institute of Technology, Kitakyushu, Japan Tuesday, 26 July 2016 103-F360-4 Nuclear Power for Distant Solar System Destinations Ballroom F 1500 - 1730 hrs Moderator: Lee Mason, Chief, Thermal Energy Conversions Branch, NASA Glenn Research Center Panelists: Rex Geveden John Casani Leonard Dudzinski Susan Voss Patrick McClure Chief Operating Officer NASA Jet Propulsion Laboratory (ret.) Science Mission Directorate President Los Alamos National Laboratory BWX Technologies, Inc. NASA Global Nuclear Network Analysis, LLC Tuesday, 26 July 2016 104-GTE-10 Advanced Materials and Technology for Gas Turbine Engines 251 A Chaired by: M. RICKLICK, Embry Riddle Aeronautical University 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4849 AIAA-2016-4850 AIAA-2016-4851 AIAA-2016-4852 AIAA-2016-4853 Integrated High Temperature Sensors for The influences of foreign object damage Preliminary Investigation of an Oblique Effect of Semi-Molten Particulate on Fatigue Analysis of a Cylindrical Turbine Advanced Propulsion Materials on the high cycle fatigue behavior of Jet Impingement Cooling on a CMC Rough Tailored Thermal Barrier Coatings for Gas Disk with Integrated Heat Pipes K. Wong, S. Sahoo, M. McFarland, Acree titanium alloy TC4 Surface Turbine Engine S. Eisenmann, T. Schmidt, V. Gümmer, Technical Technologies, Inc., Concord, CA Z. Zhao, X. Xu, W. Chen, T. Wu, Nanjing University K. Krishna, M. Ricklick, Embry-Riddle Aeronautical A. Ghoshal, M. Murugan, M. Walock, B. Barnett, University of Munich, Garching, Germany; A. of Aeronautics and Astronautics, Nanjing, China University, Daytona Beach, FL M. Pepi, S. Jeffrey, Army Research Laboratory, Hupfer, University of the German Federal Armed Aberdeen Proving Ground, MD; et al. Forces, Neubiberg, Germany Tuesday, 26 July 2016 105-GTE-11 Turbines III 251 B Chaired by: M. ATTIA, Embry-Riddle Aeronautical University 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-4854 AIAA-2016-4855 AIAA-2016-4856 AIAA-2016-4857 A Comparative Evaluation of Heat Transfer Investigation of Pressure Drop and Heat Experimental and Computational Flow Analysis of a Coupled Micro- and Triple- and Friction Behavior of a Square Channel Transfer Behavior of a Square Channel Analyses of a Single Jet Impinging on a Impingement Cooling Configuration in the with Sharp and Rounded 45° Ribs at with 45° Angle Turbulators on One and Flat Plate C3X Vane Wide Range of Reynolds Numbers Using Two Wall Configuration M. Benson, M. Cremins, A. Lachance, C. Snow, B. C. Rossman, M. Ricklick, Embry-Riddle Aeronautical Experimental and Numerical Computation C. Vergos, L. Ahmed, P. Tran, T. Buchanan, E. Van Poppel, C. Verhulst, U.S. Military Academy, University, Daytona Beach, FL L. Ahmed, P. Tran, C. Vergos, E. Fernandez, University Fernandez, J. Kapat, University of Central Florida, West Point, NY; et al. of Central Florida, Orlando, FL; L. Mears, J. Rodriguez, Orlando, FL Siemens, Orlando, FL; et al. Tuesday, 26 July 2016 60 106-GTE-12 Gas Turbine Engine Testing Techniques 251 C Chaired by: R. HANCOCK, AFRL/RQT and J. KELLY, AEDC 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-4858 AIAA-2016-4859 AIAA-2016-4860 AIAA-2016-4861 Approximation of Engine Casing An Inverse Heat Conduction Problem Experimental and Numerical Analysis of Investigation on the dynamic response of Temperature Constraints for Casing applied to the Rotor Casing of a Transonic a Piezo Driven Fluidic Device for Active aero-engine structures due to fan blade out Mounted Electronics Turbine Flow Control event through subscale testing J. Kratz, D. Culley, J. Chapman, NASA Glenn B. Hilbert, S. Morris, University of Notre Dame, M. Mair, L. Chen, J. Turner, M. Bacic, P. Ireland, L. Liu, W. Chen, Z. Zhao, G. Luo, Nanjing University of Research Center, Cleveland, OH Notre Dame, IN University of Oxford, Oxford, United Kingdom Aeronautics and Astronautics, Nanjing, China Tuesday, 26 July 2016 107-HR-5 Development and Evaluation of Novel O/F Formulations and Combinations 253 AB Chaired by: T. SHIMADA, Japan Aerospace Exploration Agency and S. WHITMORE, Utah State University 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-4862 AIAA-2016-4863 AIAA-2016-4864 AIAA-2016-4865 Combustion Characteristics of Gas Hybrid Development of a 75 mm Hybrid Rocket Design and performance evaluation of AP and Boron combustion characteristics

Rocket using H2O as Oxidizer-Effect of Motor to Test Metal Additives hybrid rocket using 95 wt.% H2O2 in Staged Hybrid Rocket Engine Mg-Al Particle Sizes- C. Maharaj, K. Veale, J. Pitot, C. Bemont, S. Kang, D. Lee, E. Lee, S. Kwon, Korea Advanced D. Lee, C. Lee, Konkuk University, Seoul, South Y. Sato, T. Kuwahara, Self, Funabashi, Japan University of KwaZulu-Natal, Durban, South Africa Institute of Science and Technology, Daejeon, Korea South Korea Tuesday, 26 July 2016 108-HR-6 Combustion Stability, Motor Performance, and Related Issues 255 B Chaired by: B. MADHANABHARATAM, Aerospace Consultant and A. KARABEYOGLU, Space Propulsion Group Inc. 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4866 AIAA-2016-4867 AIAA-2016-4868 AIAA-2016-4869 AIAA-2016-4870 AIAA-2016-4871 Nondestructive Mapping of Hybrid Rocket Effects of Radiation Heating on Additively A Fundamental Study on the Hybrid Pressure Oscillation and Combustion Computed Tomography Characterization Measuring Time-Varying Fuel Regression Fuel Grains Printed Hybrid Fuel Grain O/F Shift Rocket Clustering for the Rocket Sled in Shear Layer of Hybrid Rocket Post of a Porous Hybrid Motor Grain with Rates with Image Processing in a Hybrid A. Costantino, California Institute of Technology, S. Whitmore, S. Merkley, Utah State University, Propulsion System Chamber Added Contrast Agent Rocket Motor Pasadena, CA; P. Narsai, B. Cantwell, Stanford Logan, UT D. Nakata, K. Yasuda, S. Horio, K. Higashino, Y. Moon, C. Lee, Konkuk University, Seoul, South J. Buckley, M. Denny, G. Nelson, University of P. Narsai, K. Venkataraman, K. Stober, B. Cantwell, University, Stanford, CA Muroran Institute of Technology, Muroran, Japan Korea Alabama, Huntsville, Huntsville, AL Stanford University, Stanford, CA Tuesday, 26 July 2016 109-HSABP-7 Numerical Analysis of High-Speed Air-Breathing Propulsion and Their Integration 254 C Chaired by: H. HUO, General Electric 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-4872 AIAA-2016-4873 AIAA-2016-4874 AIAA-2016-4875 Aerothermodynamics cycle model for new Ignition Test of Solid Fuel Ramjet Combustor Numerical Analysis of a Dual-mode The Effects of Air Vitiation on the hypersonic propulsion: Rocket Ignited W. Jung, S. Baek, Korea Advanced Institute of Science Scramjet Engine VS a Rocket-Based Supersonic Turbulent Channel flow using Supersonic Combustion Ram Jet and Technology, Daejeon, South Korea; J. Park, T. Combined-Cycle Engine Direct Numerical Simulation J. Barros, Federal University of Minas Gerais, Belo Kwon, Defense Research and Development Institute, L. Shi, Northwestern Polytechnical University, X. Chen, Zhejiang University, Hangzhou, China; X. Horizonte, Brazil; M. Gabaldo, Technology Consultation Kyung Ju, South Korea; S. Kwon, Korea Advanced Xi’an, China Li, Chinese Academy of Sciences, Beijing, China; Services srl, Villafranca di Verona, Italy; M. Guerra, Institute of Science and Technology, Daejeon, South H. Dou, Zhejiang University, Hangzhou, China Lumar Metals, Santana do Paraíso, Brazil Korea Tuesday, 26 July 2016 110-HSABP-8 Pulse Detonation Physics, and/or Combined Cycle with Other Utility to High-Speed Propulsion 255 A Chaired by: K. KAILASANATH, Naval Research Laboratory and A. HAYASHI, Aoyama Gakuin University 61 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4876 AIAA-2016-4877 AIAA-2016-4878 AIAA-2016-4879 AIAA-2016-4880 Preliminary Parametric Analysis of a Mach Disk Pressure Measurement Technique Analytical Model of Shock Dynamics in Criteria for rotating detonation to pass Adaptive simulations of viscous and inviscid Rotating Detonation Engine by Analytic within Rotating Detonation Engine Pulse Detonation Engine Nozzles obstacles near the inlet detonations in supersonic combustible Methods J. Codoni, K. Cho, Air Force Research Laboratory, Wright- J. Peace, F. Lu, University of Texas, Arlington, Y. Wang, Southwest University of Science and mixture using a hot jet initiation A. Mizener, F. Lu, University of Texas, Arlington, Patterson AFB, OH; J. Hoke, Innovative Scientific Solutions, Arlington, TX Technology, Mianyang, China X. Cai, J. Liang, Hypersonic Propulsion Center, Arlington, TX Inc., Dayton, OH; F. Schauer, Air Force Research Laboratory, Changsha, China Wright-Patterson AFB, OH Tuesday, 26 July 2016 111-ITAR-2 Launch Vehicles I (CAT-IV) 151 DE Chaired by: C. BROPHY, Naval Postgraduate School and S. CLAFLIN, Aerojet Rocketdyne 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2016-4881 AIAA-2016-4882 AIAA-2016-4883 AIAA-2016-4884 Development and Testing 100 lbf Non- Development of 10 inch Diameter HTP CubeSat Propulsion Module Schlieren Visualizations within a Rotating Launch Vehicle Low Shock Stage Toxic Monopropellant Thruster. Consider Titanium Rolling Metal Diaphragm Tank A. Vazquez, N. Love, A. Choudhuri, University of Detonation Engine Separation System for ITAR session. for Green Propellant Texas, El Paso, El Paso, TX J. Codoni, Innovative Scientific Solutions, Inc., Dayton, H. Golden, S. Sawhill, Systima Technologies, Inc., A. Shchetkovskiy, T. McKechnie, Plasma Processes, H. Conomos, J. Yager, J. Moore, R. Goddard, T. OH; K. Cho, Air Force Research Laboratory, Wright- Kirkland, WA LLC, Huntsville, AL; S. Mustaikis, Dynetics, Inc., Salzler, J. Fetes, Moog, Niagara Falls, NY; et al. Patterson AFB, OH; J. Hoke, Innovative Scientific Huntsville, AL Solutions, Inc., Dayton, OH; F. Schauer, Air Force Research Laboratory, Wright-Patterson AFB, OH Tuesday, 26 July 2016 113-NFF-4 Nuclear Thermal Propulsion: Engines and Missions 251 E Chaired by: C. JOYNER, Aerojet Rocketdyne and S. BOROWSKI, NASA Glenn Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4885 AIAA-2016-4886 AIAA-2016-4887 AIAA-2016-4888 Oral Presentation AIAA-2016-4889 Nuclear Thermal Rocket - Arc Jet Three-Dimensional Analysis of a Hydrogen Comparing Low Enriched Fuel to Highly Engine Design Attributes Relative to HEU Realizing Commercial Missions to Atmospheric Mining in the Outer Solar Integrated System Model Containment Process For Nuclear Thermal Enriched Fuel for use in Nuclear Thermal and LEU Core Approaches for a Small the Moon Using Conventional and System: Outer Planet Orbital Transfer and B. Taylor, W. Emrich, NASA Marshall Space Flight Engine Ground Testing Propulsion Systems Thrust NTP Bipropellant Nuclear Thermal Rocket Lander Analyses Center, Huntsville, AL T. Wang, E. Stewart, F. Canabal, NASA Marshall V. Patel, Center for Space Nuclear Research, Idaho C. Joyner, D. Levack, T. Jennings, Aerojet (NTR) Propulsion B. Palaszewski, NASA Glenn Research Center, Space Flight Center, Huntsville, AL Falls, ID; M. Eades, Ohio State University, Columbus, Rocketdyne, West Palm Beach, FL; M. Eades, Ohio S. Borowski, S. Ryan, L. Burke, NASA Glenn Cleveland, OH OH; P. Venneri, Korea Advanced Institute of Science and State University, Columbus, OH; V. Patel, Center Research Center, Cleveland, OH; D. McCurdy, J. Technology, Daejeon, South Korea; C. Joyner, Aerojet for Space Nuclear Research, Idaho Falls, ID Fittje, Vantage Partners, LLC, Brook Park, OH; C. Rocketdyne, West Palm Beach, FL Joyner, Aerojet Rocketdyne, West Palm Beach, FL Tuesday, 26 July 2016 114-PC-9 Advanced Combustor Concepts 255 C Chaired by: R. HAUSEN, Honywell and E. LYNCH, Aerojet Rocketdyne 1500 hrs 1530 hrs 1600 hrs AIAA-2016-4890 AIAA-2016-4891 AIAA-2016-4892 Alternative Bio-Derived JP-8 Class Fuel A Comparison of Three Second-Generation Flame-Flow interaction under Distributed and JP-8 Fuel: Flame Tube Combustor Test Swirl-Venturi Lean Direct Injection Combustor Combustion Conditions Results Compared using a GE TAPS Injector Concepts A. Khalil, A. Gupta, University of Maryland, College Configuration K. Tacina, NASA Glenn Research Center, Cleveland, Park, College Park, MD Y. Hicks, S. Tedder, R. Anderson, NASA Glenn OH; P. Lee, Woodward FST, Inc., Zeeland, MI; H. Research Center, Cleveland, OH Mongia, Purdue University, West Lafayette, IN; B. Dam, Woodward FST, Inc., Zeeland, MI; Z. He, D. Podboy, NASA Glenn Research Center, Cleveland, OH 62 Tuesday, 26 July 2016 115-PC-10 Combustion Instability 255 D Chaired by: O. KNAB, Airbus Defense & Spaceafran Launcher and T. DROZDA, NASA Langley Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-4893 AIAA-2016-4894 AIAA-2016-4895 AIAA-2016-4896 AIAA-2016-4897 AIAA-2016-4898 Review of experimental test cases for Generations of unstable combustion in a Towards Numerical Prediction of Jet Fuels Exploration of POD-Galerkin Techniques Variation of Dominant Instability Mode Numerical Study of the Influence of the modelling high frequency combustion non-premixed GCH4/GOX rocket injector Sensitivity of Flame Dynamics in a Swirl for Developing Combustion Response with Fuel Configuration in an Inverted Opening Ratio on the Damping Capacity instability (Invited paper) H. Terashima, Hokkaido University, Sapporo, Spray Combustion System Functions Coaxial Injector of the Injector J. Hardi, S. Gröning, S. Webster, S. Beinke, D. Japan; Y. Daimon, Japan Aerospace Exploration R. Ranjan, A. Panchal, G. Hannebique, S. Menon, C. Huang, W. Anderson, C. Merkle, Purdue A. Dasari, M. Gamba, University of Michigan, Ann H. An, W. Nie, S. Feng, Equipment Academy, Suslov, M. Oschwald, German Aerospace Center Agency (JAXA), Tsukuba, Japan Georgia Institute of Technology, Atlanta, GA University, West Lafayette, IN Arbor, Ann Arbor, MI Beijing, China (DLR), Lampoldshausen, Germany Tuesday, 26 July 2016 116-PC-11 Combustion Diagnostics 255 E Chaired by: C. KIRCHBERGER, German Aerospace Center (DLR) and S. SILVESTRI 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4899 AIAA-2016-4900 AIAA-2016-4901 AIAA-2016-4902 AIAA-2016-4903 Lean Blowout with a High Pressure Well Fuel Distribution and Gas Temperature Planar Laser Absorption Spectroscopy for Assessment of flames heat radiation Hydrocarbon Fuel Thermal Performance Stirred Reactor Measurements in a Nonuniformly-Fueled the Resolution of Simultaneous, Spatially- prediction Modeling based on Systematic J. Gross, D. Shouse, C. Neuroth, Air Force Research Bluff-Body Flame Distinct Absorption Paths A. da Silva, M. Venturini, N. Caetano, Federal Measurement and Comprehensive Laboratory, Wright-Patterson AFB, OH B. Huelskamp, L. Goss, Innovative Scientific Solutions, J. France, M. Gamba, University of Michigan, Ann University of Santa Maria, Santa Maria, Brazil Chromatographic Analysis Inc., Dayton, OH; D. Richardson, Spectral Energies, Arbor, Ann Arbor, MI M. Billingsley, Air Force Research Laboratory, LLC, Dayton, OH; G. Wang, General Electric Company, Edwards AFB, CA; N. Keim, B. Hill-Lam, Johns Niskayuna, NY; A. Lynch, V. Belovich, Air Force Hopkins University, Columbia, MD; R. Synovec, Research Laboratory, Wright-Patterson AFB, OH; et al. University of Washington, Seattle, Seattle, WA Tuesday, 26 July 2016 117-SATS-1 Small Satellites I 251 F Chaired by: J. STRAUB, University of North Dakota 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-4904 AIAA-2016-4905 AIAA-2016-4906 AIAA-2016-4907 Design Optimization and Performance Complete EM System Development for Development of Propulsion System with Development of a MEMS Pyrotechnic Evaluation of A Monopropellant Satellite Busek’s 1U CubeSat Green Propulsion Bi-propellants Based on Green Propellant Thruster for Micro Propulsion Applications Thruster Module for Microsatellite H. Shukla, Birla Institute of Technology, C. Nichith , P. P, S. Sharan, S. Mani, V. Sanal M. Tsay, J. Zwahlen, D. Lafko, C. Feng, M. Robin, J. Matsushima, M. Kaku, M. Banno, H. Sahara, Ranchi, India; R. Singh Nandan, P. Shukla, Kumar, Kumaraguru College of Technology, Busek Company, Inc., Natick, MA Tokyo Metropolitan University, Tokyo, Japan; Y. V. Kumar N, Vikram Sarabhai Space Centre, Coimbatore, India Araki, Astroscale Japan, Inc., Tokyo, Japan Thiruvananthapuram, India; M. Varma, Birla Institute of Technology, Ranchi, India Tuesday, 26 July 2016 118-SR-4 Advanced Solid Rockets (Nozzles, Cases, and Controllable) 254 A Chaired by: H. CIEZKI, DLR - German Aerospace Center and K. NAUMANN, Bayern-Chemie GmbH 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-4909 AIAA-2016-4910 AIAA-2016-4911 AIAA-2016-4908 Brazilian Thrust Vector Control System Design of Environmental Friendly Chevron Investigation of Vortex Valve Controlled Electrolytic Combustion in the Polyvinyl Development: Status and Trends Nozzles for Lower Stage Rockets Variable Thrust SRM Alcohol + Hydroxyl Ammonium Nitrate T. Wekerle, Technological Institute of Aeronautics R. Sathyaprabha , S. Vigneshwaran , R. Manishaa, X. Yu, Northwestern Polytechnical University, Solid Propellant (ITA), São José dos Campos, Brazil; E. Barbosa, S. Ajith, S. Mani, V. Sanal Kumar, Kumaraguru Xi’an, China; Y. Wang, China Aerospace Science J. Baird, J. Lang, A. Hiatt, R. Frederick, University C. Batagini, Aeronautics and Space Institute (IAE), College of Technology, Coimbatore, India and Technology Corporation (CASC), Shanghai, of Alabama, Huntsville, Huntsville, AL São José dos Campos, Brazil; L. Loures da Costa, China; X. Wei, Northwestern Polytechnical L. Trabasso, Technological Institute of Aeronautics University, Xi’an, China (ITA), São José dos Campos, Brazil

63 Tuesday, 26 July 2016 119-TM-4 Heat Transfer and Transport Modeling and Analysis I 151 AB Chaired by: J. MEHTA, Belcan AETD 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-4912 AIAA-2016-4913 AIAA-2016-4914 AIAA-2016-4915 AIAA-2016-4916 Effect of internal partitions on thermal Thermal analysis of RBCC engine at Numerical Study of Decreasing the Enhanced ECS/Generator Models in an Predictions of the Air Flow Regimes and comfort and IAQ level provided by underfloor ejector, ramjet and scramjet modes Spread of Sarin (GB) in an Air-conditioned Integrated Air Vehicle Platform Thermal Comfort in Islamic Worship:Religious air distribution system in a typical Office T. Jing, G. He, B. Lin, W. Li, F. Qin, Y. Liu, Aircraft Cabin A. Donovan, R. Roberts, M. Wolff, Wright State Rituals of Hajar and her infant Ishmael Space Northwestern Polytechnical University, Xi’an, China A. Farag, Egyptian Armed Forces, Cairo, Egypt; E. University, Dayton, OH between Al-Safa and Al-Marwah. A. AbouZeid, E. Khalil, Cairo University, Cairo, Egypt Khalil, M. Hassan, Cairo University, Cairo, Egypt A. ElDegwy, E. Khalil, Cairo University, Cairo, Egypt Tuesday, 26 July 2016 120-PLNRY-5 Formula for Success and Longevity in the Aerospace Business Ballroom A-D 1800 - 1930 hrs Moderators: Bonnie Prado Pino, Graduate Student, School of Aeronautics and Astronautics, Purdue University Guillermo Jaramillo Pizarro, Graduate Student, School of Aeronautics and Astronautics, Purdue University Panelists: David Bowles Duane Cuttrell Julie Van Kleeck Rickey Shyne Director Director, Operations Engineering and Technical Vice President, Advanced Space and Launch Business Unit Director, Research and Engineering NASA Langley Research Center Operations,Lockheed Martin Corporation Aerojet Rocketdyne NASA Glenn Research Center Tuesday, 26 July 2016 121-NFF-5 Future Flight Propulsion Systems I 150 G Chaired by: B. PALASZEWSKI, NASA Glenn Research Center and B. CASSENTI, University of Connecticut 1900 hrs 1930 hrs 2000 hrs AIAA-2016-4917 AIAA-2016-4918 AIAA-2016-4919 WWAT: Warp Drives, Wormholes, Destination Universe: Some Thoughts on Testing the Possibility of Weight Changes Antigravity and Time Travel Faster-Than Light (FTL) Travel in Highly-Polarized Electrets B. Cassenti, University of Connecticut, Storrs, G. Bennett, Metaspace Enterprises, Boise, ID M. Tajmar, T. Schreiber, Dresden University of Storrs, CT Technology, Dresden, Germany Wednesday Wednesday, 27 July 2016 122-PLNRY-6 The Impact of Additive Manufacturing on the Design Process Ballroom A-D 0800 - 0900 hrs Elizabeth Robertson Team Lead, Liquid Engine Systems Branch Marshall Space Flight Center Wednesday, 27 July 2016 123-NW-6 Networking Coffee Break Exhibit Hall C 0845 - 0930 hrs Wednesday, 27 July 2016 124-ADP-2 Seal Material Advancements and Advanced Seal Technology 255 E Chaired by: P. DUNLAP, NASA Glenn Research Center and N. SARAWATE, GE Global Research and B. DEV, GE Global Research Center 64 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4920 AIAA-2016-4921 AIAA-2016-4922 AIAA-2016-4923 Film Riding Pressure Activated Leaf Seal Non-Contacting Finger Seals Static Characterization of thermoplastic- An Electrically Conductive Elastomer Seal Proof of Concept Performance Test Results at Ambient and elastomeric seals at high pressures and for Spacecraft T. Kirk, A. Bowsher, P. Crudgington, Cross High Temperatures temperatures C. Daniels, H. Oravec, J. Mather, University of Manufacturing Company, Ltd., Devizes, United M. Proctor, NASA Glenn Research Center, B. Dev, J. Wang, O. Samudrala, Q. Xuele, General Akron, Akron, OH; P. Dunlap, NASA Glenn Research Kingdom; C. Grondahl, J. Dudley, CMG Tech, LLC, Cleveland, OH Electric Company, Niskayuna, NY Center, Cleveland, OH Rexford, NY; A. Pawlak, Cross Manufacturing Company, Ltd., Devizes, United Kingdom Wednesday, 27 July 2016 125-APC-3 Advanced Propulsion Concepts II 251 C Chaired by: A. REISZ, Reisz Engineers and J. ROBINSON, Retired f/Boeing 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4924 AIAA-2016-4925 AIAA-2016-4926 Experimental Investigation on Rotating Laser powered air breathing blast wave Feasibility Study of a DRBCC-Powered Detonation Engine with Different Mixing propulsion guided by donut mode beam Single-Stage-To-Orbit Launch Vehicle Distance K. Mori, Nagoya University, Nagoya, Japan F. Zhang, H. Zhang, B. Wang, Tsinghua University, X. Han, S. Zhang, J. Wang, Peking University, Beijing, China Beijing, China Wednesday, 27 July 2016 126-APS-4 Space and Aircraft Power Generation, Processing and Performance 151 G Chaired by: J. HAINES, Retired - formerly ESA/ESTEC and G. LAM, Lockheed Martin Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4927 AIAA-2016-4928 AIAA-2016-4929 AIAA-2016-4930 Solar Probe Plus (SPP) Power System Proposal and Development of a High Improving Solar Arrays for LILT and High Further Analyses of the NASA Glenn Electronics Voltage Variable Frequency Alternating Radiation Environments Research Center Solar Cell and A. Baisden, D. Frankford, Johns Hopkins University Current Power System for Hybrid Electric J. McNatt, NASA Glenn Research Center, Cleveland, Photovoltaic Materials Experiment Applied Physics Laboratory, Laurel, MD Aircraft OH; C. Taylor, NASA Langley Research Center, onboard the International Space Station D. Sadey, L. Taylor, R. Beach, NASA Glenn Hampton, VA; M. Piszczor, NASA Glenn Research M. Myers, M. Piszczor, M. Krasowski, N. Prokop, Research Center, Cleveland, OH Center, Cleveland, OH D. Wolford, J. McNatt, NASA Glenn Research Center, Cleveland, OH Wednesday, 27 July 2016 127-ECS-3 Energetic Systems and Component Developments 254 C Chaired by: B. SMITH, Pacific Scientific Energetic Materials Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation AIAA-2016-4931 AIAA-2016-4932 AIAA-2016-4933 2016 CAD/PAD Technology Roadmap A Review on Relationship between Thermal-Mechanical Characterization of Detonating Cord Assembly (DCA) Second Update Reliability and Lot Acceptance Sample Bridgewires and Surrounding Materials Source Project Overview J. Burchett, T. Blachowski, A. Woods, Naval Size for ECS Utilizing Thermal Transient Testing T. Blachowski, Naval Surface Warfare Center, Surface Warfare Center, Indian Head, MD L. Yang, Self, La Canada Flintridge, CA C. Moore, J. Morgan, L. Roberson, NASA Kennedy Indian Head, MD; G. Teowee, Austin Star Space Center, Cape Canaveral, FL; J. Carney, Detonator, Brownsville, TX University of Florida, Gainesville, Gainesville, FL; J. Whittaker, a.i. solutions, Inc., Cape Canaveral, FL; J. Glass, Vencore, Cape Canaveral, FL

65 Wednesday, 27 July 2016 128-EDU-3 Propulsion Education III 253 AB Chaired by: R. FREDERICK, University of Alabama @ Huntsville and M. HITT, The University of Alabama in Huntsville 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4934 AIAA-2016-4936 AIAA-2016-4937 AIAA-2016-4935 Measurement of Micro-Thruster A parametric model for thrust chamber ITA Candy rocket motor design and solid Laboratory Experimentation and Basic Performance Characteristics Using a preliminary design propellant manufacture challenges Research Investigating Electric Solid Magnetically Levitating Thrust Stand R. Rezende, V. de Castro Perez, A. Pimenta, D. Bontorin, S. Gomes, L. Rocco, R. Jachura, J. Propellant Electrolytic Characteristics A. Patel, D. Lineberry, J. Cassibry, R. Frederick, Technological Institute of Aeronautics (ITA), São Rocco, K. Iha, Technological Institute of Aeronautics A. Hiatt, R. Frederick, University of Alabama, University of Alabama, Huntsville, Huntsville, AL José dos Campos, Brazil (ITA), São José dos Campos, Brazil Huntsville, Huntsville, AL Wednesday, 27 July 2016 129-EP-20 Plasma Plume Modeling 250 A Chaired by: K. KOMURASAKI, The University of Tokyo and J. LITTLE, Princeton University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4938 AIAA-2016-4939 AIAA-2016-4940 AIAA-2016-4941 On the Validity of the Boltzmann SM/MURF: Current Capabilities and Numerical Simulations of Unsteady Carbon Back Sputter Modeling for Hall Assumption for Electrons in Plasma Plume Verification as a Replacement of AFRL Plasma Plume Flows Thruster Testing Modeling Plume Simulation Tool COLISEUM C. Cai, Michigan Technological University, J. Gilland, G. Williams, J. Burt, Ohio Aerospace Y. Hu, J. Wang, University of Southern California, S. Araki, R. Martin, ERC, Inc., Edwards AFB, CA; Houghton, MI Institute, Brook Park, OH; J. Yim, NASA Glenn Los Angeles, CA D. Bilyeu, J. Koo, Air Force Research Laboratory, Research Center, Cleveland, OH Edwards AFB, CA Wednesday, 27 July 2016 130-EP-21 Mid Power Hall Thruster Development 250 B Chaired by: S. MAZOUFFRE, ICARE-CNRS and P. CAGAS, Virginia Tech 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4942 AIAA-2016-4943 AIAA-2016-4944 Laboratory Testing of Hall Thrusters for Integration Tests of the 4 kW-class High Research and Development of low- All-electric Propulsion Satellite and Deep Voltage Hall Accelerator Power Processing Power and High-Power Three-Types Hall Space Explorers Unit with the HiVHAc and the SPT-140 Hall Thrusters at Osaka Institute of Technology I. Funaki, Japan Aerospace Exploration Agency Effect Thrusters T. Kakuma, H. Tahara, Osaka Institute of (JAXA), Sagamihara, Japan; S. Iihara, IHI Corporation, H. Kamhawi, L. Pinero, T. Haag, W. Huang, D. Technology, Osaka, Japan Tomioka, Japan; S. Cho, K. Kubota, Japan Aerospace Ahern, NASA Glenn Research Center, Cleveland, Exploration Agency (JAXA), Chofu, Japan; H. OH; R. Liang, Space Systems Loral, Palo Alto, Watanabe, Tokyo Metropolitan University, Hino, Japan; CA; et al. K. Fuchigami, IHI Corporation, Isogo, Japan; et al. Wednesday, 27 July 2016 131-EP-22 Cathodes & Neutralizers 250 C Chaired by: D. GOEBEL, Jet Propulsion Laboratory and A. LOPEZ ORTEGA, Jet Propulsion Laboratory 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4945 AIAA-2016-4946 AIAA-2016-4947 Experimental Performance 3D Particle Simulation for Electron Performance of a Hall Thruster Operating Characterization of a Novel Direct Current Extraction Mechanisms of a Miniature with a Radio Frequency Plasma Cathode Cold Cathode Neutralizer for Electric Microwave Discharge Neutralizer H. Watanabe, M. Ichimura, H. Takegahara, Tokyo Thruster Applications K. Hiramoto, Yokohama National University, Metropolitan University, Hino, Japan A. Gurciullo, A. Knoll, University of Surrey, Yokohama, Japan; Y. Nakagawa, H. Koizumi, K. Guildford, United Kingdom; P. Bianco, Airbus, Komurasaki, University of Tokyo, Tokyo, Japan; Y. Portsmouth, United Kingdom Takao, Yokohama National University, Yokohama, 66 Japan Wednesday, 27 July 2016 132-EP-23 Advanced EP Concepts 250 D Chaired by: H. WHITE, NASA-Johnson Space Center and J. KOLBECK 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4948 AIAA-2016-4949 AIAA-2016-4950 AIAA-2016-4951 Antenna Coupling and Thrust Experimental Performance Analysis of Advances in Duration Testing of the Preliminary Investigation of an External Measurements in a Direct Wave-Drive the BUSTLab Microwave Electrothermal VASIMR® VX-200SS™ System Discharge Plasma Thruster Thruster Thruster J. Squire, M. Carter, F. Chang Diaz, L. Dean, M. B. Karadag, Graduate University for Advanced M. Feldman, E. Choueiri, Princeton University, M. Yildiz, Turkish Air Force Academy, Istanbul, Giambusso, Ad Astra Rocket Company, Webster, Studies, Sagamihara, Japan; S. Cho, Japan Aerospace Princeton, NJ Turkey; M. Celik, Bogazici University, Istanbul, TX; J. Castro, Ad Astra Rocket Company, Liberia, Exploration Agency (JAXA), Sagamihara, Japan; Y. Turkey Costa Rica; et al. Oshio, Tokyo University of Agriculture and Technology, Fuchu, Japan; Y. Hamada, University of Tokyo, Hongo, Japan; I. Funaki, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; K. Komurasaki, University of Tokyo, Hongo, Japan Wednesday, 27 July 2016 133-F360-5 Rising Leaders in Aerospace -- Forum 360 Combined Session Ballroom F 0930 - 1200 hrs This session will begin with Rex Geveden, Chief Operating Officer, BWX Technologies, Inc., speaking about “Seven Career Hacks for Professional Success.”.After that, there will be a round table of persons talking about their own and colleagues’ professional success. Mr. Geveden will moderate and coordinate the question and answer period. Wednesday, 27 July 2016 134-FFP-2 Fossil-Fuel Power Technologies II 150 DE Chaired by: A. CHOUDHURI, University of Texas at El Paso and B. KHANDELWAL, The University of Sheffield 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4952 AIAA-2016-4953 AIAA-2016-4954 AIAA-2016-4955 AIAA-2016-4956 Reactor Parameters Effects on Hydrogen The Effect of the Fuel Change from Petroleum Bio-Ethanol Fuel Mixtures Theoretical Emission Characteristics of Laminar Experimental Investigation of the Laminar Production from Hydrogen Sulfide Kerosene to HEFA Alternative Jet Fuel on Influence on Aviation Reciprocating Prevaporized Petroleum and Biodiesel Flame Speeds of GTL Fuel Blends A. El-Melih, University of Maryland, College Park, the Emission of an RQL Type Gas Turbine Engines Flames at near Stoichiometric Conditions S. Samim, S. Ahmed, Qatar University, Doha, College Park, MD; S. Ibrahim, A. Al Shoaibi, Combustor J. Vega, J. Leyton, L. Monico, University of San A. Balakrishnan, R. Parthasarathy, S. Gollahalli, Qatar Petroleum Institute, Abu Dhabi, United Arab K. Okai, University of Tokyo, Tokyo, Japan; H. Fujiwara, Buenaventura, Bogota, Colombia University of Oklahoma, Norman, Norman, OK Emirates; A. Gupta, University of Maryland, M. Makida, K. Shimodaira, H. Yamada, Japan College Park, College Park, MD Aerospace Exploration Agency (JAXA), Tokyo, Japan; M. Nakamura, Mitsubishi Group, Nagoya, Japan Wednesday, 27 July 2016 135-GEPC-2/EOA-1 Low Carbon Aviation- Electric Propulsion and Technologies 254 B Chaired by: M. BRADLEY, Boeing Commercial Airplanes and T. ABDEL-SALAM, East Carolina University and E. GARCIA, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Air Force Research Laboratory More Exploration of Enabling Technologies and Carbon Emissions Impact of Hybrid Electric Enabling Technology Development for Review of Hybrid and Turbo Electric Electric Aircraft Technologies Preliminary Design of High Efficiency, Propulsion and Secondary Power Systems Hybrid and Distributed Electric Aircraft Propulsion for Large Transport Aircraft J. Nairus, AFRL Aerospace Systems Directorate, High Specific Power Drive for Hybrid C. Lents, United Technologies Research Center, Propulsion J. Felder, NASA Glenn Research Center, Cleveland, Ohio, OH Propulsion Systems Hartford, CT M. Armstrong, Rolls Royce, Cherry Point, NC OH F. Luo, Ohio State University, Columbus, OH Wednesday, 27 July 2016 136-GTE-14 Compressors III 251 A 67 Chaired by: J. CSANK, NASA Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4957 AIAA-2016-4958 AIAA-2016-4959 AIAA-2016-4960 Application of Symmetry Property for Analytical Modeling of Helium Compressor Three-objective Optimization for the Design Optical Characterization of a Cross flow Transient Response Analysis of Mistuned Performance of Mechanical Component Using Evolutionary fan for Distributed Propulsion Bladed Disks D. Wilson, P. Balaji, University of Texas, Arlington, Numerical Simulation Approach G. Raush, Technical University of Catalonia, J. Yao, W. Zhu, N. Hu, Chongqing University, Arlington, TX N. Nagaiah, J. Kapat, University of Central Florida, Tarrassa, Spain; L. Villafane, Stanford University, Chongqing, China; J. Wang, Beihang University, Orlando, FL; C. Geiger, Universal Orlando Resort, Stanford, CA; G. Paniagua, Purdue University, West Beijing, China Orlando, FL Lafayette, IN Wednesday, 27 July 2016 137-GTE-15/ABPSI-6/HSABP-11 Undergraduate Engine Design Competition 251 B 0930 - 1200 hrs The AIAA Foundation and the Technical Committees GTE, ABPSI, and HSABP, have worked together to sponsor a design competition. Undergraduate students from universities around the world were asked to prepare a design report to respond to a Request for Proposal (RFP). This RFP asked students to design a candidate engine for a next-generation trainer.

All of the reports have been reviewed and scored by technical experts, and this session features the top three proposal winners, who have been invited to the AIAA Propulsion and Energy Forum 2016 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 1st-3rd place ranking. The final rankings will be announced at the conclusion of the session. Wednesday, 27 July 2016 138-HR-7 Design and Development of Novel Hybrid Rocket Motor Concepts II 255 B Chaired by: S. COOGAN, Southwest Research Institute and Y. CHEN, National Space Organization Taiwan 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4961 AIAA-2016-4962 AIAA-2016-4963 AIAA-2016-4964 AIAA-2016-4965 Design of a Hybrid CubeSat Orbit Insertion A Hybrid Mars Ascent Vehicle Concept for Experiments of an Ejector-jet using a Wax- Static Burning Tests on a Bread Board Design of a Lab-Scale Hybrid Rocket Test Motor Low Temperature Storage and Operation based Fuel Hybrid Rocket Motor Model of Altering-intensity Swirling- Stand E. Jens, A. Karp, B. Nakazono, D. Eldred, M. A. Karp, B. Nakazono, J. Benito Manrique, R. Y. Nakada, I. Nakagawa, Tokai University, Oxidizer-Flow-Type Hybrid Rocket Engine J. Thomas, J. Stahl, G. Morrow, E. Petersen, Texas DeVost, D. Vaughan, Jet Propulsion Laboratory, Shotwell, D. Vaughan, Jet Propulsion Laboratory, Hiratsuka, Japan K. Ozawa, T. Usuki, G. Mishima, K. Kitagawa, A&M University, College Station, TX California Institute of Technology, Pasadena, CA California Institute of Technology, Pasadena, CA; Institute of Space and Astronautical Science, G. Story, NASA Marshall Space Flight Center, Sagamihara, Japan; M. Yamashita, M. Mizuchi, Huntsville, AL Kyushu University, Fukuoka, Japan; et al. Wednesday, 27 July 2016 139-HSABP-9 Experimental and Numerical Analysis of High Speed Propulsion Systems 255 A Chaired by: T. O’BRIEN, Raytheon Missiles Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4966 AIAA-2016-4967 AIAA-2016-4968 AIAA-2016-4969 Design and Experiments of a Continuous Theoretical and Experimental Preliminary Experiments on Transpiration Flow Field Characteristics of Non- Rotating Detonation Engine: a Spinning Consideration of the Continuous Rotating Cooling in Ramjets and Scramjets Axisymmetric High Subsonic Jets Wave Generator and Modulated Fuel/ Detonation Engine F. Strauss, C. Manfletti, D. Freudenmann, J. Witte, G. Valentich, R. Kumar, Florida State University, Oxidizer Mixing M. Kurosaka, C. Knowlen, J. Boening, University of S. Schlechtriem, German Aerospace Center (DLR), Tallahassee, FL; D. Cuppoletti, M. Alphonso, C. J. Boening, J. Heath, T. Byrd, J. Koch, A. Mattick, Washington, Seattle, Seattle, WA Hardthausen, Germany Harris, Northrop Grumman Corporation, Redondo R. Breidenthal, University of Washington, Seattle, Beach, CA Seattle, WA; et al. Wednesday, 27 July 2016 68 140-ITAR-3 Explosives and Energetic Materials (CAT-V) 151 DE Chaired by: J. CASTRO, Aerojet Rocketdyne and C. BROPHY, Naval Postgraduate School 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4970 AIAA-2016-4971 AIAA-2016-4972 AIAA-2016-4973 AIAA-2016-4974 High Energy Radiation Effects on Microgravity Flight Testing of Multi-Pulse Design and Development of Gaseous Design and Fabrication of an Ultra-Low- Pyrooshock Dynamic Loading Impacts on Spacecraft Service Valve O-ring Leak Small Solid Motors (Consider for ITAR Hydrogen and Oxygen Tank Pressurization Cost Variant of the Bantam Liquid Rocket Thermoelectric Module Assemblies and Rates Session) Assemblies for the Space Launch System Engine Family for Application to the DARPA Bi-Couples in Multi-Mission Radioisotope G. Coll, R. Gigliuto, G. Webster, M. Espinosa, NASA S. Williams, P. Takahashi, J. Sousa, Digital Solid Core Stage Experimental Spaceplane (XS-1) and Other Thermoelectric Generators Goddard Space Flight Center, Greenbelt, MD State Propulsion, Inc., Reno, NV; A. Nicholas, H. Pitts, M. Ettleman, The Boeing Company, Huntsville, Future Low-Cost Launch Applications T. Hendricks, D. Neff, N. Keyawa, B. Nesmith, P. Naval Research Laboratory, Washington, D.C. AL; P. Park, V. Cardoso, R. Kelly, Y. Gerasimov, Valcor J. Castro, W. Sack, J. Littles, Aerojet Rocketdyne, West Bahrami, A. Derkevorkian, Jet Propulsion Laboratory, Engineering Corporation, Springfield, NJ Palm Beach, FL California Institute of Technology, Pasadena, CA; et al. Wednesday, 27 July 2016 141-LP-12 Rocket Engine Components 251 D Chaired by: S. CHIANESE, SpaceX and A. DEVEREAUX, Surrey Satellite Technology Ltd (SSTL) 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4975 AIAA-2016-4976 AIAA-2016-4977

Development and Testing of a O 2/CH 4 Characterising the Infrared Signature of a Digital Image Correlation Techniques Torch Igniter for Propulsion Systems Liquid Propellant Engine Plume Applied to Large Scale Rocket Engine L. Sanchez, J. Chaparro, S. Torres, N. Love, A. C. Higgins, QinetiQ, Sevenoaks, United Kingdom; T. Testing Choudhuri, University of Texas, El Paso, El Paso, TX Smithson, Defense Research and Development Canada, P. Gradl, NASA Marshall Space Flight Center, Québec, Canada; I. Coxhill, Moog, Aylesbury, United Huntsville, AL Kingdom; P. Fournier, S. Ringuette, Defense Research and Development Canada, Québec, Canada Wednesday, 27 July 2016 142-LP-13 Propulsion Systems - Design & Test II 251 E Chaired by: D. COOTE, NASA Stennis Space Center and D. GUADAGNOLI, Orbital ATK 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-4978 AIAA-2016-4979 AIAA-2016-4980 AIAA-2016-4981 Numerical Studies of Dynamic Response Experimental Study of Liquid Injector Monopropellant Hydrazine Thrusters— Effects of Water Hammer on Propulsion for an Oxidizer Injector to Detonation Elements for Use in Rotating Detonation Bringing Updated Designs to Flight Systems Wave Engines V. Yarnot, M. Dawson, O. Morgan, Aerojet B. Brindle, J. Gilbert, J. Moore, G. Risha, Penn K. Mikoshiba, S. Sardeshmukh, D. Stechmann, S. W. Anderson, D. Lim, Purdue University, West Rocketdyne, Redmond, WA State Altoona, Altoona, PA Heister, Purdue University, West Lafayette, IN Lafayette, IN; M. Washington, U.S. Air Force Academy, Colorado Springs, CO; S. Heister, Purdue University, West Lafayette, IN Wednesday, 27 July 2016 143-LP-14 Turbomachinery 251 F Chaired by: B. MARCU and S. FORDE, Aerojet Rocketdyne 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4982 AIAA-2016-4983 AIAA-2016-4984 AIAA-2016-4985 AIAA-2016-4986 Unique Characteristics of Imbalanced The Design and Analysis of Low Solidity Turbopump Design and Development for High Suction Performance Pumps Characterization of Rotating Cavitation in a Torque Force of a Partial Admission Vaned Diffusers for Increased Turbopump the Virgin Galactic NewtonThree Engine with Large Inlet Blade Angles and an Four Bladed Inducer Turbine for 50% Partiality Throttling Capability System Integrated Stability Control Device C. Lettieri, Delft University of Technology, Delft, The K. Yada, S. Kawasaski, M. Uchiumi, Japan S. Sargent, Barber-Nichols, Inc., Arvada, CO S. Sargent, J. Noall, Barber-Nichols, Inc., Arvada, R. Lundgreen, Ohio State University, Columbus, Netherlands; Z. Spakovszky, Massachusetts Institute of Aerospace Exploration Agency (JAXA), Kakuda, CO; M. Becker, S. Macklin, Virgin Galactic, Long OH; K. Oliphant, Concepts NREC, White River Technology, Cambridge, MA; D. Jackson, The Aerospace Japan; H. Kato, K. Funazaki, Iwate University, Beach, CA Junction, VT; D. Maynes, S. Gorrell, Brigham Corporation, Los Angeles, CA; V. Wang, Massachusetts Morioka, Japan Young University, Provo, UT Institute of Technology, Cambridge, MA Wednesday, 27 July 2016 69 144-NFF-6 Future Flight Propulsion Systems II 150 G Chaired by: B. CASSENTI, University of Connecticut and M. TAJMAR, Dresden University of Technology 0930 hrs 1000 hrs 1030 hrs AIAA-2016-4987 AIAA-2016-4988 AIAA-2016-4989 Anomalous Electromagnetically Induced First Measurements of a 0.6 Gigawatt Propulsion Estimates for High Energy Propulsion Effects on Self-contained Superconducting Gravity-Impulse- Lunar Missions Using Future Propellants “RAMA” Devices Generator B. Palaszewski, NASA Glenn Research Center, H. Brito, R. De Alessandro, M. Brito, Aeronautical I. Lörincz, M. Tajmar, Dresden University of Cleveland, OH; G. Bennett, Metaspace Enterprises, University Institute, Cordoba, Argentina Technology, Dresden, Germany Boise, ID Wednesday, 27 July 2016 145-PC-12 Green Propulsion 255 C Chaired by: C. CADOU, University of Maryland and H. CIEZKI, DLR - German Aerospace Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4990 AIAA-2016-4991 AIAA-2016-4992 AIAA-2016-4993 AIAA-2016-4994

Comparison of single and multi-injector Investigation of Green Hypergolic Characterization of a Multi-Injector GOX/ Studies on Flame Behaviors of GCH4/ A 1D Multiphase Mixture Model for the GOC/CH4 combustion chambers Propellants for Hybrid Rockets CH4 Combustion Chamber GO2 Coaxial Jets in a Model Combustor at Design of Catalysts for Monopropellant M. Celano, S. Silvestri, C. Bauer, N. Perakis, K. Stober, A. Thomas, B. Evans, B. Cantwell, S. Silvestri, M. Celano, G. Schlieben, O. Haidn, Elevated Pressure Thrusters G. Schlieben, O. Haidn, Technical University of Stanford University, Stanford, CA Technical University of Munich, Munich, Germany H. Kim, S. Choi, T. Kim, O. Kwon, Sungkyunkwan C. Boffa, O. Haidn, Technical University of Munich, Munich, Munich, Germany University, Suwon, South Korea Munich, Germany Wednesday, 27 July 2016 146-PC-13 Single Injector Test Case Modeling 255 D Chaired by: O. HAIDN, Technische Universität München and Y. DAIMON, Japan Aerospace Exploration Agency 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-4995 AIAA-2016-4996 AIAA-2016-4997 AIAA-2016-4998 AIAA-2016-4999 Numerical Investigation of Flow and Numerical Investigation of Flow and Numerical Investigation of Flow and Numerical Modeling of Flow and Combustion On the Effects of Chemical Kinetics and

Combustion in a Single Element GCH4/ Combustion in a Single-Element GCH4/GOX Combustion in a Single-Element GCH4/GOX in a Single-Element GCH4/GOX Rocket Thermal Conditions on the Flow and Flame Gox Rocket Combustor Rocket Combustor: Chemistry Modeling and Rocket Combustor: A comparative LES study Combustor: Aspects of Turbulence Modeling Features in a Single-Element GCH4/GOX C. Roth, O. Haidn, A. Chemnitz, T. Sattelmayer, Turbulence-Combustion Interaction H. Müller, J. Zips, M. Pfitzner, University of the German A. Chemnitz, T. Sattelmayer, C. Roth, O. Haidn, Rocket Combustor Technical University of Munich, Munich, Germany; D. Maestro, B. Cuenot, CERFACS, Toulouse, France; A. Federal Armed Forces, Munich, Germany; D. Maestro, Technical University of Munich, Munich, Germany; Y. R. Ranjan, A. Panchal, S. Menon, Georgia Institute G. Frank, University of the German Federal Armed Chemnitz, T. Sattelmayer, C. Roth, O. Haidn, Technical B. Cuenot, CERFACS, Toulouse, France; S. Menon, Daimon, Japan Aerospace Exploration Agency (JAXA), of Technology, Atlanta, GA Forces, Munich, Germany; H. Müller, Technical University of Munich, Munich, Germany; et al. Georgia Institute of Technology, Atlanta, GA; et al. Tsukuba, Japan; R. Keller, University of Stuttgart, University of Munich, Munich, Germany; et al. Stuttgart, Germany; et al. Wednesday, 27 July 2016 147-SR-5 Solid Rocket Developments Past and Present 254 A Chaired by: M. RANDALL, Aerojet-Rocketdyne East and D. POE, Aerojet-Rocketdyne 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-5000 AIAA-2016-5001 AIAA-2016-5002 AIAA-2016-5003 Observation in Ballistic Evaluation Motor Multidisciplinary Optimization of a Solid Effect of Ageing on Mechanical Properties “Thermal-Mechanical” Coupled Model Static Firing: Graphite Nozzle Cracking Propellant Sectional Geometry for Internal of Composite Solid Propellants Based on Porous Media Characteristics of T. K, A. Rao, R. Jakka, Defence Research and Ballistic and Structural Strength Criteria H. Naseem, H. Murthy, P. Ramakrishna, Indian EPDM insulator Char Layer Development Organisation, Jagdalpur, India C. Tola, M. Nikbay, Istanbul Technical University, Institute of Technology Madras, Chennai, India Y. Liu, J. Pei, Northwestern Polytechnical Istanbul, Turkey University, Xi’an, China Wednesday, 27 July 2016 148-TM-5 Heat Transfer and Transport Modeling and Analysis II 151 AB 70 Chaired by: C. TARAU, Advanced Cooling Technologies and E. KHALIL, Cairo University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-5004 AIAA-2016-5005 AIAA-2016-5006 AIAA-2016-5007 Air Cycle Machine Transient Modeling with CFD Investigation of Smoke Management Lumped Parameter Modelling and Testing of Oxidizer Composition Effects on NOx Exergy Analysis In Underground Tunnels a Free Piston Stirling Engine Heat Exchanger Emissions from Swirl Burner M. Bracey, S. Nuzum, R. Roberts, M. Wolff, E. Khalil, W. El-Sayed Sweida, O. Huzzayyin, Cairo Using Laminated Woven Copper Wire Mesh as E. Khalil, A. Ahmed, M. Hassan, H. Kayed, Cairo Wright State University, Dayton, OH; J. Zumberge, University, Cairo, Egypt Heat Transfer Areas University, Cairo, Egypt Air Force Research Laboratory, Wright-Patterson F. Senda, South African Nuclear Energy Corporation, AFB, OH Pelindaba, South Africa; P. Senda, R. Dobson, Stellenbosch University, Stellenbosch, South Africa Wednesday, 27 July 2016 149-PLNRY-7 The Strategic Challenges and Opportunities in the Power and Propulsion Markets Ballroom A-D 1330 - 1500 hrs Pierre Chao Founding Partner Renaissance Strategic Advisors Wednesday, 27 July 2016 150-ABPSI-5 Propulsion Systems Integration 255 F Chaired by: D. CROWE, Air Force Institute of Technology and A. PRAKASH, University of Teesside 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-5008 AIAA-2016-5009 AIAA-2016-5010 AIAA-2016-5011 Computational and Experimental Parametrical Optimization of a three- Development of an Engine-Integrated Fuel Development And Analysis of a Group 1 Evaluation of a Complex Inlet Swirl dimensional Dump Diffuser with Cell Concept Demonstrator: Phase I Efforts UAV Series Hybrid Power System with Two Pattern Generation System Aerodynamically-shaped Flame Tube for L. Pratt, S. Vannoy, C. Cadou, University of Engine Options D. Sanders, C. Nessler, W. Copenhaver, M. List, T. Modern Aircraft Engines Maryland, College Park, College Park, MD M. Hageman, C. Wisniewski, U.S. Air Force Janczewski, Air Force Research Laboratory, Wright- C. Selvakarthick , S. Ajith, H. Nagaraju Doddi, V. Academy, Colorado Springs, CO Patterson AFB, OH Sanal Kumar, Kumaraguru College of Technology, Coimbatore, India; V. Rangaraj, J. Allen, University of Oklahoma, Norman, OK Wednesday, 27 July 2016 151-ECD-3 Stirling Components and Systems 151 AB Chaired by: T. HENDRICKS, NASA-Jet Propulsion Laboratory and L. MASON, NASA Glenn Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-5012 AIAA-2016-5013 AIAA-2016-5014 AIAA-2016-5015 AIAA-2016-5016 AIAA-2016-5017 Fission Surface Power Technology Two-Step Multi-Physics Analysis of an Performance Testing of a High Active Vibration Reduction of the Stirling Engine Performance with Maturing Technologies for Stirling Space Demonstration Test Results Annular Linear Induction Pump for Fission Temperature Linear Alternator for Stirling Advanced Stirling Convertor Optimized Piston and Displacer Power Generation M. Briggs, M. Gibson, S. Geng, NASA Glenn Power Systems Convertors S. Wilson, J. Metscher, N. Schifer, NASA Glenn Waveforms S. Wilson, B. Nowlin, NASA Glenn Research Research Center, Cleveland, OH; J. Sanzi, Vantage S. Geng, T. Reid, NASA Glenn Research Center, J. Metscher, S. Geng, NASA Glenn Research Research Center, Cleveland, OH M. Briggs, NASA Glenn Research Center, Cleveland, Center, Cleveland, OH; M. Dobbs, P. Schmitz, Partners, LLC, Cleveland, OH Cleveland, OH Center, Cleveland, OH OH Vantage Partners, LLC, Brook Park, OH; J. Huth, Converter Source, LLC, Athens, OH Wednesday, 27 July 2016 71 152-ECS-4 Young Professionals and Energetic Components & Systems - An Educational Series Panel Session 254 B 1500 - 1730 hrs Wednesday, 27 July 2016 153-EE-2 Renewable Fuel Generation And Processing 150 G Chaired by: S. DUNCAN, Aerospace Systems Design Laboratory, Georgia Tech and Y. YAVOR, Technion - Israel Ins. of Technology 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-5018 AIAA-2016-5019 AIAA-2016-5020 AIAA-2016-5021 AIAA-2016-5022 AIAA-2016-5023 Optimal Technique for Separation of Dry (CO2) Reformation of Methane using Simultaneous Differential Thermal and Aluminum-Water Reaction Mechanism – The Generalized Onsager Model for a Analysis of High-Speed Rotating Flow in Particle-rich Syngas in Cyclone for Nickel-Barium Catalyst Thermogravimetric Analysis of Chicken Modeling of the Different Reaction Stages Binary Gas Mixture with Swirling Feed 2D Polar (r - θ) Coordinate Efficient Methanation K. Burra, A. Gupta, University of Maryland, College Manure Gasification using Nitrogen and Y. Yavor, Technion--Israel Institute of Technology, S. Pradhan, Indian Institute of Science, Bengaluru, S. Pradhan, Indian Institute of Science, Bengaluru, O. Olalekan, E. Ogedengbe, University of Lagos, Park, College Park, MD Carbon Dioxide Haifa, Israel India India Akoka-Yaba, Nigeria R. Amano, M. Hussaein, University of Wisconsin, Milwaukee, Glendale, WI Wednesday, 27 July 2016 154-EP-24 HERMeS Hall Thruster II 250 A Chaired by: T. MATLOCK and S. GILDEA, AFRL 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-5024 AIAA-2016-5025 AIAA-2016-5026 AIAA-2016-5027 AIAA-2016-5028 Transient Thermal Analysis of the 12.5 kW 2000-hour Wear-Testing of the HERMeS Hollow Cathode Assembly Development NASA’s HERMeS Hall Thruster Electrical Ion Acoustic Turbulence and Ion Energy HERMeS Hall Thruster Thruster for the HERMeS Hall Thruster Configuration Characterization Measurements in the Plume of the HERMeS S. Reilly, M. Sekerak, R. Hofer, Jet Propulsion G. Williams, J. Gilland, Ohio Aerospace Institute, T. Sarver-Verhey, H. Kamhawi, NASA Glenn P. Peterson, H. Kamhawi, W. Huang, G. Williams, Thruster Hollow Cathode Laboratory, California Institute of Technology, Cleveland, OH; P. Peterson, Vantage Partners, Research Center, Cleveland, OH; D. Goebel, J. J. Gilland, J. Yim, NASA Glenn Research Center, N. Yanes, California Institute of Technology, Pasadena, Pasadena, CA LLC, Cleveland, OH; H. Kamhawi, W. Huang, M. Polk, Jet Propulsion Laboratory, California Institute Cleveland, OH; et al. CA; B. Jorns, Jet Propulsion Laboratory, California Swiatek, NASA Glenn Research Center, Cleveland, of Technology, Pasadena, CA; P. Peterson, D. Institute of Technology, Pasadena, CA; A. Friss, OH; et al. Robinson, Vantage Partners, LLC, Brook Park, OH Colorado State University, Fort Collins, CO; J. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; P. Guerrero, J. Austin, California Institute of Technology, Pasadena, CA Wednesday, 27 July 2016 155-EP-25 High Power Hall Thruster & PPU Development 250 B Chaired by: O. DUCHEMIN, Snecma S.A. and R. CONVERSANO, Jet Propulsion Laboratory 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-5029 AIAA-2016-5030 AIAA-2016-5031 AIAA-2016-5032 AIAA-2016-5033 Investigation of Channel Interactions in a Investigation of Channel Interactions in a Performance of a High-Fidelity 4kW-Class Electric Propulsion Electronics Activities in High Input Voltage, Power Processing Unit Nested Hall Thruster Part II: Probes and Nested Hall Thruster Part I: Acceleration Engineering Model PPU and Integration Europe 2016 Performance Demonstration Performance Region Velocimetry with HiVHAc System M. Gollor, ESA, Noordwijk, The Netherlands; E. W. Santiago, K. Bozak, L. Pinero, R. Scheidegger, S. Cusson, E. Dale, A. Gallimore, University of M. Georgin, V. Dhaliwal, A. Gallimore, University of L. Pinero, H. Kamhawi, NASA Glenn Research Bourguignon, Thales Group, Charleroi, Belgium; M. Gonzalez, A. Birchenough, NASA Glenn Michigan, Ann Arbor, Ann Arbor, MI Michigan, Ann Arbor, Ann Arbor, MI Center, Cleveland, OH; V. Shilo, Colorado Power G. Glorieux, Airbus, Elancourt, France; N. Wagner, Research Center, Cleveland, OH; et al. Electronics, Inc., Fort Collins, CO Airbus, Friedrichshafen, Germany; J. Palencia, 72 Crisa, Tres Cantos, Spain; P. Galantini, Selex ES, Nerviano, Italy; et al. Wednesday, 27 July 2016 156-EP-26 Magnetoplasmadynamics and EP Diagnostics 250 C Chaired by: R. LOBBIA, University of Michigan and P. PETERSON, NASA Glenn Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-5034 AIAA-2016-5035 AIAA-2016-5036 AIAA-2016-5037 AIAA-2016-5038 AIAA-2016-5039 Plume and beam properties of miniaturized Kinetic modelling of collisionless electron Measurement of Electron and Neutral Collisionless electron cooling in Foundation of the new laboratory - MIPT Thrust Performance and Cathode low-power cylindrical Hall thruster for micro- cooling on magnetized plasma expansions Atom Density Downstream of an Electric unmagnetized plasma thruster plumes Plasma Propulsion Lab Temperature Evaluation of MW Class satellites S. Correyero Plaza, J. Navarro, E. Ahedo, G. Propulsion M. Merino-Martinez, P. Fajardo, E. Ahedo, Charles A. Skrylev, D. Krivoruhko, O. Gorshkov, Moscow Quasi-Steady MPD Thruster H. Kim, Korea Advanced Institute of Science and Sánchez, Charles III University of Madrid, Leganes, N. Yamamoto, M. Iwamoto, T. Morita, H. III University of Madrid, Leganes, Spain Institute of Physics and Technology, Dolgoprudny, Y. Oshio, Tokyo University of Agriculture and Technology, Daejeon, South Korea; S. Lee, Korea Spain Nakashima, Kyushu University, Kasuga, Japan Russia Technology, Koganei, Japan; S. Tonooka, Graduate Institute of Materials Science, Changwon, South Korea; University for Advanced Studies, Sagamihara, Y. Lim, J. Kim, W. Choe, Korea Advanced Institute of Japan; I. Funaki, Japan Aerospace Exploration Science and Technology, Daejeon, South Korea Agency (JAXA), Sagamihara, Japan Wednesday, 27 July 2016 157-EP-28 Micropropulsion 250 E Chaired by: W. HOSKINS, Aerojet Rocketdyne and M. GLASCOCK 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-5040 AIAA-2016-5041 AIAA-2016-5042 AIAA-2016-5043 AIAA-2016-5044 AIAA-2016-5045 Micropropulsion Based on Vacuum Arc A Vacuum Arc Thruster with Ablatable Preliminary Measurements of an Linear Actuated Micro-Cathode Arc The IFM 350 Nano Thruster - Introducing Lifetime Testing of the mN-FEEP Thruster Physics and Technology: A Review Anode Integrated Prototype of the CubeSat Thruster System very high Δv Capabilities for Nanosats A. Reissner, University of Applied Sciences, Wiener J. Kolbeck, M. Keidar, George Washington J. Kolbeck, J. Lukas, G. Teel, M. Keidar, George Ambipolar Thruster S. Hurley, M. Keidar, George Washington and Cubesats Neustadt, Austria University, Washington, D.C.; A. Anders, Lawrence Washington University, Washington, D.C. T. Collard, J. Sheehan, University of Michigan, Ann University, Washington, D.C. A. Reissner, FOTEC, Wiener Neustadt, Austria Berkeley National Laboratory, Berkeley, CA Arbor, Ann Arbor, MI Wednesday, 27 July 2016 158-GTE-16 Turbines IV 250 F Chaired by: C. PERULLO, Georgia Institute of Technology 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-5046 AIAA-2016-5047 AIAA-2016-5048 AIAA-2016-5049 Determination of Transient Heat Transfer Integrated Turbine Tip Clearance and Gas An Experimental and Numerical Multi-objective optimization method for Rates for a Film Cooled Metal Plate Turbine Engine Simulation Investigation of the Flow Field and Heat high pressure turbine casing based on in a Blowdown Facility using Infrared J. Chapman, Vantage Partners, LLC, Cleveland, Transfer from a Single Impinging Jet with thermal-structural coupling analysis Thermography OH; T. Guo, J. Kratz, J. Litt, NASA Glenn Research Varying Confinement Conditions W. Chen, Z. Zhao, X. Dai, Nanjing University of L. Chen, R. Mathison, Ohio State University, Center, Cleveland, OH J. Hodges, L. Blanchette, H. Zawati, E. Fernandez, Aeronautics and Astronautics, Nanjing, China Columbus, OH University of Central Florida, Orlando, FL; J. Rodriguez, Siemens, Orlando, FL; J. Kapat, University of Central Florida, Orlando, FL Wednesday, 27 July 2016 159-GTE-17 Aerodynamic Flows in Gas Turbine Engines 251 A Chaired by: A. SURYANARAYANAN, FMC Technologies 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-5050 AIAA-2016-5051 AIAA-2016-5052 AIAA-2016-5053 AIAA-2016-5054 Transition and turbulence in a wall- Large eddy simulation of flat plate film Application of the Maximum Lyapunov Experimental Study on Effusion Cooling Application of Crossflow Transition Criteria bounded channel flow at high Mach cooling flow characteristics based on Exponent to Analyze the Effect on the with Tangential Air Inlet to Local Correlation-Based Transition number plasma actuation Flow Separation with Vibration Wall H. Yu, J. Suo, H. Liang, L. Zheng, Northwestern Model S. Pradhan, Indian Institute of Science, Bengaluru, G. Li, J. Yu, F. Chen, L. Li, Y. Song, Harbin Institute W. Jinchun, F. Xin, G. Huang, H. Shuli, Nanjing Polytechnical University, Xi’an, China C. Bode, J. Friedrichs, Technical University of India of Technology, Harbin, China University of Aeronautics and Astronautics, Braunschweig, Braunschweig, Germany; C. Müller, Nanjing, China; Z. Yuanchi, General Electric F. Herbst, Leibniz University, Hannover, Germany Company, Suzhou, China

73 Wednesday, 27 July 2016 160-GTE-18 Gas Turbine Inlets 251 B Chaired by: D. FOUTCH, The Boeing Company 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-5055 AIAA-2016-5056 AIAA-2016-5057 AIAA-2016-5058 AIAA-2016-5059 Numerical investigation on influence of Performance Estimation for Serpentine Fast Uncertainty Quantification in Engine Analysis and Comparison of Inlet Modeling of ice accretion on rotating cone suction in S-shaped inlet to the rear fan- Nozzle Coupled with Aero-engine Nacelle Inlet Design Using a Reduced Distortion Flow Physics at Design and in aero-engine stage performance S. Xiaolin, Z. Wang, L. Zhou, J. Shi, Northwestern Dimensional Polynomial Chaos Approach Near Stall Operating Condition Using L. Zhang, M. Zhang, X. Zhang, Z. Liu, J. Yu, H. Liu, Harbin Institute of Technology, Polytechnical University, Xi’an, China X. Gao, Y. Wang, N. Spotts, N. Xie, S. Roy, A. Proper Orthogonal Decomposition Northwestern Polytechnical University, Xi’an, China Harbin, China; L. Liu, Hangzhou Dianzi University, Prasad, Colorado State University, Fort Collins, CO R. Spencer, S. Gorrell, M. Jones, Brigham Young Hangzhou, China; G. Li, F. Chen, Y. Song, Harbin University, Provo, UT; E. Duque, Intelligent Light, Institute of Technology, Harbin, China Rutherford, NJ Wednesday, 27 July 2016 161-GTE-19 Gas Turbine Engine Modeling 251 C Chaired by: J. TAI, Georgia Institute of Technology 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-5060 AIAA-2016-5061 AIAA-2016-5062 AIAA-2016-5063 AIAA-2016-5064 AIAA-2016-5065 Exergetic, Exergoeconomic and Dynamic Modeling of a Mixed-Flow Design Parameter Identification of the Development and Validation of an NPSS Uncertainty Quantification and Size Estimation and Performance Analysis Exergoenvironmental Analysis of Afterburning Turbofan Using MATLAB/ Air Supply for a Turboshaft Engine Quick- Model of a Small Turbojet Engine Management in Engine Conceptual Design of a New Intercooled and Recuperated Intercooled Gas Turbine Engine Simulink Start System S. Vannoy, C. Cadou, University of Maryland, J. Tai, J. Mines, E. Inclan, S. Zhu, Georgia Institute Aero-engine A. Almutairi, P. Pilidis, Cranfield University, R. Buettner, R. Roberts, M. Wolff, Wright State M. Kerler, C. Schäffer, W. Erhard, V. Gümmer, College Park, College Park, MD of Technology, Atlanta, GA Y. Xu, H. Tang, M. Chen, Beihang University, Cranfield, United Kingdom; N. Al-Mutawa , Kuwait University, Dayton, OH Technical University of Munich, Garching, Germany Beijing, China University, Kuwait, Kuwait Wednesday, 27 July 2016 162-HR-8 Internal Ballistics Modeling II 255 B Chaired by: A. KARP, Jet Propulsion Laboratory and M. KOBALD, DLR-German Aerospace Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-5066 AIAA-2016-5067 AIAA-2016-5068 AIAA-2016-5069 Modeling of Paraffin-Based Fuels in the Pressure-Measurement Based Estimation Development and Testing of Three Generalized Trkalian Flows: Swirling Simulation of Hybrid Rocket Flowfields of Fuel Regression Rate in Hybrid Rockets Alternative Designs for Additively Motion in Rockets with Arbitrary Headwall G. Leccese, D. Bianchi, F. Nasuti, University of C. Carmicino, University of Naples “Federico II”, Manufactured Hybrid Thrusters Injection Rome “La Sapienza”, Rome, Italy Naples, Italy; D. Pastrone, Technical University of S. Whitmore, S. Mathias, Utah State University, O. Cecil, J. Majdalani, Auburn University, Auburn, AL Turin, Turin, Italy Logan, UT Wednesday, 27 July 2016 163-HSABP-10 Experimental Developments in High-speed Air-Breathing Systems 255 A Chaired by: R. MOEHLENKAMP, Aerojet Rocketdyne 1500 hrs 1530 hrs 1600 hrs AIAA-2016-5070 AIAA-2016-5071 AIAA-2016-5072 Control of Shock Wave – Boundary Layer Experimental Investigation of Fuel Cooled Experimental Study on Start/Unstart Interaction Using Nanosecond Dielectric Combustor Behavior of Two Dimensional Mixed Barrier Discharge Plasma Actuators L. Taddeo, N. Gascoin, K. Chetehouna, National Compression Inlet by Cowl Actuation K. Kinefuchi, A. Starikovskiy, R. Miles , Princeton Institute of Applied Sciences (INSA), Bourges, R. Ananthapadmanaban, T. Murganandam, Indian University, Princeton, NJ France; A. Ingenito, F. Gamma, University of Rome Institute of Technology Madras, Chennai, India “La Sapienza”, Rome, Italy; M. Bouchez, MBDA, Bourges, France; et al. Wednesday, 27 July 2016 164-ITAR-4 Launch Vehicles II (CAT-IV) 151 DE Chaired by: N. JOSHI, GE and K. KAILASANATH, Naval Research Laboratory 74 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-5073 AIAA-2016-5074 AIAA-2016-5075 AIAA-2016-5076 AIAA-2016-5077 The Influence of Pore Pressure Modeling Nusselt Number Correlation for Rocket Experimental Investigation of Fine Droplet Engine Inlet Impacts on Mixing, Development and Validation of on Thermal Analysis of Charring Materials Nozzle Analysis Injectors on AF-M315E Microthruster Operability and Performance of Rotating Autonomous Operational Sequences for T. Laker, M. Ewing, Orbital ATK, Promontory, UT B. Losser, M. Ewing, Orbital ATK, Promontory, UT Operation Detonation Wave Combustors the NEXT System R. Grist, C. Knowlen, University of Washington, C. Brophy, A. Chaves, Naval Postgraduate School, R. Thomas, M. Patterson, NASA Glenn Research Seattle, Seattle, WA; G. Shaw, S. Sawhill, Systima Monterey, CA Center, Cleveland, OH Technologies, Inc., Kirkland, WA Wednesday, 27 July 2016 165-LP-15 Injectors 251 D Chaired by: I. LEYVA, AFOSR and S. SCHUMAKER, Air Force Reseach Laboratory 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-5078 AIAA-2016-5079 AIAA-2016-5080 AIAA-2016-5081 Study on Combustion Characteristics of LOX/ Mixing of Supercritical Fluid in Shear Performance Evaluation of Rocket Engine Study on atomization and combustion LNG (methane) Co-axial Type Injector under Coaxial Injector Configuration Combustors using Ethanol/Liquid Oxygen characteristics of LOX/Methane pintle High Pressure Condition S. Sardeshmukh, W. Anderson, Purdue University, Pintle Injector injectors H. Asakawa, IHI Corporation, Tomioka, Japan; H. West Lafayette, IN K. Sakaki, H. Kakudo, S. Nakaya, M. Tsue, F. Xinxin, S. Chibing, National University of Nanri, I. Masuda, Japan Aerospace Exploration Agency University of Tokyo, Tokyo, Japan; R. Kanai, K. Defense Technology, Changsha, China (JAXA), Tsukuba, Japan; R. Shinohara, Y. Ishikawa, H. Suzuki, Interstellar Technologies, Inc., Tokyo, Sakaguchi, IHI Corporation, Tomioka, Japan Japan; et al. Wednesday, 27 July 2016 166-LP-16 Combustion Stability 251 E Chaired by: P. GLOYER, Gloyer-Taylor Laboratory and D. LINEBERRY, UAH Propusion Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-5082 AIAA-2016-5083 AIAA-2016-5084 AIAA-2016-5085 AIAA-2016-5086 AIAA-2016-5087 Dynamic Characteristics of Various Liquid Experimental Investigation of Transverse Large Eddy Simulations of Transverse High Amplitude Acoustic Field Effects on High Frequency Transverse Acoustic Numerical Investigation on Combustion Propulsion Engine Cycles as Relates to Combustion Instabilities in a High Pressure Combustion Instability in a Multi-element Air-Assisted Liquid Jet Forcing of Cryogenic Impinging Jets at Instability in a small MMH/NTO Liquid Pogo Stability Analysis Multi-Element Combustor Injector A. Ficuciello, F. Baillot, J. Blaisot, National Center High Pressure Rocket Engine D. Ransom, Southwest Research Institute, San R. Gejji, Purdue University, West Lafayette, IN; M. Harvazinski, Air Force Research Laboratory, for Scientific Research (CNRS), Saint-Étienne-du- M. Roa, Sierra Lobo, Inc., Edwards AFB, CA; J. Qin, H. Zhang, B. Wang, Tsinghua University, Antonio, TX B. Austin, IN Space, LLC, West Lafayette, IN; W. Edwards AFB, CA; Y. Desai, HyPerComp, Inc., Rouvray, France; C. Richard, University of Rouen, S. Schumaker, D. Talley, Air Force Research Beijing, China Anderson, Purdue University, West Lafayette, IN Westlake Village, CA; D. Talley, V. Sankaran, Air Saint-Étienne-du-Rouvray, France; M. Théron, Laboratory, Edwards AFB, CA Force Research Laboratory, Edwards AFB, CA French Space Agency (CNES), Paris, France Wednesday, 27 July 2016 167-LP-17 Combustors II 251 F Chaired by: A. LEKEUX, CNES and G. COLL, Orbital ATK 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-5088 AIAA-2016-5089 AIAA-2016-5090 AIAA-2016-5091 Material Compatibility of Bio-Ethanol Fuel Designing and Building a Hydrogen Modeling of Fuel Film Cooling Using Development of Hydrogen with Rocket Engine Combustion Chamber Peroxide-Kerosene Rocket Engine Steady State RANS and Unsteady DES PeroxideKerosene 2,500 N Bipropellant Cooling Channels V. Tacussis, Z. Seider, A. Demarest, S. Nyquist, San Approaches Thruster for Long-term Operation by Film N. Azuma, Japan Aerospace Exploration Agency Jose State University, San Jose, CA K. Brown, E. Coy, M. Harvazinski, V. Sankaran, Air Cooling (JAXA), Tsukuba, Japan; D. Ogawa, A. Iijima, Force Research Laboratory, Edwards AFB, CA S. Heo, S. Kwon, S. Jung, Korea Advanced K. Higashino, Muroran Institute of Technology, Institute of Science and Technology, Daejeon, Muroran, Japan; T. Hiraiwa, Japan Aerospace South Korea Exploration Agency (JAXA), Tsukuba, Japan; M. Oguma, National Institute of Advanced Industrial 75 Science and Technology, Tsukuba, Japan Wednesday, 27 July 2016 168-LP-18 Green Propellants III 253 AB Chaired by: T. POURPOINT, Purdue University and J. SAUER, Orbital Technologies Corporation 1500 hrs 1530 hrs 1600 hrs AIAA-2016-5092 AIAA-2016-5093 AIAA-2016-5094 Development and testing of a nitrous- Study on the Thermal Decomposition of Pressure Drop Measurement of Porous

oxide/ethanol bi-propellant rocket engine Bioethanol as a High-Pressure Rocket Materials: Flashback Arrestors for a N2O/ J. Phillip, S. Youngblood, New Mexico Institute Propellant C2H4 Premixed Green Propellant of Mining and Technology, Socorro, NM; M. A. Iijima, D. Nakata, K. Higashino, Muroran L. Werling, S. Müller, A. Hauk, H. Ciezki, S. Grubelich, W. Saul, Sandia National Laboratories, Institute of Technology, Muroran, Japan Schlechtriem, German Aerospace Center (DLR), Albuquerque, NM; M. Hargather, New Mexico Lampoldshausen, Germany Institute of Mining and Technology, Socorro, NM Wednesday, 27 July 2016 169-PC-14 Combustion Modeling 255 C Chaired by: D. MAESTRO and C. ROTH, TU München 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-5095 AIAA-2016-5096 AIAA-2016-5097 AIAA-2016-5098 An Overview of Spray Modeling With Numerical Investigation of Liquid Jet Breakup Computational simulation on the Solid rocket motor burn simulation OpenNCC and its Application to Emissions and Droplet Statistics with Comparison to performance of Scramjet combustor using considering complex 3D propellant grain Predictions of a LDI Combustor at High X-ray Radiography Multi-strut circular shaped injector geometries Pressure L. Bravo, Army Research Laboratory, Aberdeen Proving K. Pandey, G. Choubey, National Institute of G. Mejia, R. Jachura, S. Gomes, L. Rocco, J. Rocco, M. Raju, Vantage Partners, LLC, Brook Park, OH Ground, MD; D. Kim, F. Ham, Cascade Technologies, Technology, Silchar, India K. Iha, Technological Institute of Aeronautics (ITA), Inc., Palo Alto, CA; C. Powell, D. Duke, K. Matusik, São José dos Campos, Brazil Argonne National Laboratory, Argonne, IL; et al. Wednesday, 27 July 2016 170-PC-15 Rotating Detonation Concepts 255 D Chaired by: J. MURPHY, The Aerospace Corporation and C. CADOU, University of Maryland 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-5099 AIAA-2016-5100 AIAA-2016-5101 AIAA-2016-5102 AIAA-2016-5103 High-Pressure Rotating Detonation Engine Experimental Study of Effects of Injector Numerical Simulation towards Numerical Study for Rotating Detonation Experimental Study of Research of Testing and Flameholding Analysis with Configurations on Rotating Detonation Investigating the Factor for Velocity Propagation in a Two-Parallel-Plane Centrifugal-Compressor-Radial-Turbine Hydrogen and Natural Gas Engine Performance Decrease of Detonation Wave in Rotating Combustor Type Rotating Detonation Engine D. Stechmann, S. Heister, S. Sardeshmukh, K. Goto, Y. Kato, K. Ishihara, K. Matsuoka, J. Detonation Engine Chamber Y. Kumazawa, J. Fujii, A. Matsuo, Keio University, C. Ishiyama, K. Miyazaki, S. Nakagami, K. Purdue University, West Lafayette, IN Kasahara, Nagoya University, Nagoya, Japan; A. J. Fujii, Y. Kumazawa, A. Matsuo, Keio University, Yokohama, Japan; S. Nakagami, K. Matsuoka, J. Matsuoka, J. Kasahara, Nagoya University, Matsuo, Keio University, Yokohama, Japan; et al. Yokohama, Japan; S. Nakagami, K. Matsuoka, J. Kasahara, Nagoya University, Nagoya, Japan Chikusa, Japan; A. Matsuo, Keio University, Kasahara, Nagoya University, Nagoya, Japan Hiyoshi, Japan; et al. Wednesday, 27 July 2016 171-PC-16 Combustion Dynamics II 255 E Chaired by: B. CHEHROUDHI, Advanced Technology Consultants and J. LEYLEGIAN, Manhattan College 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-5104 AIAA-2016-5105 AIAA-2016-5106 AIAA-2016-5107 AIAA-2016-5108 Comparative Analysis of Alternative Fuels Numerical Simulation of Interaction Numerical Studies of Detonation Initiation An Experimental Study on the Numerical investigation of the initiation in Detonation Combustion of Detonation with Metal Particles in by Supersonic Projectiles using a High- Deflagration-to-Detonation Transition in and propagation of oblique detonation M. Azami, M. Savill, Cranfield University, Cranfield, Condensed Matter Order Adaptive Cut-cell Method Millimeter Scale Tubes waves in a confined combustion chamber United Kingdom J. Zhang, Florida Institute of Technology, B. Muralidharan, S. Menon, Georgia Institute of J. He, W. Fan, T. Yan, Y. Chi, Northwestern H. Lee, W. Fan, Northwestern Polytechnical Melbourne, FL; T. Jackson, University of Florida, Technology, Atlanta, GA Polytechnical University, Xi’an, China University, Xi’an, China; Q. Xiao, McGill University, Gainesville, Gainesville, FL Montréal, Canada Wednesday, 27 July 2016 172-PP-1 Propulsion and Power Systems of Unmanned Systems 150 DE 76 Chaired by: L. CHEN, Texas A&M University 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-5109 AIAA-2016-5110 AIAA-2016-5111 AIAA-2016-5112 Oral Presentation Energy Management Strategy of Hybrid Influence and efficiency of energy Combustion and Performance Sensitivity The Testing of a Small-Scale Wave Rotor for D-DALUS Cyclogyro Exploratory PEMFC-PV-Battery Propulsion System for harvesting on the process of de-orbiting to Fuel Cetane Number in an Aviation Use as a Modified Brayton-Cycle Engine Propulsion System for UAVs Low Altitude UAVs using bare electrodynamic tether system Diesel Engine M. McClearn, M. Polanka, K. Lapp, Air Force Institute D. Wills, M. Schwaiger, Innovative Aeronautics X. Zhang, L. Liu, G. Xu, Beijing Institute of Q. Xia, K. Xie, X. Liu, Z. Wu, N. Wang, Beijing M. Szedlmayer, C. Kweon, K. Kruger, Army of Technology, Wright-Patterson AFB, OH; M. Technologies GmbH, Linz, Austria Technology, Beijing, China Institute of Technology, Beijing, China Research Laboratory, Aberdeen Proving Ground, Mataczynski, F. Schauer, Air Force Research Laboratory, MD; J. Gibson, R. Armstrong, C. Lindsey, U.S. Wright-Patterson AFB, OH; D. Paxson, NASA Glenn Army AMRDEC, Redstone Aresenal, AL; et al. Research Center, Cleveland, OH Wednesday, 27 July 2016 173-SATS-2 Small Satellites II 254 C Chaired by: J. STRAUB, University of North Dakota 1500 hrs 1530 hrs AIAA-2016-5113 Small Satellites Fusion Panel Application of Technology Readiness Levels to Micro-Propulsion Systems W. Hargus, J. Singleton, Air Force Research Laboratory, Edwards AFB, CA Wednesday, 27 July 2016 174-SR-6 Solid Propellant Developments 254 A Chaired by: B. LEARY, Johns Hopkins University Applied Physics Laboratory and C. ROUSSEAU, Denel (Pty) Ltd. 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-5114 AIAA-2016-5115 AIAA-2016-5116 AIAA-2016-5117 AIAA-2016-5118 AIAA-2016-5119 Effect of Particle Size on Microwave Laboratory-Scale Burning of Composite Stability of filler-binder interface under Combustion Characteristics in the Comparison of Solid Propellant Burning Study on the Thermal Decomposition Seeded Plasma Enhancement of Solid Propellant Using In-Situ Synthesized hygrothermal aging Secondary Combustor of Ducted Rockets Rate Determination Methods from Characteristics of AP/HTPB Composite Composite Propellant Combustion Iron Oxide C. Pereira, Technological Institute of Aeronautics (ITA), -Effects of the Changing Distance Rate of Industrial Point of View Propellant under High Heat Flux S. Barkley, K. Zhu, M. Ballestero, J. Michael, T. A. Demko, C. Dillier, G. Morrow, T. Sammet, Texas São José dos Campos, Brazil; L. Madureira, Aeronautics B Particles- Ö. Atak, B. Ziraman, M. Yumusak, ROKETSAN X. Lyu, X. Liu, X. Pang, P. Wang, Northwestern Sippel, Iowa State University, Ames, IA A&M University, College Station, TX; K. Grossman, and Space Institute (IAE), São José dos Campos, K. Shirotori, T. Kuwahara, Nihon University, Chiba, Missile Industries, Inc., Ankara, Turkey Polytechnical University, Xi’an, China S. Seal, University of Central Florida, Orlando, Brazil; J. Schpector, Federal University of São Carlos, Japan FL; et al. São Carlos, Brazil; L. Villar, Aeronautics and Space Institute (IAE), São José dos Campos, Brazil Wednesday, 27 July 2016 175-TM-6 Nano-Technology for Thermal Management (Panel) 151 G 1500 - 1630 hrs Panelists will discuss the application of nano-technology for aerospace and terrestrial thermal management, with emphasis on challenges and opportunities. Each panel member will also make a short presentation to highlight his/her scope of involvement in nano-technology and view of the future demands for this technology for thermal management.

Panelists: Keunhan (Kay) Park Massood Tabib-Azar Assistant Professor of Mechanical Engineering, Micro/Nanoscale Energy USTAR Professor and Chair of Solid-State/Circuits/MEMS Curricular Transport & Conversion Laboratory Committee, Electrical & Computer Engineering, University of Utah University of Utah Visiting Scholar, EECS, University of California Berkeley (2015-2016)

77 Wednesday, 27 July 2016 176-TM-7 Heat Transfer and Transport Modeling and Analysis III 151 G Chaired by: E. OGEDENGBE, ENERGHX Consulting/University of Lagos 1500 hrs 1630 hrs 1700 hrs 1730 hrs No Presentation AIAA-2016-5120 AIAA-2016-5121 AIAA-2016-5122 Outdoor Air Conditioning: Case Study of Sensitivity Analysis of Upwinding Schemes Air Flow Regimes in Air-Conditioned Open Football Stadium for Three Dimensional Advection-Diffusion Spectators’ Zone of Qatar Stadium M. Ashmawy, E. Khalil, Cairo University, Cairo, Transport Using Control-Volume Based E. Khalil, M. Ashmawy, W. Abdelsameaa, Cairo Egypt Finite Element Method University, Cairo, Egypt K. Olaitan, E. Ogedengbe, University of Lagos, Akoka-Yaba, Nigeria Author/Session Chair Index Ababneh, M., 29-TM-1, 58-TM-2 Ardalic, J., 27-PC-2 Bauer, K., 49-LP-4 Bowsher, A., 124-ADP-2 Castelli, M., 57-SR-2 Abbas, M., 43-GTE-4 Aretskin-Hariton, E., 46-GTE-9 Baurle, R., 81-HSABP-6 Boyd, I., 37-EP-6, 101-EP-18 Castonguay, K., 4-ADP-1 AbdelGhany, E., 97-EE-1 Arias, F., 53-NFF-1 Baydar, E., 32-ABPSI-2 Bozak, K., 155-EP-25 Castro, J., 132-EP-23, 140-ITAR-3 Abdellatif, O., 97-EE-1 Armstrong, M., 135-GEPC-2/EOA-1 Beach, R., 126-APS-4 Bracey, M., 148-TM-5 Caswell, A., 45-GTE-6 Abdel-Salam, T., 75-GEPC-1, 135-GEPC-2/EOA-1 Armstrong, R., 172-PP-1 Bear, P., 17-GTE-1 Bradley, M., 75-GEPC-1, 135-GEPC-2/EOA-1 Catina, J., 4-ADP-1 Abdelsameaa, W., 176-TM-7 Arnold, S., 44-GTE-5 Beard, D., 29-TM-1, 58-TM-2 Brady, K., 45-GTE-6 Cavallini, E., 57-SR-2, 89-SR-3 Aberle, S., 44-GTE-5 Arthur, N., 72-EP-13 Beckel, S., 20-HSABP-1 Brand, A., 46-GTE-9 Cecil, O., 162-HR-8 AbouZeid, A., 119-TM-4 Asakawa, H., 165-LP-15 Becker, M., 143-LP-14 Braun, J., 18-GTE-2, 95-APC-2 Celano, M., 145-PC-12 Acosta, W., 26-PC-1 Ashmawy, M., 176-TM-7 Behbahani, A., 5-AEC-1, 94-AEC-2 Bravo, L., 169-PC-14 Celik, M., 99-EP-16, 132-EP-23 Acosta-Zamora, A., 42-FFP-1 Atak, Ö., 174-SR-6 Behruzi, P., 25-LP-3, 51-LP-6 Breidenthal, R., 139-HSABP-9 Cetegen, B., 82-ITAR-1 Adams, E., 7-APS-1 Attia, M., 44-GTE-5, 45-GTE-6, 105-GTE-11 Beinke, S., 115-PC-10 Briggs, M., 58-TM-2, 151-ECD-3 Chakraborty, I., 43-GTE-4 Ahedo, E., 156-EP-26 Atwell, M., 52-LP-7 Bell, R., 52-LP-7 Brindle, B., 142-LP-13 Chakravarthula, V., 66-ECD-2 Ahern, D., 72-EP-13, 130-EP-21 Aulisio, M., 7-APS-1 Bellenoue, M., 55-PC-4, 56-PC-5 Brito, H., 144-NFF-6 Chandler, F., 59-VS-1 Ahmed, A., 148-TM-5 Austin, B., 112-LP-11, 166-LP-16 Belovich, V., 116-PC-11 Brito, M., 144-NFF-6 Chandoke, A., 94-AEC-2 Ahmed, L., 105-GTE-11 Austin, J., 154-EP-24 Bemish, R., 73-EP-14 Brophy, C., 111-ITAR-2, 140-ITAR-3, 164-ITAR-4 Chang, C., 26-PC-1 Ahmed, S., 134-FFP-2 Axdahl, E., 48-HSABP-4 Bemont, C., 79-HR-4, 107-HR-5 Brown, K., 167-LP-17 Chang Diaz, F., 132-EP-23 Aigner, M., 45-GTE-6, 56-PC-5 Azami, M., 171-PC-16 Benavides, G., 70-EP-11 Bruckner, A., 95-APC-2 Chap, A., 85-NFF-3 Ajibade, F., 36-EDES-2 Azuma, N., 167-LP-17 Benito Manrique, J., 138-HR-7 Bruno, C., 21-HSABP-2 Chaparro, J., 141-LP-12 Ajith, S., 28-SR-1, 83-LP-8, 93-ABPSI-4, 118-SR-4, Bacha, C., 23-LP-1 Bennett, G., 96-APS-3, 121-NFF-5, 144-NFF-6 Buchanan, T., 105-GTE-11 Chapman, J., 10-EDU-1, 106-GTE-12, 158-GTE-16 50-ABPSI-5 Bacic, M., 106-GTE-12 Bennett, R., 96-APS-3 Buckley, J., 108-HR-6 Chato, D., 84-LP-9 Ajmani, K., 87-PC-7 Badhan, A., 42-FFP-1 Benson, M., 76-GTE-7, 105-GTE-11 Budinger, M., 33-AEP-1 Chaves, A., 164-ITAR-4 Akhlaghi, M., 32-ABPSI-2 Bae, D., 26-PC-1 Berdoyes, M., 28-SR-1 Buettner, R., 94-AEC-2, 161-GTE-19 Chedevergne, F., 57-SR-2 Akiki, M., 55-PC-4, 89-SR-3 Bae, S., 26-PC-1 Berens, T., 93-ABPSI-4 Burchett, J., 127-ECS-3 Chehroudhi, B., 54-PC-3, 171-PC-16 Aksu, T., 87-PC-7 Baek, S., 109-HSABP-7 Berg, S., 15-EP-5, 23-LP-1 Burke, L., 113-NFF-4 Chemnitz, A., 146-PC-13

78 Alberts, S., 51-LP-6 Baglini, J., 35-ECS-1 Besnard, E., 49-LP-4 Burra, K., 153-EE-2 Chen, F., 159-GTE-17, 160-GTE-18 Allen, J., 150-ABPSI-5 Bahrami, P., 140-ITAR-3 Beveridge, L., 85-NFF-3 Burt, A., 70-EP-11 Chen, L., 106-GTE-12, 158-GTE-16, 172-PP-1 Allen, M., 23-LP-1 Bai, H., 80-HSABP-5 Bianchi, D., 162-HR-8 Burt, J., 129-EP-20 Chen, M., 161-GTE-19 Almuqati, N., 86-PC-6 Baillot, F., 166-LP-16 Bianco, P., 131-EP-22 Bushman, S., 51-LP-6, 52-LP-7 Chen, T., 59-VS-1 Almutairi, A., 161-GTE-19 Baird, J., 118-SR-4 Billets, S., 7-APS-1 Butler, M., 7-APS-1 Chen, W., 104-GTE-10, 106-GTE-12, 158-GTE-16 Al-Mutawa, N., 161-GTE-19 Baisden, A., 7-APS-1, 126-APS-4 Billingsley, M., 116-PC-11 Byerley, A., 10-EDU-1 Chen, X., 109-HSABP-7 Alon, G., 71-EP-12 Bak, J., 38-EP-7 Bilyeu, D., 129-EP-20 Byrd, T., 139-HSABP-9 Chen, Y., 47-HR-2, 79-HR-4, 138-HR-7 Alotaibi, M., 86-PC-6 Baker, K., 70-EP-11 Bindl, S., 4-ADP-1 Byrne, L., 13-EP-3, 99-EP-16 Cheng, Y., 55-PC-4 Al Otaibi, R., 86-PC-6 Balaji, P., 136-GTE-14 Birchenough, A., 7-APS-1, 155-EP-25 Cabrera, L., 42-FFP-1 Chetehouna, K., 163-HSABP-10 Alphonso, M., 139-HSABP-9 Balakrishnan, A., 134-FFP-2 Blachowski, T., 127-ECS-3 Cadou, C., 145-PC-12, 150-ABPSI-5, 161-GTE-19, Chi, Y., 171-PC-16 Al Shoaibi, A., 134-FFP-2 Ballestero, M., 27-PC-2, 174-SR-6 Blaisot, J., 166-LP-16 170-PC-15 Chianese, S., 141-LP-12 Amano, R., 153-EE-2 Ballinger, I., 25-LP-3 Blanchette, L., 8-ECD-1, 158-GTE-16 Caetano, N., 116-PC-11 Chibing, S., 165-LP-15 Amato, N., 50-LP-5 Bambauer, M., 56-PC-5 Bock, D., 102-EP-19 Cagas, P., 37-EP-6, 130-EP-21 Chicatelli, A., 46-GTE-9 An, H., 115-PC-10 Banno, M., 117-SATS-1 Bode, C., 159-GTE-17 Cai, C., 129-EP-20 Cho, K., 110-HSABP-8, 111-ITAR-2 Ananthapadmanaban, R., 163-HSABP-10 Banuti, D., 88-PC-8 Bodnya, I., 97-EE-1 Cai, X., 110-HSABP-8 Cho, S., 37-EP-6, 39-EP-8, 69-EP-10, 130-EP-21, Anders, A., 157-EP-28 Barari, G., 54-PC-3 Bodruzzaman, M., 94-AEC-2 Canabal, F., 113-NFF-4 132-EP-23 Anderson, J., 15-EP-5, 101-EP-18 Barato, F., 78-HR-3 Boening, J., 139-HSABP-9 Cantwell, B., 19-HR-1, 79-HR-4, 108-HR-6, 145-PC-12 Choe, W., 38-EP-7, 156-EP-26 Anderson, P., 34-APS-2 Barber, T., 24-LP-2 Boffa, C., 145-PC-12 Cao, S., 54-PC-3 Choi, M., 29-TM-1, 58-TM-2, 175-TM-6 Anderson, R., 114-PC-9 Barbosa, E., 118-SR-4 Bolotin, G., 96-APS-3 Cardiff, E., 40-EP-9 Choi, S., 145-PC-12 Anderson, W., 26-PC-1, 29-TM-1, 55-PC-4, 58-TM-2, Barklay, C., 96-APS-3 Boniface, C., 99-EP-16 Cardin, J., 102-EP-19 Chou, T., 47-HR-2 115-PC-10, 142-LP-13, 165-LP-15, 166-LP-16 Barkley, S., 27-PC-2, 174-SR-6 Bontempo, J., 7-APS-1 Cardoso, V., 140-ITAR-3 Choubey, G., 169-PC-14 Andersson, N., 50-LP-5 Barnes, J., 65-AEP-2 Bontorin, D., 128-EDU-3 Carlotti, S., 19-HR-1 Choudhuri, A., 42-FFP-1, 68-EDU-2, 111-ITAR-2, Andrus, I., 82-ITAR-1 Barnett, B., 104-GTE-10 Boots, D., 93-ABPSI-4 Carmicino, C., 162-HR-8 134-FFP-2, 141-LP-12 Anusonti-Inthra, P., 44-GTE-5 Barraud, G., 33-AEP-1 Borowski, S., 113-NFF-4 Carney, J., 127-ECS-3 Choueiri, E., 11-EP-1, 12-EP-2, 132-EP-23 Appel, L., 71-EP-12, 99-EP-16 Barros, J., 109-HSABP-7 Bouchez, M., 163-HSABP-10 Carter, M., 132-EP-23 Chowdhury, A., 42-FFP-1 Arakawa, T., 80-HSABP-5 Basidh, A., 18-GTE-2 Bourguignon, E., 155-EP-25 Casalis, G., 57-SR-2 Chuck, C., 3-ABPSI-1, 33-AEP-1, 65-AEP-2 Araki, S., 129-EP-20 Batagini, C., 118-SR-4 Boust, B., 55-PC-4, 56-PC-5 Cassenti, B., 121-NFF-5, 144-NFF-6 Chung, T., 96-APS-3 Araki, Y., 117-SATS-1 Bauer, C., 54-PC-3, 56-PC-5, 145-PC-12 Bouyges, M., 57-SR-2 Cassibry, J., 53-NFF-1, 128-EDU-3 Ciezki, H., 49-LP-4, 118-SR-4, 145-PC-12, 168-LP-18 Author/Session Chair Index Cirillo, F., 25-LP-3 David, W., 96-APS-3 Dunlap, P., 124-ADP-2 Fleeman, E., 10-EDU-1 Gibson, M., 151-ECD-3 Cisneros, J., 93-ABPSI-4 Dawson, M., 142-LP-13 Duque, E., 160-GTE-18 Flynn, J., 84-LP-9 Gigliuto, R., 140-ITAR-3 Claflin, S., 19-HR-1, 78-HR-3, 111-ITAR-2 De Alessandro, R., 144-NFF-6 Eades, M., 113-NFF-4 Forde, S., 83-LP-8, 143-LP-14 Gilbert, J., 142-LP-13 Clarke, S., 33-AEP-1 de Almeida, L., 28-SR-1 Edamoto, M., 53-NFF-1 Fosse, J., 33-AEP-1 Gilbert, N., 18-GTE-2 Clayman, L., 11-EP-1 Dean, L., 132-EP-23 Ediger, J., 33-AEP-1 Fouquet, N., 33-AEP-1 Gildea, S., 154-EP-24 Coban, K., 43-GTE-4 De Angelo, B., 29-TM-1 Eisenmann, S., 104-GTE-10 Fournier, P., 141-LP-12 Gilland, J., 129-EP-20, 154-EP-24 Coburn, V., 54-PC-3 Deans, M., 23-LP-1 Elzahaby, A., 90-TM-3 Foutch, D., 46-GTE-9, 160-GTE-18 Ginn, S., 33-AEP-1 Codoni, J., 110-HSABP-8, 111-ITAR-2 de Araujo, R., 28-SR-1 ElDegwy, A., 119-TM-4 France, J., 116-PC-11 Giri, G., 77-GTE-8 Cohen, K., 94-AEC-2 de Castro Perez, V., 128-EDU-3 Eldred, D., 138-HR-7 Frank, G., 146-PC-13 Glascock, M., 102-EP-19, 157-EP-28 Coll, G., 140-ITAR-3, 167-LP-17 De Korver, V., 52-LP-7 ElHarriri, G., 97-EE-1 Frankford, D., 126-APS-4 Glass, J., 127-ECS-3 Collao, M., 44-GTE-5 Delange, J., 52-LP-7 Elkins-Tanton, L., 13-EP-3 Frederick, R., 10-EDU-1, 47-HR-2, 68-EDU-2, 118-SR-4, Glorieux, G., 155-EP-25 Collard, T., 157-EP-28 de la Torre, M., 42-FFP-1 Elliott, T., 4-ADP-1 128-EDU-3 Glowacki, J., 19-HR-1 Collicott, S., 51-LP-6 DeLaurentis, D., 75-GEPC-1 El-Melih, A., 134-FFP-2 Frediani, L., 5-AEC-1 Gloyer, P., 166-LP-16 Colpan, C., 43-GTE-4 Delgado, J., 13-EP-3 El-Sayed Sweida, W., 148-TM-5 Freitas, W., 8-ECD-1 Glusman, J., 95-APC-2 Connolly, J., 46-GTE-9 Demarest, A., 167-LP-17 Emrich, W., 113-NFF-4 Freudenmann, D., 139-HSABP-9 Goddard, R., 111-ITAR-2 Conomos, H., 111-ITAR-2 Demko, A., 27-PC-2, 54-PC-3, 174-SR-6 Engelbrecht, C., 52-LP-7 Friedrichs, J., 159-GTE-17 Godfey, J., 4-ADP-1 Conversano, R., 98-EP-15, 155-EP-25 Demmons, N., 73-EP-14 Englander, J., 40-EP-9 Frieman, J., 39-EP-8, 99-EP-16 Goebel, D., 13-EP-3, 100-EP-17, 101-EP-18, 131-EP-22, Coogan, S., 47-HR-2, 138-HR-7 de Natris, M., 25-LP-3 Epstein, A., 75-GEPC-1 Friss, A., 154-EP-24 154-EP-24 Coogan, W., 12-EP-2 Denny, M., 108-HR-6 Erbschloe, D., 97-EE-1 Frongillo, J., 14-EP-4 Goldberg, C., 93-ABPSI-4 Cooper, C., 10-EDU-1 Depew, D., 86-PC-6 Erhard, W., 161-GTE-19 Fu, Q., 48-HSABP-4 Golden, H., 111-ITAR-2 Coote, D., 142-LP-13 Derkevorkian, A., 140-ITAR-3 Ernst, B., 17-GTE-1 Fuchigami, K., 130-EP-21 Goldman, J., 70-EP-11 Copenhaver, W., 150-ABPSI-5 De Rose, F., 25-LP-3 Errico, M., 66-ECD-2 Fujii, J., 170-PC-15 Gollahalli, S., 134-FFP-2 Cornella, B., 12-EP-2 Desai, Y., 166-LP-16 Esker, B., 75-GEPC-1 Fujiwara, H., 134-FFP-2 Gollor, M., 155-EP-25 Cornu, N., 13-EP-3 Dev, B., 124-ADP-2 Espinosa, M., 140-ITAR-3 Funaki, I., 39-EP-8, 69-EP-10, 130-EP-21, 132-EP-23, Gomes, S., 128-EDU-3, 169-PC-14

79 Correyero Plaza, S., 156-EP-26 Devereaux, A., 141-LP-12 Ettleman, M., 140-ITAR-3 156-EP-26 Gonthier, K., 35-ECS-1 Costantino, A., 108-HR-6 DeVost, M., 138-HR-7 Evans, B., 78-HR-3, 86-PC-6, 145-PC-12 Funazaki, K., 143-LP-14 Gonzalez, M., 6-APC-1, 155-EP-25 Cottle, A., 18-GTE-2 Dhaliwal, V., 155-EP-25 Everett, M., 68-EDU-2 Gabaldo, M., 109-HSABP-7 Gorrell, S., 76-GTE-7, 77-GTE-8, 143-LP-14, 160-GTE-18 Cox, J., 44-GTE-5 Diallo, A., 38-EP-7 Ewing, M., 164-ITAR-4 Gagnon, N., 45-GTE-6 Gorshkov, O., 156-EP-26 Coxhill, I., 141-LP-12 Diamant, K., 13-EP-3 Eyi, S., 93-ABPSI-4 Galantini, P., 155-EP-25 Goss, C., 18-GTE-2 Coy, E., 167-LP-17 Dillier, C., 54-PC-3, 174-SR-6 Eytan, R., 99-EP-16 Galfetti, L., 19-HR-1, 27-PC-2 Goss, L., 18-GTE-2, 116-PC-11 Cremins, M., 105-GTE-11 Di Lorenzo, M., 27-PC-2 Fahrenthold, E., 35-ECS-1 Gallimore, A., 155-EP-25 Goto, K., 170-PC-15 Crowe, D., 3-ABPSI-1, 150-ABPSI-5 Ding, Y., 5-AEC-1 Fajardo, P., 156-EP-26 Gamba, M., 115-PC-10, 116-PC-11 Gottiparthi, K., 88-PC-8 Crudgington, P., 124-ADP-2 Dobbs, M., 151-ECD-3 Fan, W., 171-PC-16 Gamma, F., 163-HSABP-10 Gounder, J., 56-PC-5 Csank, J., 46-GTE-9, 136-GTE-14 Dobson, R., 148-TM-5 Fan, X., 81-HSABP-6, 90-TM-3 Ganesh Shankar, S., 93-ABPSI-4 Govardhan, M., 17-GTE-1 Csonka, S., 75-GEPC-1 Dodson, C., 71-EP-12, 100-EP-17, 101-EP-18 Farag, A., 90-TM-3, 119-TM-4 Gao, X., 43-GTE-4, 160-GTE-18 Gradl, P., 83-LP-8, 141-LP-12 Cuenot, B., 146-PC-13 Dong, D., 90-TM-3 Farias, E., 19-HR-1 Garcia, E., 135-GEPC-2/EOA-1 Greatrix, D., 19-HR-1 Culley, D., 46-GTE-9, 106-GTE-12 Donovan, A., 119-TM-4 Favini, B., 57-SR-2, 89-SR-3 Garg, S., 46-GTE-9 Grigsby, D., 4-ADP-1 Cunha, F., 28-SR-1 Dossi, S., 27-PC-2 Felder, J., 93-ABPSI-4, 135-GEPC-2/EOA-1 Garner, C., 13-EP-3 Grimaud, L., 99-EP-16 Cuppoletti, D., 81-HSABP-6, 139-HSABP-9 Dou, H., 109-HSABP-7 Feldman, M., 132-EP-23 Gascoin, N., 163-HSABP-10 Grinstein, D., 27-PC-2 Cusson, S., 155-EP-25 Dowdy, M., 25-LP-3 Feng, C., 117-SATS-1 Gatto, C., 4-ADP-1, 52-LP-7 Grist, R., 95-APC-2, 164-ITAR-4 Custer, C., 77-GTE-8 Drelich, J., 70-EP-11 Feng, S., 115-PC-10 Gea, L., 33-AEP-1, 65-AEP-2 Grohmann, J., 45-GTE-6 D, D., 18-GTE-2 Drennan, S., 18-GTE-2 Fengyuan, Z., 22-HSABP-3 Geiger, C., 136-GTE-14 Grondahl, C., 124-ADP-2 Dai, X., 158-GTE-16 Driscoll, E., 23-LP-1 Ferlauto, M., 3-ABPSI-1 Gejji, R., 166-LP-16 Gröning, S., 115-PC-10 Daimon, Y., 115-PC-10, 146-PC-13 Drobny, C., 102-EP-19 Fernandez, E., 76-GTE-7, 105-GTE-11, 158-GTE-16 Geng, S., 8-ECD-1, 151-ECD-3 Gross, A., 17-GTE-1 Dale, E., 155-EP-25 Drozda, T., 81-HSABP-6, 115-PC-10 Fernelius, M., 76-GTE-7 Genin, C., 50-LP-5 Gross, J., 116-PC-11 Dam, B., 114-PC-9 Du, L., 5-AEC-1 Feszty, D., 93-ABPSI-4, 97-EE-1 Georgin, M., 155-EP-25 Grossman, K., 54-PC-3, 174-SR-6 Daniels, C., 124-ADP-2 Ducharme, E., 75-GEPC-1 Fetes, J., 111-ITAR-2 Gerasimov, Y., 140-ITAR-3 Grubelich, M., 168-LP-18 Dankanich, J., 13-EP-3, 73-EP-14 Duchemin, O., 155-EP-25 Feyintola, I., 66-ECD-2 Gerlach, D., 66-ECD-2 Guadagnoli, D., 142-LP-13 Dankongkakul, B., 14-EP-4, 70-EP-11 Dudley, J., 124-ADP-2 Ficuciello, A., 166-LP-16 Ghilardi, M., 78-HR-3 Guan, F., 21-HSABP-2 Darkwa, J., 29-TM-1, 90-TM-3 Duffy, K., 65-AEP-2 Firdosy, S., 66-ECD-2 Ghoshal, A., 82-ITAR-1, 104-GTE-10 Guerra, M., 109-HSABP-7 Dasari, A., 115-PC-10 Duke, D., 169-PC-14 Fittje, J., 113-NFF-4 Giambusso, M., 132-EP-23 Guerrero, P., 154-EP-24 da Silva, A., 116-PC-11 Duncan, S., 9-EDES-1, 36-EDES-2, 97-EE-1, 153-EE-2 Flanigan, S., 52-LP-7 Gibson, J., 172-PP-1 Gümmer, V., 104-GTE-10, 161-GTE-19 Author/Session Chair Index Gunasekar, S., 18-GTE-2 Herdy, J., 10-EDU-1 Ichinokiyama, D., 8-ECD-1 Kakuma, T., 130-EP-21 King, L., 15-EP-5, 70-EP-11 Guo, T., 158-GTE-16 Herman, D., 40-EP-9, 98-EP-15 Iha, K., 128-EDU-3, 169-PC-14 Kaliyaperumal, A., 17-GTE-1 King, P., 82-ITAR-1 Gupta, A., 9-EDES-1, 42-FFP-1, 114-PC-9, 134-FFP-2, Hernandez, M., 42-FFP-1 Ihme, M., 88-PC-8 Kamhawi, H., 11-EP-1, 13-EP-3, 70-EP-11, 98-EP-15, Kirchberger, C., 49-LP-4, 116-PC-11 153-EE-2 Hertel, T., 7-APS-1 Iihara, S., 130-EP-21 130-EP-21, 154-EP-24, 155-EP-25 Kirk, D., 25-LP-3, 84-LP-9 Gurciullo, A., 131-EP-22 Hiatt, A., 118-SR-4, 128-EDU-3 Iijima, A., 167-LP-17, 168-LP-18 Kamps, L., 78-HR-3 Kirk, M., 52-LP-7 Gury, L., 49-LP-4 Hickey, J., 88-PC-8 Ilardi, B., 12-EP-2 Kanai, R., 165-LP-15 Kirk, T., 124-ADP-2 Gutierrez, H., 25-LP-3 Hickman, A., 44-GTE-5, 77-GTE-8 Imai, R., 25-LP-3 Kanaoka, K., 102-EP-19 Kitagawa, K., 138-HR-7 Haag, T., 70-EP-11, 98-EP-15, 130-EP-21 Hickman, T., 70-EP-11 Inclan, E., 161-GTE-19 Kang, S., 107-HR-5 Klimov, I., 77-GTE-8 Hageman, M., 93-ABPSI-4, 150-ABPSI-5 Hicks, Y., 114-PC-9 Indiana, C., 55-PC-4 Kapat, J., 8-ECD-1, 76-GTE-7, 105-GTE-11, 136-GTE-14, Kloesel, K., 33-AEP-1 Hagenmaier, M., 20-HSABP-1, 81-HSABP-6 Hidalgo, V., 93-ABPSI-4 Ingenito, A., 163-HSABP-10 158-GTE-16 Knab, O., 115-PC-10 Haidn, O., 54-PC-3, 56-PC-5, 86-PC-6, 88-PC-8, Higashino, K., 108-HR-6, 167-LP-17, 168-LP-18 Ireland, P., 106-GTE-12 Karabeyoglu, A., 78-HR-3, 108-HR-6 Knoll, A., 131-EP-22 145-PC-12, 146-PC-13 Higgins, A., 95-APC-2 Ishihara, K., 170-PC-15 Karadag, B., 132-EP-23 Knowlen, C., 95-APC-2, 139-HSABP-9, 164-ITAR-4 Haines, J., 96-APS-3, 126-APS-4 Higgins, C., 141-LP-12 Ishikawa, K., 84-LP-9 Karakoc, T., 43-GTE-4 Kobald, M., 47-HR-2, 162-HR-8 Hakim, A., 37-EP-6 Hilbert, B., 106-GTE-12 Ishikawa, Y., 165-LP-15 Karl, S., 50-LP-5 Kobayashi, K., 80-HSABP-5 Ham, F., 169-PC-14 Hill-Lam, B., 116-PC-11 Ishiyama, C., 170-PC-15 Karp, A., 19-HR-1, 47-HR-2, 138-HR-7, 162-HR-8 Kocaman, O., 87-PC-7 Hamada, Y., 38-EP-7, 132-EP-23 Himeno, T., 65-AEP-2, 84-LP-9 Ishizaki, S., 80-HSABP-5 Karthikeyan, G., 78-HR-3 Koch, J., 139-HSABP-9 Hamajima, S., 84-LP-9 Hiraiwa, T., 167-LP-17 Isono, T., 48-HSABP-4 Kartuzova, O., 51-LP-6 Kohlman, L., 33-AEP-1 Han, X., 125-APC-3 Hiramoto, K., 131-EP-22 Iwamoto, M., 156-EP-26 Kasahara, J., 170-PC-15 Koizumi, H., 38-EP-7, 69-EP-10, 131-EP-22 Hancock, R., 106-GTE-12 Hirano, Y., 38-EP-7 Jachura, R., 128-EDU-3, 169-PC-14 Kassemi, M., 51-LP-6 Kokal, U., 99-EP-16 Hannebique, G., 55-PC-4, 115-PC-10 Hirsch, C., 26-PC-1 Jackson, B., 15-EP-5, 100-EP-17 Kathrotia, T., 45-GTE-6 Kolbeck, J., 132-EP-23, 157-EP-28 Hannemann, V., 50-LP-5 Hitotsubashi, Y., 8-ECD-1 Jackson, D., 143-LP-14 Kato, H., 143-LP-14 Komurasaki, K., 38-EP-7, 69-EP-10, 129-EP-20, Hara, K., 11-EP-1, 37-EP-6, 69-EP-10 Hitt, M., 10-EDU-1, 47-HR-2, 68-EDU-2, 128-EDU-3 Jackson, T., 86-PC-6, 171-PC-16 Kato, Y., 170-PC-15 131-EP-22, 132-EP-23 Hardi, J., 115-PC-10 Ho, A., 100-EP-17 Jakka, R., 147-SR-5 Katz, I., 11-EP-1, 37-EP-6 Konopka, M., 25-LP-3 Hardin, L., 33-AEP-1 Hodges, J., 158-GTE-16 Janczewski, T., 150-ABPSI-5 Katz-Franco, D., 99-EP-16 Koo, J., 37-EP-6, 129-EP-20

80 Hargather, M., 168-LP-18 Hofer, R., 98-EP-15, 101-EP-18, 154-EP-24 Jee, D., 97-EE-1 Kawabata, R., 78-HR-3 Koroglu, B., 54-PC-3 Hargus, W., 38-EP-7, 173-SATS-2 Hohlfeld, E., 7-APS-1 Jeffrey, S., 104-GTE-10 Kawasaski, S., 143-LP-14 Kostecka, K., 67-ECS-2 Harris, C., 81-HSABP-6, 139-HSABP-9 Hoke, J., 82-ITAR-1, 110-HSABP-8, 111-ITAR-2 Jemcov, A., 77-GTE-8 Kawashima, R., 53-NFF-1, 69-EP-10, 102-EP-19 Krasowski, M., 126-APS-4 Harrison, W., 97-EE-1 Holgate, T., 96-APS-3 Jenkins, B., 4-ADP-1 Kayed, H., 148-TM-5 Kratz, J., 106-GTE-12, 158-GTE-16 Hartfield, R., 17-GTE-1, 22-HSABP-3 Hopkins, M., 70-EP-11 Jennings, T., 113-NFF-4 Keerthi, H., 68-EDU-2 Krishna, K., 104-GTE-10 Hartwig, J., 84-LP-9 Horio, S., 108-HR-6 Jens, E., 4-ADP-1, 138-HR-7 Keidar, M., 12-EP-2, 157-EP-28 Krivoruhko, D., 156-EP-26 Harvazinski, M., 166-LP-16, 167-LP-17 Hoskins, W., 157-EP-28 Jinchun, W., 159-GTE-17 Keim, N., 116-PC-11 Kröger, P., 49-LP-4 Hassan, E., 20-HSABP-1, 81-HSABP-6 Hossain, J., 76-GTE-7 Jing, T., 119-TM-4 Keller, R., 146-PC-13 Kruger, K., 172-PP-1 Hassan, M., 32-ABPSI-2, 119-TM-4, 148-TM-5 Hruby, V., 99-EP-16 John, J., 52-LP-7 Keller, S., 11-EP-1 Kubota, K., 39-EP-8, 69-EP-10, 130-EP-21 Hauk, A., 168-LP-18 Hu, N., 136-GTE-14 Johnson, I., 72-EP-13 Kelly, J., 106-GTE-12 Kudo, K., 48-HSABP-4 Hausen, R., 56-PC-5, 114-PC-9 Hu, Y., 129-EP-20 Johnson, J., 4-ADP-1 Kelly, R., 77-GTE-8, 140-ITAR-3 Kugele, J., 56-PC-5 Hawkett, B., 15-EP-5 Huang, C., 115-PC-10 Johnson, W., 84-LP-9 Kerler, M., 161-GTE-19 Kulkarni, S., 56-PC-5 Hayashi, A., 110-HSABP-8 Huang, G., 22-HSABP-3, 32-ABPSI-2, 90-TM-3, Jones, D., 68-EDU-2 Kern, F., 4-ADP-1 Kumar, A., 83-LP-8 Hayashi, D., 79-HR-4 159-GTE-17 Jones, M., 160-GTE-18 Keyawa, N., 96-APS-3, 140-ITAR-3 Kumar, G., 18-GTE-2 Hayashi, K., 49-LP-4 Huang, W., 39-EP-8, 98-EP-15, 130-EP-21, 154-EP-24 Jorns, B., 11-EP-1, 13-EP-3, 37-EP-6, 39-EP-8, Khadse, A., 8-ECD-1 Kumar, R., 139-HSABP-9 Hays, A., 32-ABPSI-2 Huelskamp, B., 116-PC-11 100-EP-17, 101-EP-18, 154-EP-24 Khalid, S., 43-GTE-4 Kumar N, V., 117-SATS-1 He, G., 22-HSABP-3, 64-ABPSI-3, 119-TM-4 Huerta, C., 37-EP-6, 101-EP-18 Joshi, N., 164-ITAR-4 Khalil, A., 114-PC-9 Kumazawa, Y., 170-PC-15 He, J., 171-PC-16 Hui, X., 55-PC-4 Joubert, E., 33-AEP-1 Khalil, E., 90-TM-3, 97-EE-1, 119-TM-4, 148-TM-5, Kurosaka, M., 139-HSABP-9 He, Z., 114-PC-9 Huihui, H., 22-HSABP-3 Joyner, C., 113-NFF-4 176-TM-7 Kurt, H., 99-EP-16 Heath, J., 139-HSABP-9 Huo, H., 109-HSABP-7 Jung, S., 167-LP-17 Khalil, M., 90-TM-3 Kuwahara, T., 49-LP-4, 107-HR-5, 174-SR-6 Hedayat, A., 51-LP-6 Hupfer, A., 104-GTE-10 Jung, W., 109-HSABP-7 Khandelwal, B., 42-FFP-1, 134-FFP-2 Kuznetsov, A., 95-APC-2 Heister, S., 51-LP-6, 142-LP-13, 170-PC-15 Hurlbert, E., 52-LP-7 Juvé, L., 33-AEP-1 Khoury, F., 94-AEC-2 Kweon, C., 54-PC-3, 172-PP-1 Henderson, E., 6-APC-1 Hurley, S., 157-EP-28 K, T., 147-SR-5 Kim, D., 169-PC-14 Kwon, O., 145-PC-12 Hendrich, C., 49-LP-4 Hussaein, M., 153-EE-2 Kailasanath, K., 82-ITAR-1, 86-PC-6, 110-HSABP-8, Kim, H., 38-EP-7, 145-PC-12, 156-EP-26 Kwon, S., 107-HR-5, 109-HSABP-7, 167-LP-17 Hendricks, T., 140-ITAR-3, 151-ECD-3 Huth, J., 151-ECD-3 164-ITAR-4 Kim, J., 26-PC-1, 38-EP-7, 156-EP-26 Kwon, T., 109-HSABP-7 Heo, S., 167-LP-17 Huzzayyin, O., 148-TM-5 Kakami, A., 102-EP-19 Kim, M., 26-PC-1 Lacava, P., 28-SR-1 Hepler, M., 12-EP-2 Ibrahim, S., 134-FFP-2 Kaku, M., 117-SATS-1 Kim, T., 145-PC-12 Lachance, A., 105-GTE-11 Herbst, F., 17-GTE-1, 159-GTE-17 Ichimura, M., 131-EP-22 Kakudo, H., 165-LP-15 Kinefuchi, K., 163-HSABP-10 Ladeinde, F., 20-HSABP-1, 80-HSABP-5 Author/Session Chair Index Lafko, D., 117-SATS-1 Liou, M., 45-GTE-6 Maicke, B., 24-LP-2 Mears, L., 105-GTE-11 Mulkey, H., 23-LP-1 Lai, A., 47-HR-2 List, M., 77-GTE-8, 150-ABPSI-5 Mair, M., 106-GTE-12 Mechentel, F., 19-HR-1, 47-HR-2 Müller, C., 159-GTE-17 Laker, T., 164-ITAR-4 Litt, J., 10-EDU-1, 158-GTE-16 Majdalani, J., 24-LP-2, 57-SR-2, 89-SR-3, 162-HR-8 Mehta, J., 90-TM-3, 119-TM-4 Müller, H., 146-PC-13 Lam, G., 7-APS-1, 126-APS-4 Little, J., 129-EP-20 Majumdar, A., 51-LP-6 Meier, W., 45-GTE-6 Müller, S., 168-LP-18 Lamanna, G., 55-PC-4, 88-PC-8 Littles, J., 140-ITAR-3 Makela, J., 99-EP-16 Mejia, G., 169-PC-14 Mundahl, A., 23-LP-1 Lamarre, N., 73-EP-14 Liu, H., 160-GTE-18 Makida, M., 134-FFP-2 Melcher, J., 52-LP-7 Munipalli, R., 82-ITAR-1 Lang, J., 118-SR-4 Liu, L., 106-GTE-12, 160-GTE-18, 172-PP-1 Malo-Molina, F., 20-HSABP-1, 80-HSABP-5 Menon, S., 55-PC-4, 87-PC-7, 115-PC-10, 146-PC-13, Murakami, A., 48-HSABP-4 Lapp, K., 172-PP-1 Liu, P., 22-HSABP-3 Manfletti, C., 139-HSABP-9 171-PC-16 Muralidharan, B., 171-PC-16 Larusson, R., 50-LP-5 Liu, Q., 69-EP-10 Mani, K., 77-GTE-8 Merino-Martinez, M., 156-EP-26 Murganandam, T., 163-HSABP-10 Laufer, P., 102-EP-19 Liu, T., 99-EP-16 Mani, S., 28-SR-1, 93-ABPSI-4, 117-SATS-1, 118-SR-4 Merkle, C., 115-PC-10 Murphy, J., 170-PC-15 Lavelle, T., 10-EDU-1 Liu, X., 22-HSABP-3, 172-PP-1, 174-SR-6 Manishaa, R., 118-SR-4 Merkley, S., 47-HR-2, 108-HR-6 Murthy, H., 147-SR-5 Leary, B., 174-SR-6 Liu, Y., 5-AEC-1, 119-TM-4, 147-SR-5 Manning, R., 25-LP-3 Metscher, J., 151-ECD-3 Murugan, M., 104-GTE-10 Leccese, G., 162-HR-8 Liu, Z., 22-HSABP-3, 64-ABPSI-3, 82-ITAR-1, 95-APC-2, Marcu, B., 143-LP-14 Metsker, Y., 56-PC-5 Mustaikis, S., 111-ITAR-2 LeClair, A., 51-LP-6 160-GTE-18 Marks, C., 17-GTE-1 Meyer, M., 25-LP-3, 84-LP-9 Mutschler, M., 56-PC-5 Lee, C., 107-HR-5, 108-HR-6 Lobbia, R., 156-EP-26 Marrese-Reading, C., 15-EP-5, 73-EP-14 Michael, J., 27-PC-2, 174-SR-6 Myers, J., 11-EP-1 Lee, D., 107-HR-5 Lohner, K., 50-LP-5 Marsell, B., 25-LP-3 Michalski, Q., 56-PC-5 Myers, M., 126-APS-4 Lee, E., 107-HR-5 Lopez, J., 54-PC-3 Marshall, W., 112-LP-11 Mikellides, I., 11-EP-1, 37-EP-6, 39-EP-8, 71-EP-12, Nabity, J., 32-ABPSI-2 Lee, H., 171-PC-16 Lopez Ortega, A., 11-EP-1, 37-EP-6, 39-EP-8, Marsilio, R., 3-ABPSI-1 100-EP-17 Nagaiah, N., 136-GTE-14 Lee, J., 7-APS-1 100-EP-17, 131-EP-22 Martin, C., 3-ABPSI-1 Miki, K., 45-GTE-6 Nagaraju Doddi, H., 150-ABPSI-5 Lee, P., 45-GTE-6, 87-PC-7, 114-PC-9 Lord, P., 13-EP-3 Martin, R., 129-EP-20 Mikitchuk, D., 71-EP-12 Nagata, H., 78-HR-3, 79-HR-4 Lee, S., 38-EP-7, 156-EP-26 Lörincz, I., 144-NFF-6 Martinez, A., 70-EP-11 Mikoshiba, K., 142-LP-13 Nairus, J., 135-GEPC-2/EOA-1 Lee, T., 13-EP-3 Losser, B., 164-ITAR-4 Mason, L., 36-EDES-2, 151-ECD-3 Miles, R., 163-HSABP-10 Naitoh, K., 64-ABPSI-3 Lekeux, A., 52-LP-7, 167-LP-17 Lou, Z., 20-HSABP-1 Masquelet, M., 24-LP-2, 54-PC-3 Miley, G., 72-EP-13 Nakada, Y., 138-HR-7 Lemieux, P., 36-EDES-2 Loures da Costa, L., 118-SR-4 Masse, R., 23-LP-1 Millar, R., 5-AEC-1, 94-AEC-2 Nakagami, S., 170-PC-15

81 Lents, C., 33-AEP-1, 135-GEPC-2/EOA-1 Love, N., 42-FFP-1, 68-EDU-2, 111-ITAR-2, 141-LP-12 Masuda, I., 165-LP-15 Miller, C., 15-EP-5, 73-EP-14 Nakagawa, I., 138-HR-7 Leray, D., 33-AEP-1 Lozano, P., 15-EP-5 Mataczynski, M., 172-PP-1 Miller, J., 23-LP-1 Nakagawa, Y., 131-EP-22 Lettieri, C., 143-LP-14 Lu, F., 32-ABPSI-2, 110-HSABP-8 Mather, J., 124-ADP-2 Miller, S., 73-EP-14, 83-LP-8 Nakamura, M., 134-FFP-2 Lev, D., 71-EP-12, 99-EP-16 Lu, H., 64-ABPSI-3 Mathers, A., 99-EP-16 Millsaps, K., 82-ITAR-1 Nakano, R., 48-HSABP-4 Levack, D., 113-NFF-4 Lu, X., 69-EP-10 Mathias, S., 162-HR-8 Mines, J., 161-GTE-19 Nakashima, H., 156-EP-26 Lewandowski, E., 96-APS-3 Lu, Y., 81-HSABP-6, 90-TM-3 Mathison, R., 158-GTE-16 Mishima, G., 138-HR-7 Nakata, D., 108-HR-6, 168-LP-18 Lewe, J., 97-EE-1 Lucht, R., 87-PC-7 Matlock, T., 101-EP-18, 154-EP-24 Miyagi, K., 102-EP-19 Nakatsukasa, G., 66-ECD-2 Leylegian, J., 50-LP-5, 171-PC-16 Lukas, J., 157-EP-28 Matsuo, A., 170-PC-15 Miyazaki, K., 170-PC-15 Nakaya, S., 165-LP-15 Leyton, J., 134-FFP-2 Lundgreen, R., 143-LP-14 Matsuoka, K., 170-PC-15 Mizener, A., 110-HSABP-8 Nakazono, B., 47-HR-2, 138-HR-7 Leyva, I., 165-LP-15 Lungu, P., 56-PC-5 Matsushima, J., 117-SATS-1 Mizuchi, M., 138-HR-7 Nalianda, D., 93-ABPSI-4 Li, B., 66-ECD-2 Luo, F., 135-GEPC-2/EOA-1 Mattick, A., 139-HSABP-9 Moder, J., 45-GTE-6, 51-LP-6 Nalim, M., 18-GTE-2 Li, C., 82-ITAR-1 Luo, G., 106-GTE-12 Matusik, K., 169-PC-14 Moehlenkamp, R., 21-HSABP-2, 163-HSABP-10 Nanri, H., 165-LP-15 Li, G., 38-EP-7, 101-EP-18, 159-GTE-17, 160-GTE-18 Luo, M., 88-PC-8 Mauro, S., 70-EP-11 Moessner, D., 52-LP-7 Naraghi, M., 50-LP-5 Li, J., 55-PC-4 Luo, Y., 5-AEC-1 Mavris, D., 43-GTE-4, 97-EE-1 Mohagheghi, M., 8-ECD-1 Narsai, P., 19-HR-1, 79-HR-4, 108-HR-6 Li, L., 159-GTE-17 Lynch, A., 116-PC-11 Maxwell, J., 59-VS-1 Molinsky, J., 25-LP-3 Naseem, H., 147-SR-5 Li, W., 119-TM-4 Lynch, E., 114-PC-9 Maxwell, T., 58-TM-2 Mongia, H., 45-GTE-6, 87-PC-7, 114-PC-9 Nash, L., 54-PC-3 Li, X., 81-HSABP-6, 109-HSABP-7 Lyu, X., 174-SR-6 Maynes, D., 143-LP-14 Monico, L., 134-FFP-2 Nassar, A., 77-GTE-8 Liang, H., 159-GTE-17 Ma, H., 21-HSABP-2 Mazouffre, S., 99-EP-16, 130-EP-21 Moon, Y., 108-HR-6 Nasuti, F., 162-HR-8 Liang, J., 110-HSABP-8 Ma, N., 82-ITAR-1 McAdams, J., 52-LP-7 Moore, C., 127-ECS-3 Natan, B., 27-PC-2 Liang, R., 13-EP-3, 130-EP-21 MacDonald, N., 101-EP-18 McClearn, M., 172-PP-1 Moore, J., 23-LP-1, 111-ITAR-2, 142-LP-13 Naumann, K., 49-LP-4, 118-SR-4 Lim, D., 142-LP-13 Macklin, S., 143-LP-14 McCurdy, D., 113-NFF-4 Morehead, R., 52-LP-7 Navarro, J., 156-EP-26 Lim, Y., 38-EP-7, 156-EP-26 Macmann, O., 94-AEC-2 McCurry, C., 94-AEC-2 Morgan, J., 127-ECS-3 Neff, D., 140-ITAR-3 Lin, B., 119-TM-4 MacManus, D., 93-ABPSI-4 McFarland, M., 104-GTE-10 Morgan, O., 142-LP-13 Negishi, H., 84-LP-9 Lin, J., 47-HR-2 Madhanabharatam, B., 108-HR-6 McHenry, S., 28-SR-1 Mori, K., 125-APC-3 Negri, M., 49-LP-4 Lin, W., 44-GTE-5 Madureira, L., 174-SR-6 McKechnie, T., 111-ITAR-2 Morita, T., 53-NFF-1, 156-EP-26 Nellis, B., 4-ADP-1 Lin, Y., 33-AEP-1, 55-PC-4 Maestro, D., 146-PC-13, 169-PC-14 McNatt, J., 126-APS-4 Moroz, L., 77-GTE-8 Nelson, G., 108-HR-6 Lindsey, C., 172-PP-1 Maggi, F., 19-HR-1, 27-PC-2 McQuirter, A., 76-GTE-7 Morris, S., 44-GTE-5, 77-GTE-8, 106-GTE-12 Neri, A., 57-SR-2, 89-SR-3 Lineberry, D., 24-LP-2, 128-EDU-3, 166-LP-16 Maharaj, C., 107-HR-5 McTavish, S., 97-EE-1 Morrow, G., 27-PC-2, 138-HR-7, 174-SR-6 Nesmith, B., 140-ITAR-3 Author/Session Chair Index Nessler, C., 150-ABPSI-5 Özyörük, Y., 28-SR-1 Phillip, J., 168-LP-18 Rayman, M., 13-EP-3 S, R., 83-LP-8 Neuroth, C., 116-PC-11 P, P., 117-SATS-1 Pilidis, P., 93-ABPSI-4, 161-GTE-19 Redmond, M., 19-HR-1 Sack, W., 140-ITAR-3 Neville, J., 7-APS-1 Paccagnella, E., 78-HR-3 Pimenta, A., 128-EDU-3 Reese, S., 24-LP-2 Sadey, D., 126-APS-4 Nguyen, T., 27-PC-2 Pack, S., 4-ADP-1 Pinero, L., 7-APS-1, 130-EP-21, 155-EP-25 Reid, T., 151-ECD-3 Sahara, H., 117-SATS-1 Ni, J., 66-ECD-2 Pai, M., 54-PC-3 Pinto, P., 49-LP-4 Reilly, S., 154-EP-24 Saheby, E., 32-ABPSI-2 Nichith, C., 28-SR-1, 83-LP-8, 117-SATS-1 Paintal, S., 99-EP-16 Piszczor, M., 8-ECD-1, 126-APS-4 Reissner, A., 157-EP-28 Sahoo, S., 104-GTE-10 Nicholas, A., 140-ITAR-3 Palaszewski, B., 85-NFF-3, 113-NFF-4, 121-NFF-5, Pitot, J., 107-HR-5 Reisz, A., 6-APC-1, 95-APC-2, 125-APC-3 Said, A., 42-FFP-1 Nie, W., 115-PC-10 144-NFF-6 Pitts, H., 140-ITAR-3 Ren, J., 69-EP-10 Saito, N., 53-NFF-1 Niehues, J., 67-ECS-2 Palencia, J., 155-EP-25 Podboy, D., 114-PC-9 Ren, X., 45-GTE-6 Saito, Y., 78-HR-3, 79-HR-4 Niehuis, R., 4-ADP-1, 44-GTE-5 Panchal, A., 55-PC-4, 115-PC-10, 146-PC-13 Poe, D., 147-SR-5 Rezende, R., 68-EDU-2, 128-EDU-3 Sakaguchi, H., 165-LP-15 Nielsen, T., 82-ITAR-1 Pancotti, A., 12-EP-2 Polanka, M., 18-GTE-2, 82-ITAR-1, 172-PP-1 Rheaume, J., 33-AEP-1, 66-ECD-2 Sakaki, K., 165-LP-15 Nikbay, M., 147-SR-5 Pande, B., 59-VS-1 Polanskey, C., 13-EP-3 Rhodes, R., 6-APC-1 Sakuma, Y., 84-LP-9 Nishizawa, A., 65-AEP-2 Pandey, K., 169-PC-14 Polk, J., 69-EP-10, 71-EP-12, 98-EP-15, 100-EP-17, Riccius, J., 24-LP-2 Sakurai, T., 79-HR-4 Noall, J., 143-LP-14 Pang, X., 174-SR-6 154-EP-24 Richard, C., 166-LP-16 Sakuranaka, N., 80-HSABP-5 Nobbe, S., 56-PC-5 Paniagua, G., 17-GTE-1, 18-GTE-2, 48-HSABP-4, Polzin, K., 70-EP-11, 101-EP-18 Richards, W., 88-PC-8 Salzler, T., 111-ITAR-2 Nojima, K., 80-HSABP-5 136-GTE-14 Poothokaran, J., 25-LP-3 Richardson, D., 116-PC-11 Samim, S., 134-FFP-2 Noland, J., 13-EP-3 Papathakis, K., 33-AEP-1 Port, D., 44-GTE-5 Ricklick, M., 29-TM-1, 76-GTE-7, 104-GTE-10, Samland, M., 76-GTE-7 Nomura, H., 65-AEP-2 Parammasivam, K., 18-GTE-2 Pote, B., 99-EP-16 105-GTE-11 Sammet, T., 54-PC-3, 174-SR-6 Nordeen, C., 82-ITAR-1 Paravan, C., 19-HR-1, 27-PC-2 Pourpoint, T., 168-LP-18 Riehl, R., 90-TM-3 Samples, S., 69-EP-10 Norick, T., 7-APS-1 Park, J., 109-HSABP-7 Powell, C., 169-PC-14 Riggins, D., 43-GTE-4 Samudrala, O., 124-ADP-2 Nowlin, B., 151-ECD-3 Park, P., 140-ITAR-3 Pradhan, S., 4-ADP-1, 97-EE-1, 153-EE-2, 159-GTE-17 Rimoli, J., 101-EP-18 Sanal Kumar, V., 28-SR-1, 83-LP-8, 93-ABPSI-4, Nürmberger, F., 102-EP-19 Parker, M., 47-HR-2, 73-EP-14 Prager, J., 72-EP-13 Ringuette, S., 141-LP-12 117-SATS-1, 118-SR-4, 150-ABPSI-5 Nuzum, S., 148-TM-5 Parlett, A., 10-EDU-1 Prakash, A., 3-ABPSI-1, 150-ABPSI-5 Risha, G., 142-LP-13 Sánchez, G., 156-EP-26 Nyquist, S., 167-LP-17 Parthasarathy, R., 134-FFP-2 Prasad, A., 160-GTE-18 Risse, S., 49-LP-4 Sanchez, L., 141-LP-12

82 O’Brien, T., 139-HSABP-9 Pastrone, D., 19-HR-1, 162-HR-8 Pratt, A., 87-PC-7 Roa, M., 166-LP-16 Sanders, D., 3-ABPSI-1, 150-ABPSI-5 O’Dowd, D., 10-EDU-1 Patel, A., 128-EDU-3 Pratt, L., 150-ABPSI-5 Roberson, B., 72-EP-13 Sandifer, C., 66-ECD-2 Oefelein, J., 88-PC-8 Patel, M., 7-APS-1, 96-APS-3 Prince, B., 15-EP-5, 73-EP-14 Roberson, L., 127-ECS-3 Sankaran, R., 88-PC-8 Ogawa, D., 167-LP-17 Patel, V., 113-NFF-4 Proctor, M., 124-ADP-2 Roberts, R., 66-ECD-2, 94-AEC-2, 119-TM-4, 148-TM-5, Sankaran, V., 88-PC-8, 166-LP-16, 167-LP-17 Ogedengbe, E., 36-EDES-2, 66-ECD-2, 97-EE-1, Patino, M., 11-EP-1 Prokop, N., 126-APS-4 161-GTE-19 Sannino, J., 52-LP-7 153-EE-2, 176-TM-7 Patterson, M., 164-ITAR-4 Pryor, O., 54-PC-3 Roberts, W., 95-APC-2 Santiago, W., 98-EP-15, 155-EP-25 Oguma, M., 167-LP-17 Pavarin, D., 78-HR-3 Qin, F., 64-ABPSI-3, 119-TM-4 Robin, M., 117-SATS-1 Sanzi, J., 151-ECD-3 Oh, D., 13-EP-3, 99-EP-16 Pawlak, A., 124-ADP-2 Qin, J., 166-LP-16 Robinson, D., 154-EP-24 Sarawate, N., 124-ADP-2 Oh, S., 97-EE-1 Paxson, D., 18-GTE-2, 22-HSABP-3, 172-PP-1 Qin, Y., 39-EP-8 Robinson, J., 6-APC-1, 95-APC-2, 125-APC-3 Sardeshmukh, S., 142-LP-13, 165-LP-15, 170-PC-15 Ohkawa, Y., 39-EP-8 Peace, J., 110-HSABP-8 Rachner, M., 56-PC-5 Roboam, X., 33-AEP-1 Sareni, B., 33-AEP-1 Ohlinger, W., 71-EP-12 Peeples, S., 70-EP-11 Raisanen, A., 37-EP-6 Rocco, J., 128-EDU-3, 169-PC-14 Sargent, S., 143-LP-14 Oishige, Y., 79-HR-4 Pei, J., 147-SR-5 Raitses, Y., 11-EP-1, 38-EP-7 Rocco, L., 128-EDU-3, 169-PC-14 Saripalli, P., 40-EP-9 Okai, K., 65-AEP-2, 134-FFP-2 Pekardan, C., 95-APC-2 Raj, M., 83-LP-8 Rodriguez, J., 105-GTE-11, 158-GTE-16 Sarver-Verhey, T., 154-EP-24 Okuno, Y., 8-ECD-1 Pencil, E., 72-EP-13 Rajoriya, G., 27-PC-2 Rodriguez, M., 53-NFF-1, 85-NFF-3 Sathyaprabha, R., 118-SR-4 Olaitan, K., 176-TM-7 Pepi, M., 104-GTE-10 Raju, M., 169-PC-14 Rojas Mata, S., 11-EP-1 Sato, Y., 107-HR-5 Olalekan, O., 153-EE-2 Perakis, N., 145-PC-12 Ramakrishna, P., 3-ABPSI-1, 27-PC-2, 147-SR-5 Romadanov, I., 38-EP-7 Sattelmayer, T., 26-PC-1, 146-PC-13 Oliphant, K., 143-LP-14 Pereira, C., 174-SR-6 Ramesh kumar, T., 28-SR-1, 83-LP-8 Romanov, V., 82-ITAR-1 Saucier, C., 81-HSABP-6 Oliver, L., 56-PC-5 Perez-Grande, D., 100-EP-17 Ramsel, J., 49-LP-4 Rossman, C., 105-GTE-11 Sauer, J., 168-LP-18 Oravec, H., 124-ADP-2 Perkins, H., 18-GTE-2 Randall, M., 147-SR-5 Roth, C., 146-PC-13, 169-PC-14 Saul, W., 168-LP-18 Oriti, S., 96-APS-3 Perullo, C., 137-GTE-15/ABPSI-6/HSABP-11, Rangaraj, V., 150-ABPSI-5 Rotlisberger, L., 13-EP-3 Savill, M., 171-PC-16 Oschwald, M., 115-PC-10 158-GTE-16 Ranjan, R., 55-PC-4, 115-PC-10, 146-PC-13 Rousseau, C., 89-SR-3, 174-SR-6 Sawhill, S., 35-ECS-1, 111-ITAR-2, 164-ITAR-4 Oshio, Y., 39-EP-8, 132-EP-23, 156-EP-26 Petersen, E., 27-PC-2, 54-PC-3, 138-HR-7 Ransom, D., 166-LP-16 Rovey, J., 23-LP-1, 73-EP-14, 102-EP-19 Saygin, Y., 87-PC-7 Östlund, J., 50-LP-5 Peterson, D., 20-HSABP-1 Rao, A., 147-SR-5 Roy, B., 10-EDU-1 Schäffer, C., 161-GTE-19 Ott, R., 57-SR-2 Peterson, M., 77-GTE-8 Rao, P., 35-ECS-1 Roy, S., 160-GTE-18 Schauer, F., 82-ITAR-1, 110-HSABP-8, 111-ITAR-2, Ouyang, J., 39-EP-8 Peterson, P., 98-EP-15, 99-EP-16, 154-EP-24, 156-EP-26 Rathi, N., 3-ABPSI-1 Rozendaal, A., 44-GTE-5 172-PP-1 Ozawa, K., 138-HR-7 Petitot, S., 55-PC-4 Rauch, B., 45-GTE-6 Ryan, S., 113-NFF-4 Scheidegger, R., 155-EP-25 Ozcan, M., 43-GTE-4 Petro, E., 72-EP-13 Raush, G., 136-GTE-14 Ryon, J., 4-ADP-1 Schifer, N., 151-ECD-3 Ozer, A., 28-SR-1 Pfitzner, M., 146-PC-13 Ravi, V., 66-ECD-2 S, A., 83-LP-8 Schillo, K., 53-NFF-1 Author/Session Chair Index Schinder, A., 101-EP-18 Shuli, H., 159-GTE-17 Stechmann, D., 142-LP-13, 170-PC-15 Taylor, B., 113-NFF-4 Uptergrove, P., 68-EDU-2 Schlechtriem, S., 49-LP-4, 139-HSABP-9, 168-LP-18 Silvestri, S., 116-PC-11, 145-PC-12 Steinberg, A., 56-PC-5, 88-PC-8 Taylor, C., 126-APS-4 UsLu, S., 87-PC-7 Schlieben, G., 145-PC-12 Simons, M., 4-ADP-1 Stewart, E., 113-NFF-4 Taylor, L., 126-APS-4 Usrey, M., 5-AEC-1 Schmidt, J., 29-TM-1 Singh Nandan, R., 117-SATS-1 Stewart, M., 51-LP-6 Tedder, S., 114-PC-9 Usuki, T., 138-HR-7 Schmidt, T., 104-GTE-10 Singleton, J., 173-SATS-2 Stober, K., 19-HR-1, 79-HR-4, 86-PC-6, 108-HR-6, Tedrake, R., 99-EP-16 Utz, R., 96-APS-3 Schmitz, P., 151-ECD-3 Sippel, T., 27-PC-2, 174-SR-6 145-PC-12 Teel, G., 157-EP-28 Valencia, E., 93-ABPSI-4 Schneider, D., 50-LP-5 Skrylev, A., 156-EP-26 Storey, J., 25-LP-3 Tegner, J., 21-HSABP-2 Valentich, G., 139-HSABP-9 Schönherr, T., 38-EP-7 Slabaugh, C., 87-PC-7 Story, G., 19-HR-1, 138-HR-7 Temme, J., 54-PC-3 Vancil, B., 71-EP-12 Schpector, J., 174-SR-6 Slater, J., 32-ABPSI-2, 64-ABPSI-3 Strasser, M., 4-ADP-1 Teowee, G., 127-ECS-3 Van Dresar, N., 84-LP-9 Schreiber, T., 121-NFF-5 Slavinskaya, N., 86-PC-6 Straub, J., 117-SATS-1, 173-SATS-2 Terashima, H., 88-PC-8, 115-PC-10 Vannoy, S., 150-ABPSI-5, 161-GTE-19 Schumaker, S., 165-LP-15, 166-LP-16 Slobodov, I., 72-EP-13 Strauss, F., 139-HSABP-9 Terhune, K., 15-EP-5, 98-EP-15 Van Poppel, B., 105-GTE-11 Schwaiger, M., 172-PP-1 Slough, J., 12-EP-2 Su, W., 29-TM-1 Tess, M., 54-PC-3 Varma, M., 117-SATS-1 Schwer, D., 82-ITAR-1, 86-PC-6 Smith, B., 101-EP-18, 127-ECS-3 Sujith, R., 45-GTE-6 Thauvin, J., 33-AEP-1 Vasu, S., 54-PC-3 Scott, J., 67-ECS-2 Smith, K., 66-ECD-2 Sujittosakul, S., 66-ECD-2 Theba, R., 79-HR-4 Vaudolon, J., 99-EP-16 Seal, S., 54-PC-3, 174-SR-6 Smith, L., 87-PC-7 Sun, M., 80-HSABP-5 Théron, M., 166-LP-16 Vaughan, D., 47-HR-2, 138-HR-7 Sedwick, R., 61-NFF-2, 72-EP-13, 85-NFF-3 Smith, R., 24-LP-2 Sun, X., 78-HR-3 Thiede, G., 24-LP-2 Vazquez, A., 111-ITAR-2 Seider, Z., 167-LP-17 Smith, T., 70-EP-11 Sunahara, A., 53-NFF-1 Thiry, N., 48-HSABP-4 Veale, K., 79-HR-4, 107-HR-5 Seitz, T., 94-AEC-2 Smithson, T., 141-LP-12 Sung, C., 45-GTE-6 Thomas, A., 19-HR-1, 86-PC-6, 145-PC-12 Vega, J., 134-FFP-2 Seixal, J., 70-EP-11 Smolyakov, A., 38-EP-7 Suo, J., 159-GTE-17 Thomas, G., 46-GTE-9 Venkataraman, K., 19-HR-1, 79-HR-4, 108-HR-6 Sekerak, M., 98-EP-15, 101-EP-18, 154-EP-24 Snow, C., 105-GTE-11 Suryanarayanan, A., 159-GTE-17 Thomas, J., 138-HR-7 Venkatesan, K., 87-PC-7 Selby, M., 13-EP-3 Snyder, J., 98-EP-15 Surzhikov, S., 21-HSABP-2 Thomas, R., 164-ITAR-4 Venneri, P., 113-NFF-4 Seleznev, R., 21-HSABP-2 Soeda, K., 79-HR-4 Suslov, D., 115-PC-10 Thorn, C., 17-GTE-1 Venturini, M., 116-PC-11 Selvakarthick, C., 150-ABPSI-5 Soejima, M., 80-HSABP-5 Suzuki, K., 165-LP-15 Thornock, R., 3-ABPSI-1 Vergos, C., 105-GTE-11 Senda, F., 148-TM-5 Sohret, Y., 43-GTE-4 Svarnas, P., 38-EP-7 Thorpe, D., 6-APC-1 Verhulst, C., 105-GTE-11

83 Senda, P., 148-TM-5 Solano, H., 97-EE-1 Swanson, T., 13-EP-3 Thrasher, J., 102-EP-19 Vial, V., 13-EP-3 Seo, H., 26-PC-1 Solomon, Y., 27-PC-2 Swiatek, M., 154-EP-24 Thumann, A., 49-LP-4 Vieille, B., 52-LP-7 Seume, J., 17-GTE-1 Sondergaard, R., 17-GTE-1 Synovec, R., 116-PC-11 Tian, H., 78-HR-3 Vigil Lopez, C., 7-APS-1 Sharan, S., 83-LP-8, 117-SATS-1 Song, K., 97-EE-1 Szabo, J., 99-EP-16 Tighe, W., 38-EP-7 Vignesh, S., 28-SR-1, 83-LP-8, 93-ABPSI-4 Shastry, R., 40-EP-9 Song, W., 80-HSABP-5 Szedlmayer, M., 172-PP-1 Tilley, S., 13-EP-3 Vigneshwaran, S., 83-LP-8, 118-SR-4 Shaw, G., 164-ITAR-4 Song, Y., 96-APS-3, 159-GTE-17, 160-GTE-18 Tachibana, T., 102-EP-19 Tola, C., 147-SR-5 Vijay, C., 27-PC-2 Shchetkovskiy, A., 111-ITAR-2 Soulas, G., 40-EP-9 Tacina, K., 114-PC-9 Tolson, B., 96-APS-3 Villafane, L., 136-GTE-14 Sheehan, J., 157-EP-28 Sousa, J., 18-GTE-2, 95-APC-2, 102-EP-19, 140-ITAR-3 Tacussis, V., 167-LP-17 Tomioka, S., 48-HSABP-4, 80-HSABP-5 Villar, L., 174-SR-6 Shen, Q., 21-HSABP-2 Spakovszky, Z., 143-LP-14 Taddeo, L., 163-HSABP-10 Tonooka, S., 156-EP-26 Vishnu, N., 83-LP-8 Sherbina, A., 77-GTE-8 Spektor, R., 11-EP-1, 38-EP-7, 100-EP-17 Tagashira, T., 65-AEP-2 Toro Medina, J., 5-AEC-1 Vivek, S., 93-ABPSI-4 Shi, D., 96-APS-3 Spence, D., 73-EP-14 Tahara, H., 56-PC-5, 102-EP-19, 130-EP-21 Torres, S., 141-LP-12 von Sethe, C., 56-PC-5 Shi, J., 160-GTE-18 Spencer, R., 160-GTE-18 Tai, J., 43-GTE-4, 137-GTE-15/ABPSI-6/HSABP-11, Totani, T., 79-HR-4 Wafi, T., 90-TM-3 Shi, K., 77-GTE-8 Spirnak, J., 76-GTE-7 161-GTE-19 Trabasso, L., 118-SR-4 Wagner, C., 58-TM-2 Shi, L., 22-HSABP-3, 64-ABPSI-3, 109-HSABP-7 Spores, R., 23-LP-1 Tajmar, M., 85-NFF-3, 102-EP-19, 121-NFF-5, 144-NFF-6 Tran, P., 105-GTE-11 Wagner, N., 155-EP-25 Shi, X., 69-EP-10 Spotts, N., 160-GTE-18 Takahashi, M., 80-HSABP-5 Travis, J., 95-APC-2 Walker, M., 98-EP-15, 99-EP-16, 101-EP-18 Shilo, V., 155-EP-25 Springer, R., 81-HSABP-6 Takahashi, P., 102-EP-19, 140-ITAR-3 Tremont, B., 76-GTE-7 Walker, S., 47-HR-2 Shimada, T., 78-HR-3, 107-HR-5 Spurling, A., 89-SR-3 Takahashi, R., 8-ECD-1 Tsay, M., 14-EP-4, 117-SATS-1 Walock, M., 104-GTE-10 Shimazu, A., 12-EP-2 Spurrier, Z., 47-HR-2 Takahashi, Y., 78-HR-3 Tsue, M., 165-LP-15 Walter, S., 32-ABPSI-2 Shimodaira, K., 134-FFP-2 Squire, J., 132-EP-23 Takao, Y., 131-EP-22 Tsuru, K., 64-ABPSI-3 Wang, B., 55-PC-4, 125-APC-3, 166-LP-16 Shinohara, R., 165-LP-15 Sreenivas, K., 44-GTE-5 Takayasu, F., 8-ECD-1 Turan, N., 99-EP-16 Wang, D., 64-ABPSI-3 Shiraki, S., 56-PC-5 Srikanth, P., 51-LP-6 Takegahara, H., 131-EP-22 Turner, J., 106-GTE-12 Wang, G., 116-PC-11 Shirotori, K., 174-SR-6 Srinivasan, B., 37-EP-6 Talamantes, G., 24-LP-2 Tussiwand, G., 49-LP-4 Wang, J., 81-HSABP-6, 86-PC-6, 124-ADP-2, 125-APC-3, Shitta, M., 66-ECD-2 Stahl, J., 138-HR-7 Talley, D., 166-LP-16 Uchiumi, M., 143-LP-14 129-EP-20, 136-GTE-14 Short, J., 4-ADP-1 Stanley, S., 24-LP-2 Tanaka, M., 8-ECD-1 Ueda, S., 48-HSABP-4 Wang, N., 172-PP-1 Shotwell, R., 19-HR-1, 138-HR-7 Starikovskiy, A., 163-HSABP-10 Tang, H., 69-EP-10, 161-GTE-19 Uhl, D., 66-ECD-2 Wang, P., 174-SR-6 Shouse, D., 116-PC-11 Stark, R., 50-LP-5 Tangirala, V., 81-HSABP-6 Ullrich, W., 26-PC-1 Wang, T., 113-NFF-4 Shukla, H., 117-SATS-1 Starkey, R., 32-ABPSI-2, 64-ABPSI-3 Tani, K., 80-HSABP-5 Umemura, Y., 84-LP-9 Wang, V., 143-LP-14 Shukla, P., 117-SATS-1 Staschus, C., 68-EDU-2 Tarau, C., 29-TM-1, 58-TM-2, 90-TM-3, 148-TM-5 Unni, V., 45-GTE-6 Author/Session Chair Index Wang, Y., 80-HSABP-5, 110-HSABP-8, 118-SR-4, Xin, F., 159-GTE-17 Zhang, M., 22-HSABP-3, 160-GTE-18 160-GTE-18 Xinxin, F., 165-LP-15 Zhang, S., 125-APC-3 Wang, Z., 22-HSABP-3, 95-APC-2, 160-GTE-18 Xu, G., 172-PP-1 Zhang, X., 22-HSABP-3, 64-ABPSI-3, 95-APC-2, Warwick, R., 7-APS-1 Xu, X., 21-HSABP-2, 104-GTE-10 160-GTE-18, 172-PP-1 Washington, M., 142-LP-13 Xu, Y., 90-TM-3, 161-GTE-19 Zhang, Y., 78-HR-3 Watanabe, H., 39-EP-8, 69-EP-10, 130-EP-21, Xue, X., 45-GTE-6 Zhang, Z., 90-TM-3 131-EP-22 Xuele, Q., 124-ADP-2 Zhao, Y., 21-HSABP-2, 55-PC-4 Watanabe, T., 65-AEP-2 Yada, K., 143-LP-14 Zhao, Z., 104-GTE-10, 106-GTE-12, 158-GTE-16 Watts, D., 26-PC-1 Yager, J., 111-ITAR-2 Zheng, L., 159-GTE-17 Watts, O., 5-AEC-1 Yakovlev, V., 17-GTE-1 Zhou, L., 95-APC-2, 160-GTE-18 Webster, G., 140-ITAR-3 Yamada, H., 134-FFP-2 Zhu, H., 78-HR-3 Webster, R., 44-GTE-5 Yamamoto, N., 53-NFF-1, 156-EP-26 Zhu, K., 27-PC-2, 174-SR-6 Webster, S., 115-PC-10 Yamashita, M., 138-HR-7 Zhu, S., 161-GTE-19 Wei, S., 47-HR-2 Yan, D., 64-ABPSI-3 Zhu, W., 136-GTE-14 Wei, X., 64-ABPSI-3, 118-SR-4 Yan, T., 171-PC-16 Ziemba, T., 72-EP-13 Wekerle, T., 118-SR-4 Yanes, N., 12-EP-2, 154-EP-24 Ziemer, J., 73-EP-14 Werling, L., 168-LP-18 Yang, C., 21-HSABP-2 Zink, G., 4-ADP-1 West, J., 25-LP-3 Yang, F., 95-APC-2 Zips, J., 146-PC-13 White, B., 7-APS-1 Yang, H., 25-LP-3 Ziraman, B., 174-SR-6 White, H., 132-EP-23 Yang, L., 67-ECS-2, 127-ECS-3 Zizin, A., 56-PC-5 Whitmore, S., 47-HR-2, 107-HR-5, 108-HR-6, 162-HR-8 Yao, J., 136-GTE-14 Zumberge, J., 148-TM-5 Whittaker, J., 127-ECS-3 Yao, W., 81-HSABP-6 Zwahlen, J., 14-EP-4, 117-SATS-1 Wilhelm, B., 7-APS-1 Yarnot, V., 142-LP-13 Williams, E., 76-GTE-7 Yasuda, K., 108-HR-6

84 Williams, G., 53-NFF-1, 70-EP-11, 129-EP-20, Yasukochi, H., 79-HR-4 154-EP-24 Yavor, Y., 153-EE-2 Williams, S., 102-EP-19, 140-ITAR-3 Yeboah, S., 90-TM-3 Wills, D., 172-PP-1 Yedavalli, R., 94-AEC-2 Wilson, D., 8-ECD-1, 136-GTE-14 Yellapantula, S., 87-PC-7 Wilson, S., 66-ECD-2, 151-ECD-3 Yershov, S., 17-GTE-1 Winglee, R., 72-EP-13 Yildiz, M., 132-EP-23 Wirz, R., 14-EP-4, 100-EP-17, 101-EP-18 Yim, J., 11-EP-1, 98-EP-15, 129-EP-20, 154-EP-24 Wisniewski, C., 150-ABPSI-5 Yokoi, T., 79-HR-4 Witte, J., 139-HSABP-9 Youngblood, S., 168-LP-18 Wojnarska, S., 97-EE-1 Yu, H., 159-GTE-17 Wolff, M., 17-GTE-1, 66-ECD-2, 119-TM-4, 148-TM-5, Yu, J., 159-GTE-17, 160-GTE-18 161-GTE-19 Yu, X., 118-SR-4 Wolford, D., 126-APS-4 Yu, Z., 32-ABPSI-2 Wong, K., 104-GTE-10 Yuan, Y., 90-TM-3 Woods, A., 127-ECS-3 Yuanchi, Z., 159-GTE-17 Wrosch, M., 58-TM-2 Yue, L., 64-ABPSI-3 Wu, J., 47-HR-2 Yumusak, M., 174-SR-6 Wu, T., 104-GTE-10 Yungster, S., 18-GTE-2 Wu, X., 21-HSABP-2 Yıldırım, A., 93-ABPSI-4 Wu, Z., 172-PP-1 Zawati, H., 158-GTE-16 Wulfkuehler, J., 85-NFF-3 Zeineldin, R., 4-ADP-1 Xia, C., 22-HSABP-3, 90-TM-3 Zein-Sabatto, S., 94-AEC-2 Xia, Q., 39-EP-8, 172-PP-1 Zhang, C., 55-PC-4 Xiao, Q., 171-PC-16 Zhang, F., 125-APC-3 Xiaolin, S., 160-GTE-18 Zhang, H., 125-APC-3, 166-LP-16 Xie, K., 39-EP-8, 172-PP-1 Zhang, J., 171-PC-16 Xie, N., 160-GTE-18 Zhang, L., 160-GTE-18 IntroNotes

www.aiaa-propulsionenergy.org 36 #aiaaPropEnergy IntroVenue Map

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www.aiaa-propulsionenergy.org 37 #aiaaPropEnergy 10–12 JULY 2017 ATLANTA, GA Mark Your Calendar and Plan to Attend!

In 2017, hundreds of thought leaders and cutting- edge engineers will congregate in Atlanta, Georgia, to discuss the innovations happening in the fields of aerospace propulsion, power, and energy. Mark your calendar and plan to attend the AIAA Propulsion and Energy Forum 10–12 July.

See You Next Year at the Hyatt Regency Atlanta!

The Call for Papers will be available in October 2016 aiaa-propulsionenergy.org

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