Leveraging Technology Synergies to Realize the Promise of Interdependent Systems

28–30 JULY 2014 CLEVELAND, OH

FINAL PROGRAM www.aiaa-propulsionenergy.org #aiaaPropEnergy

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Phil Burkholder Michael Heil We will explore the forum’s theme “Leveraging technology synergies to realize the promise of interdependent systems,” through penetrating discussions across a diverse Rolls-Royce Ohio Aerospace Institute array of areas, including: advanced technology architectures, systems management and development, the impact of technology on manufacturing, platforms, and future systems, and research and technology. We will ask not only what the “art of the possible” is in each of those areas, we will also hear from end-users about the real- world challenges and barriers that must be overcome to continue to evolve the state of the art in propulsion and energy technology and theory.

Beyond our plenary sessions, we will tackle a diverse set of integrated topics, including: the future of energy systems, opportunities and challenges of the nexus of John Kinney Christian Mari aviation, aerospace and propulsion technology, high energy and power technologies, GE Aviation SAFRAN Group advanced manufacturing technologies for propulsion and energy systems, compressing the development timeline for energy systems, and sustainable energy – among many more.

We will also take time this week to celebrate our community’s achievements. From celebrating the history of Lockheed Martin’s Skunk Works©, to examining the 70 years of propulsion technology contributions made by NASA Glenn Research Center, we will take time out to remember that the roots of our community are strong and well developed. We will celebrate new achievement, honoring four individuals whose Richard Stulen Woodrow work has shaped propulsion systems and technology as we know them. We will Whitlow, Jr. also take time to honor the 50th anniversary of the Joint Propulsion Conference, Sandia National Laboratories (retired) NASA (retired) acknowledging AIAA’s long-term commitment to providing the best forum possible for advancing the future of propulsion and energy systems.

Thank you for making the choice to attend AIAA Propulsion and Energy 2014! We are confident that this event will provide you with the best possible mix of representatives from all areas of the propulsion and energy community, the most dynamic range of topics, and an atmosphere conducive to promoting the teamwork and collaboration necessary to keep our technology generating crucial lift for the entire aerospace enterprise.

50th AIAA/ASME/SAE/ASEE Joint AIAA Propulsion and Energy Propulsion Conference 2014 is proud to feature the 12th International Energy Conversion following conferences: Engineering Conference IEEE/INCOSE EnergyTech 2014

www.aiaa-propulsionenergy.org 3 #aiaaPropEnergy IntroOrganizing Committee Forum Organizing Committee Technical Program Committee Hybrid Rockets Madhan Bala, SPG Forum General Chair Forum Technical Program Chair Liquid Propulsion Michael Heil, Ohio Aerospace Institute George Williams, Ohio Aerospace Justin Locke, United Technologies Forum Technical Chair Institute Research Center George Williams, Ohio Aerospace Forum Deputy Technical Chair – Energy Nuclear and Future Flight Propulsion Institute Simon Liu, The Aerospace Corporation Greg Meholic, The Aerospace Integration Chair Forum Deputy Technical Chair – Space Corporation David Eames, Rolls-Royce Corporation David Jacobson, NASA Glenn Research Propellants and Combustion Education Chair Center Joe Oefelein, Sandia National Laboratory Charles Cross, Wright-Patterson Air Forum Deputy Technical Chair – Aviation Propulsion Education Force Base Gerard Welch, NASA Glenn Research Robert Frederick, University of Alabama International Chair Center in Huntsville Christian Mari, SAFRAN Group Aerospace Power Systems Solid Rockets Doug Allen, retired Public Policy Chair Wes Ryan, United Launch Alliance Advanced Propulsion Concepts Carol Cash, Carol Cash & Associates Space and Earth-to-Orbit Vehicles Systems John Robinson, retired Member Engagement Chair Leo Daniel, University of New Orleans Essam Khalil, Cairo University Air Breathing Propulsion Systems Integration System Concepts and Supporting Propulsion Young Professional Chair Christopher Hughes, NASA Glenn Technologies Research Center Christine Pastor-Barsi, Sierra Lobo Corinne Gatto, Jet Propulsion Energetic Components and Systems Laboratory Recognition Chair Brian Smith, Pacific Scientific Energetic Terrestrial Energy Systems Sivaram Gogineni, Spectral Energies, Materials Company LLC Charles Alexander, Cleveland State Energy Conversion Device Technology University Exposition Chair Ed Lewandowski, NASA Glenn Research Art Mallett, Dunmore Corporation Center Social Media Chair Energy Policy, Environmental & Historical Nayo Martinez, Parametric Solutions, Inc. Perspective And Thermal Management Technology Technical Integration Chair Mike Piszczor, NASA Glenn Research Mike Piszczor, NASA Glenn Research Center Center Energy Storage Technology Society Representatives Simon Liu, The Aerospace Corporation ASME Energy Systems Models and SE Life-Cycle John Robinson, retired Management ASEE John Juhasz, retired Robert Frederick, University of Gas Turbine Engines Alabama, Huntsville Gerard Welch, NASA Glenn Research INCOSE Center John Juhasz, retired Green Engineering Ray Beach, NASA Glenn Research Rubin Del Rosario, NASA Glenn Center Research Center IEEE High Speed Air Breathing Propulsion Charles Alexander, Cleveland State Tim O’Brien, Aerojet Rocketdyne University www.aiaa-propulsionenergy.org 4 #aiaaPropEnergy IntroContents

Welcome 3

Organizing Committee 4

Forum Overview 6

Sponsors and Supporters 8

Keynote Speakers and Plenary Sessions 9

Forum 360 11 www.twitter.com/aiaa

Special Sessions – IEEE/INCOSE EnergyTech 16 www.facebook.com/AIAAfan

Special Events 19 www.youtube.com/AIAATV

Networking Events 20 www.linkedin.com/companies/aiaa

Educational Events 21 www.flickr.com/aiaaevents

Recognition Events 22 www.google.com/+aiaaorg

Exposition Hall 24 new.livestream.com/AIAAVideo/ PropEnergy2014 Exhibitors 26

General Information 30 Join the conversation! #aiaaPropEnergy Author and Session Chair Information 32

On-Site Wi Fi Information Sponsored by: ITAR Information 33 Network Name: PE-Cleveland Password: PropEnergy 14 Committee Meetings 34

Sessions at a Glance 35 AIAA is the world’s largest technical society dedicated Session Detail Matrix 41 to the global aerospace profession. With more than 35,000 individual members worldwide, and one hundred corporate members, AIAA brings together industry, Author and Session Chair Index 93 academia, and government to advance engineering and science in aviation, space, and defense. www.aiaa.org Venue Map 101 www.aiaa-propulsionenergy.org 5 #aiaaPropEnergy IntroForum Overview

MONDAY TUESDAY WEDNESDAY 28 July 29 July 30 July 0800 hrs Plenary Panel Keynote Address Keynote Address 0830 hrs

Networking Break w/pastries in Exposition Hall Networking Break w/pastries in Exposition Hall Networking Break w/pastries in Exposition Hall 0900 hrs Speakers’ Briefings in Technical Session Rooms (am & pm sessions) Speakers’ Briefings in Technical Session Rooms (am & pm sessions) Speakers’ Briefings in Technical Session Rooms (am & pm sessions)

0930 hrs

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

1130 hrs

1200 hrs Luncheon Break Luncheon Reception in Exposition Hall 1230 hrs Forum Awards Luncheon

1300 hrs Exposition Exposition 1330 hrs Plenary Panel Plenary Panel Hall Open Hall Open 1400 hrs Plenary Panel

1430 hrs Networking Break in Exposition Hall Networking Break in Exposition Hall

1500 hrs Exposition Exposition Hall Open Hall Open 1530 hrs Technical and Technical and 1600 hrs Corporate Forum 360 Poster Sessions Poster Sessions Forum 360 Forum 360 Member Exhibit Technical and 1630 hrs Reception Poster Sessions 1700 hrs

1730 hrs

1800 hrs Keynote Address 1830 hrs Reception in Exposition Hall

1900 hrs

1930 hrs Nuclear and Rising Leaders: Future Flight Brand Yourself 2000 hrs Evening Session Rising Leaders 2030 hrs Town Hall 2100 hrs

2130 hrs

www.aiaa-propulsionenergy.org 6 #aiaaPropEnergy IntroForum Overview Plenary Panels and Keynotes Get the big picture on propulsion and energy from the thought leaders in the field during these high-level discussions and presentations. From perspectives on the future of propulsion and energy, to advanced manufacturing solutions for propulsion and energy systems—you’ll get the latest from elite leaders in the field. Forum 360 These conversations with experts will cover a spectrum of timely topics including programs, systems, policy, operations, applications, platforms and more! Delve deep into subjects like hybrid electric propulsion systems, additive manufacturing, and assuring critical system behavior—just to name a few. Technical Program This is the nuts and bolts, quite literally. Check out the latest in propulsion and energy research and development from more than 500 papers presented in over 20 technical tracks. This week you will:

u Present recent advances before a knowledgeable international audience u Educate customers and providers on the latest research and product developments u Learn about the latest technology and research in the field from industry experts u Discover what lies ahead as senior industry leaders discuss their program and business challenges during keynote and panel sessions u Network to engage new contacts and refresh old ones u Recognize significant achievements from within the community

www.aiaa-propulsionenergy.org 7 #aiaaPropEnergy IntroSponsors and Supporters

AIAA would like to thank the following organizations for their support of AIAA Propulsion and Energy 2014

Executive Sponsors

Additional Sponsors

Co-Sponsors

Media Sponsor

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note please see this link about placement of ® http://wiki.answers.com/Q/Where_is_the_proper_placement_of_the_registered_trademark_symbol www.aiaa-propulsionenergy.org 8 #aiaaPropEnergy

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recommended minimum on business card 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, 28 July Tuesday, 29 July

0800-0900 hrs Grand Ballroom A 0800-0900 hrs Grand Ballroom A Perspectives on the Future of Propulsion & Energy Keynote – The Art of the Possible Future Trends, Opportunities and Senior propulsion and energy leaders will discuss some of Challenges at the Nexus of Aviation, the most pressing future challenges and share their thoughts on where propulsion and energy technology is headed in the Aerospace and Energy coming decades. The group will also address how increasing Alton Romig, Vice President, Engineering interdependencies between propulsion and energy systems will and Advanced Systems, Lockheed Martin impact future developments. Aeronautics Alton Romig will share his ideas on the future of high energy Moderator: James Free, Center Director, NASA John H. Glenn and power technologies and how the growing demands on these Research Center systems will influence the design of future aerospace vehicles. Panelists: Eric Bachelet, Executive Vice President, Research and 1300-1430 hrs Grand Ballroom A Technology, SAFRAN James Maughan, Technical Director for Aero Thermal and High Energy & Power Technologies – The View Mechanical Technologies, GE Global Research from Users Richard Parker, Director of Research & Technology, Government and industry experts will explore the synergies Rolls-Royce plc between emerging energy technologies in the aerospace and transportation sectors. The current state of these technologies 1300-1430 hrs Grand Ballroom A and evolving trends across different sectors will also be discussed.

Perspectives on the Future of Propulsion & Energy Moderator: Richard Stulen, Vice President (ret), Sandia – The View from Users National Laboratories Executives from leading aircraft and space vehicle manufacturers will build off the morning plenary to discuss how advances Panelists: in future propulsion and energy systems will benefit next- Pierre-Guy Amand, Director Engineering and Economics, generation aerospace platforms. SAFRAN Sunita Satyapal, Director, Fuel Cell Technologies Office, Energy Moderator: Graham Warwick, Managing Editor, Technology, Efficiency and Renewable Energy, U.S. Department of Energy Aviation Week Rickey Shyne, Director, Research and Engineering Directorate, Panelists: NASA Glenn Research Center Gary Smyth, Executive Director, North American Science Labs John Henderson, Lockheed Martin Fellow, Space Propulsion, Global Research and Development, General Motors Company Lockheed Martin Corporation Leslie Kovacs, Director, United Launch Alliance James Petersen, Vice President/Senior Chief Engineer, Propulsion Systems Division, Boeing Commercial Airplanes Sebastien Remy, Senior Vice President, Head of Airbus Group Innovations, Airbus Group

(continued)

www.aiaa-propulsionenergy.org 9 #aiaaPropEnergy Keynote Speakers and Plenary Sessions

Tuesday, 29 July (continued) Wednesday, 30 July

1800-1900 hrs Grand Ballroom A 0800-0900 hrs Grand Ballroom A

History of the Skunk Works© Keynote Alton Romig, Vice President, Engineering and Advanced Systems, Lockheed Martin Advanced Manufacturing Solutions Aeronautics for Propulsion and Energy Systems – e Art of the Possible Greg Morris, Additive Strategy and Business Development Manager, Known for their ability to rapidly solve even the most daunting GE Aviation challenges, employees of the Skunk Works have supported the missions of their customers for more than 70 years. That singular A leading expert from the additive manufacturing community focus has led to some of the most significant achievements in will share his thoughts on how new manufacturing techniques aerospace to include the first Mach 2 fighter, the highest-flying and technologies are revolutionizing the design and production single engine aircraft, the first (and only) operational Mach 3 of propulsion and energy systems. aircraft, the first stealth aircraft, and the first operational Mach 3 stealthy unmanned aircraft. The contribution of these Lockheed Martin Skunk Works’ 1330-1500 hrs Grand Ballroom A projects to peace, stability and prosperity for the United States and its allies is one reason why it is the only aerospace company Advanced Manufacturing Solutions for Propulsion in history to receive the National Medal of Technology and Innovation. Join Alton Romig for a discussion of the Skunk and Energy Systems – The View from Users Works approach and how it enables the men and women who Representatives from leading manufacturers of aerospace work there to continue to redefine what is possible systems will discuss how their organizations are utilizing Join us learn and about the exciting history of Lockheed Martin advanced manufacturing today and how new advancements will Skunk Works! impact their processes in the future. Moderator: Christine Furstoss, Global Technology Director, Manufacturing & Materials Technologies, GE Global Research

Panelists: Jerrol (Jay) Littles Jr., Director of Advanced Launch Propulsion Programs, Aerojet Rocketdyne Edward Morris, Director, America Makes - National Additive Manufacturing Innovation Institute Vice President, National Center for Defense Manufacturing and Machining (NCDMM) Homer “H.D.” Stevens, Chief Engineer, STAR Labs, Lockheed Martin Space Subsystems, Space Technology Advanced R&D Labs Tom Williams, Manager, Propulsion Division, NASA Marshall Space Flight Center

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

0930-1200 hrs Room 26B Compressing the Technology Development and Transition Timeline This session will discuss ways to expedite technology development, maturation, and transition via a series of interviews and audience Q&A sessions. Topics will address tomorrow’s key technologies, technology maturation and validation, and rapid transition to products. Interviewer: Alan Epstein, Vice President, Technology and These conversations will cover a spectrum of Environment, Pratt & Whitney timely topics including programs, systems, policy, Interviewees: operations, applications, platforms and more! Ed Greitzer, H.N. Slater Professor of Aeronautics and Astronautics, Massachusetts Institute of Technology Monday, 28 July Thomas Irvine, Deputy Associate Administrator, Aeronautics Research Mission Directorate, NASA Headquarters 0930-1200 hrs Room 26A Interviewer: Anthony Dean, Technology Leader - Combustion Systems, GE Global Research A Future with Hybrid Electric Propulsion Systems Interviewees: —Opportunities and Challenges Scott Cruzen, Vice President Advanced Design Technology, This panel session will review recent progress and future Williams International Co., LLC prospects for hybrid electric propulsion systems for aircraft Tom Fetterhoff, Technical Director for Test Operations, AEDC applications. Topics to be addressed will include discussion on Interviewer: Theodore Fecke, Retired USAF Senior Leader for nearer term opportunities for ground and small-scale flight Propulsion, Universal Technologies Corp. demonstrations leading to longer term applicability of the technology for larger commercial transports. Interviewees: Moderators: Ruben Del Rosario, NASA Glenn Research Center Keith Leverkuhn, Vice President, Boeing Commercial Airplanes Nateri Madavan, NASA Glenn Research Center James Newhouse, Chief, Propulsion Acquisition Division, Air Force Panelists: Materiel Command Marty Bradley, Technical Fellow, Boeing Commercial Airplanes 1500-1800 hrs Room 26A Kevin Daffey, Global Head of Electrical Power and Control Systems, Rolls-Royce plc Assuring Critical System Behavior in an Era of Neil Garrigan, Executive Manager, Aviation Advanced Technology, GE Aviation Increasing Complexity and Change John Nairus, Chief Engineer, Power and Controls Division, Air As power and energy systems continue to increase in complexity, the challenges of meeting full stakeholder objectives of achieving Force Research Laboratory desirable “system behavior” while assuring compliance with safety and environmental laws continue to grow. This panel will focus on the critical aspect of system behavior, examining the relevance and interaction of each component within a system to influence overall behavior and achieve desired outcomes. Such an “integrated” perspective is at the core of systems engineering methodology, essential to avoid risks and exploit opportunities throughout the system life cycle. Moderator: John Thomas, INCOSE International (former) President, John A. Thomas & Associates, LLC Panelists: Don Burns, Head of Innovation Systems Engineering, Rolls-Royce Corporation Eric Gebhardt, Chief Technology Officer and Vice President Engineering, GE Oil & Gas David Long, President and CEO, Vitech Corp Paul Nielsen, CEO, Software Engineering Institute Greg Pannone, President, Controltec Analytics Jon Wade, Professor, Stevens Institute of Technology (continued) www.aiaa-propulsionenergy.org 11 #aiaaPropEnergy ForumIntro 360

Monday, 28 July (continued) Tuesday, 29 July

1500-1800 hrs Room 26B 0930-1200 hrs Room 26A JPC 50th Anniversary Pioneers Session: Educating The Next Generation of Propulsion Celebrating the Past, Inﬂuencing the Future Engineers — Are Changes Needed to Better In this session we will celebrate 50 years of the Joint Propulsion Prepare the Future Workforce? Conference. Pioneers from industry, government, and With the advent of new technologies, the college engineering academia will share their experiences and discuss how their curriculum has always changed to keep up with the demands achievements will influence the next generation of aerospace placed on young engineers. But as the curriculum has changed, history. Following this portion of the program, several young have we forgotten something important? A panel of educators professionals will interview the speakers and take questions and leaders from government, industry, and universities will from the audience. discuss the skills that are needed to be successful in today’s Moderator/Emcee: Theodore Fecke, Retired USAF Senior environment and identify critical shortfalls or areas that they Leader for Propulsion, Universal Technologies Corp. see as lacking in the preparation of young engineers. Interviewers: Moderator: Nicholas Garafolo, Assistant Professor, Mechanical Lance Foster, NASA Glenn Research Center Engineering, University of Akron Zachary Grunder, Lockheed Martin Corporation Panelists: Participants: Lisa Teague, Director, Research and Technology, Rolls-Royce Mike Benzakein, Director, Executive Partnerships in Aerospace, Corporation Aviation, and Flight, The Ohio State University Dimitri Mavris, Director, ASDL, Georgia Tech Ed Greitzer, H.N. Slater Professor of Aeronautics and Mike Benzakein, Director, Executive Partnerships in Aerospace, Astronautics, Massachusetts Institute of Technology Aviation, and Flight, The Ohio State University Jim Johnson, Belcan Jose Camberos, Senior Research Aerospace Engineer, Air Force Joe Nieberding, NASA (retired) Research Laboratory Lawrence Ross, NASA (retired) Paul Orkwis, Department Head and Professor of Aerospace Tony Strazisar, NASA (retired) Engineering and Engineering Mechanics, University of Cincinnati

0930-1200 hrs Room 26B Advanced Terrestrial Energy Technologies: Generation, Storage, Distribution Recent years have seen enormous shifts in energy usage, generation and outlooks. Renewables have increased in penetration dramatically, led by photovoltaics. Low cost natural gas is reaching the market, offsetting pollutants from traditional generation. The greater penetration of renewables leads to several technological challenges, including the widescale generation, distribution, and storage of energy and efficient usage on the next grid. Moderator: Timothy J. Peshek, Research Professor of Materials Science and Engineering, Case Western Reserve University Panelists: Robert Savinell, George Dively Professor of Chemical Engineering, Case Western Reserve University Ina T. Martin, Director of Operations, Materials for Optoelectronic Research and Education (MORE) Center, Case Western Reserve University James Soeder, Senior Technologist for Power, NASA Glenn Research Center Emily Pentzer, Professor of Chemistry, Case Western Reserve University (continued) www.aiaa-propulsionenergy.org 12 #aiaaPropEnergy IntroForum 360

Tuesday, 29 July (continued) Wednesday, 30 July

1500-1800 hrs Room 26A 0930-1200 hrs Room 26A Implementation, Utilization, and Coordination Additive Manufacturing: A Holistic View—From of Advanced Energy Concepts Within the Education, Design, Research, and Production Government and Department of Defense What the can the aerospace industry learn from the new Given the reliance of the modern warfighter on advanced centers for manufacturing innovation launched by the U.S. technology, the need for lightweight, highly efficient power Department of Commerce? Panelists representing a broad sources is greater than ever for the military. Advanced industry cross-section will join representatives of the newly battery technology, photovoltaics, advanced fuels, etc., have created institutes to discuss the U.S. plans to recapture taken on ever-increasing roles within the Department of America’s lead in manufacturing innovation. Defense. This reliance on efficient, low-cost power systems Moderator: David Salay, Consultant, Ohio Aerospace Institute has increased the need for coordination and collaboration on Panelists: advanced technology between the DoD and other government agencies. This panel session will consist of a number of short Lawrence Brown, Executive Director, American Lightweight presentations from representatives of the various agencies Materials Manufacturing Innovation Institute (ALMMII) followed by a panel discussion and questions from the Dan Hartman, DMDI Representative, Rolls-Royce Corporation audience. Topics discussed will include research in advanced Larry Knauer, President, HSSE, Inc. power generation technology, system requirements, planned implementation, and coordination activities for these advanced Terri Burgess Sandu, Director, Entrepreneurship Innovation technologies. Institute, Executive Director, Workforce, Lorain County College Moderator: Michael F. Piszczor, Jr., Chief, Photovoltaic and Tim Shinbara, Technical Director, Association for Electrochemical Systems Branch, NASA Glenn Research Center Manufacturing Technology Panelists: Randall Furnas, Chief, Power Division, NASA Glenn Research 0930-1200 hrs Room 26B Center Phillip Jenkins, Senior Technologist, Naval Research Laboratory Keeping It Going: Sustainability and Growth in Evan O. Jones, Manager, Energy and Environment for National Technology and Workforce Security, Pacific Northwest National Laboratory This session will discuss the underlying factors that can impact John Nairus, Chief Engineer, Power and Controls Division, Air the technology development and transition process, including Force Research Laboratory risk aversion; apathy with regard to the national benefits of aerospace; declining investments that impede our ability to 1500-1800 hrs Room 26B develop, test, and mature key technologies adequately; and our inability to inspire and energize the workforce of tomorrow. 70 Years of Aero Propulsion Research at NASA The session will also discuss policy changes that can help Glenn Research Center mitigate these factors. Moderator: Mark Lewis, Director, Science and Technology A historical perspective on aero propulsion research conducted Policy Institute at NASA Glenn Research Center over the past 70 years will be presented, with emphasis on research related to engine noise, Panelists: combustion, CFD, controls, materials and structures, and Christopher Singer, Director of Engineering, NASA Marshall sensors and instrumentation. Space Flight Center Moderator: Dhanireddy Reddy, NASA Glenn Research Center Jerrol (Jay) Littles Jr., Director of Advanced Launch Propulsion Presenters: Programs, Aerojet Rocketdyne Neil Garrigan, Executive Manager, Aviation Advanced Clarence Chang, NASA Glenn Research Center Technology, GE Aviation Dennis Huff, NASA Glenn Research Center Sanjay Garg, NASA Glenn Research Center Larry Matus, NASA Glenn Research Center Ajay Misra, NASA Glenn Research Center Louis Povinelli, NASA Glenn Research Center

(continued) www.aiaa-propulsionenergy.org 13 #aiaaPropEnergy IntroForum 360

Wednesday, 30 July (continued) 1500-1800 hrs Room 26B 70 Years of Power and Space Propulsion at NASA 1500-1800 hrs Room 26A Glenn Research Center Energy Trends and Their Implications on A historical perspective on power and space propulsion Advanced Technology research conducted at NASA Glenn Research Center over the past 70 years will be presented, with emphasis on research Today’s energy landscape is complicated by increasing energy related to electrical, chemical and nuclear propulsion, demands, the push for increased energy efficiency, and the cryogenic propellants, direct energy conversion, and introduction of advanced energy technology. These challenges electrochemical and energy storage. have varying implications from industry, government, and Moderator: George Schmidt, NASA Glenn Research Center regional perspectives. Panelists will address the current energy situation, future trends, and potential plans from their Presenters: organization’s perspective. Stanley Borowski, NASA Glenn Research Center Moderator: Matt Moran, Sector Manager for Energy & Dianne Linne, NASA Glenn Research Center Materials, NASA Glenn Research Center Valerie Lyons, NASA Glenn Research Center Panelists: Lee Mason, NASA Glenn Research Center Larry Viterna, President, Nautica Wind Power LLC Michael Meyer, NASA Glenn Research Center Hasso Weiland, Technical Fellow, Alcoa Advanced Technical Michael Patterson, NASA Glenn Research Center Center Concha Reid, NASA Glenn Research Center Lorry Wagner, President, LEEDCo

www.aiaa-propulsionenergy.org 14 #aiaaPropEnergy ForumIntro 360

Sponsored by: AIAA’s Rising Leaders in Aerospace Forum is a special initiative taking RISING place during Propulsion and Energy 2014 that provides a forum for inLEADERS young aerospace leaders, age 35 and under, to learn from and engage AEROSPACE with others.

Monday, 28 July Tuesday, 29 July

1930-2130 hrs Room 5 1900-2030 hrs Room Town Hall: Where’s MY Apollo Vision for the “Brand Yourself” Future? Engineers need to think of themselves not just as an individual, These professionals will be fielding YOUR questions: What but as a brand. Today, an engineer’s brand is both virtual and is the future of propulsion? What are the cutting-edge in person. Come to the Rising Leaders event “Brand Yourself” technologies in space propulsion? What is happening that can where branding specialist Brad Owen of Creavos will talk motivate me or my colleagues? about how to manage your brand. Come prepared with questions as the panel will have a 60- minute Q&A session dedicated solely to answering your questions. If you would like, or prefer, you may forward your questions ahead of time. Questions can be sent to Stephen Brock, AIAA Program Manager, Students and Young Professional, at [email protected] and Christine Pastor-Barsi, Panel Moderator, at [email protected]. Moderator: Christine Pastor-Barsi, Sierra Lobo, Inc. Panelists: Curtis Johnson, Blue Origin Mike Kynard, NASA Marshall Space Flight Center Robyn Ringuette, Virgin Galactic Jeff Thornburg, SpaceX

www.aiaa-propulsionenergy.org 15 #aiaaPropEnergy IntroSpecial Sessions – IEEE/INCOSE EnergyTech

Monday, 28 July

0930–1200 hrs Room 24 1500–1800 hrs Room 24 Advancing Technology Impacts in Energy and Meeting Education Demands of Future Energy Transportation Systems Panel 1: Advancing Terrestrial and Space Panel 1: Power & Energy Systems: A Transformative Power Generation Approach to Education This panel plans to cover thermal energy and electric power Students working on undergraduate and graduate degrees in production issues facing our nation and the world over the next the area of power and energy systems have been taught the same decades, with relevant technologies ranging from near term to way for decades. With the movement toward more diverse, mid- and far term. distributed and advanced power generation such as liquid fluoride thorium nuclear reactors, fracking, geothermal, solar, Although the main focus will be on ground-based plants to wind, and in conjunction with smart grids, the entire educational provide baseload electric power, energy conversion systems process needs to be assessed and revised. This panel will explore (ECS) for space, with solar- or nuclear energy sources for output this and respond with suggested changes that need to be made. power levels ranging tens of Watts to kilo-Watts for unmanned An example of a change that needs to occur is the addition of spacecraft, and eventual mega-Watts for lunar outposts and one or more required courses in systems engineering at both planetary surface colonies, are also included. Implications the undergraduate and graduate levels that can better prepare of these technologies on future terrestrial energy systems, students for future engineering challenges. The panel will combined with advanced fracking, Thorium-based reactors, and include representative from industry and government, as well as nuclear fusion, will also be considered by the panelists. academics. The characteristics of the above mentioned ECS will be Moderator: Chuck Alexander, Cleveland State University described, both in terms of their overall energy utilization effectiveness and also with regard to climactic effects due to Panelists: exhaust emissions. Michael Ahern, WPI / Power Systems Moderator: Al Juhasz, NASA Glenn Research Center Sridhar Kota, FlexSys Inc. / University of Michigan (invited) Panelists: Timothy Croshore, First Energy (invited) Bill Thesling, Energy From Thorium Foundation. Roger Dyson, NIRVA NA Panel 2: 7. Power & Energy Future Directions Jason Mallinak, Babcock/Wilcox Ongoing developments in photovoltaic and wind generation, Al Juhasz, NASA Glenn Research Center electro-chemical and flywheel energy storage, geothermal through fracking, increased use of natural gas for electrical power generation, Brayton and Stirling conversion, and micro- Panel 2: Exponential Technology Development Driving grid and smart grid technologies are all of interest when Future Vehicle System Complexity considering the future state of the electric utility power system. Due to the regulatory landscape, driving complexity, rapidly Technology infusion in the electric power grid will encompass developing technological solutions, and societal/human some of these technologies through evolution, but others are factors, the potential production options for future road vehicle far more disruptive and will require significant changes for the integrated solutions comes with heightened risk. Whether electric power industry. This panel will explore the state of these viewed from the perspective of consumers, government agencies, technologies and the challenges for the utility industry and the industry, or investors, the uncertainties and ambiguities make barriers for the technology companies advocating their usage. decision making very difficult. This panel provides attendees Moderator: Ray Beach, NASA Glenn Research Center with an overview of the current state, the latest thinking and Panelists: analysis about the future vehicle system landscape from the perspective of leaders in key sectors. Jeff Landis, NASA Glenn Research Center Moderator: Andrew Smart, SAE International Joe Beno, University of Texas/ CEM Neil Snyder, National Renewable Energy Laboratory Panelists: Larry Viterna, Nautica Wind Power Paul Luskin, Ricardo Defense Systems Rick Kline, Cummins Diesel Greg Pannone, Control TEC

www.aiaa-propulsionenergy.org 16 #aiaaPropEnergy IntroSpecial Sessions – IEEE/INCOSE EnergyTech

Tuesday, 29 July 2014

0930–1200 hrs Room 24 1500–1800 hrs Room 24 Energy Evolution – Achieving Control and Energy Life-Cycle Vulnerability and Life-Cycle Sustainability Management Panel 1: The Evolving Smart Grid: Managing Risk with Panel 1: Managing the Life Cycle of Complex Systems: Hybrid Controls and Advanced Technology Using Advanced Models for Energy Decision Support The emergence of distributed energy resources, increases Of the many challenges confronting system developers in the in renewables, long distance transmission, and retirements modern era, perhaps none is more challenging than life-cycle of coal plants are changing the fundamental operating management of the “system of systems” contained within the assumptions that seasoned operators have relied on to keep energy sector. At the same time, the reliable delivery of energy the grid running. Combined with the retirement of the most continues to be a vital function on which all modern economies experienced operators, the risk of blackouts is increasing, perhaps depend. dramatically. This panel will discuss the likely extent of these This session will examine the availability of sophisticated emerging issues, as well as potential solutions, including “smart industry offerings in simulation tools and methods that provide grid” technologies. The panel will look at several opportunities effective life-cycle management / decision support for complex for coordination across the segments of the grid (end use, systems designers, such as the energy systems of today. Panelists distribution, transmission, and generation) to provide continued will provide a general overview and focus on the significant reliability and enhanced resiliency by utilizing hybrid control advances made in the areas of Applied Model-based SE methods schemes that allow for autonomous local actions to support in dealing with the complex systems challenges. Examples of central grid management functions. energy system models will be discussed. Moderator: Jason Black, Battelle Labs Moderator: David Long, Vitech Corp/ INCOSE Panelists: Panelists: Fred DiCenzo, Rockwell Automation Matthew Hause, Atego / PTC Ankur Ganguli, Eaton Corp Phil LePlante, Pennsylvania State University Jason Black, Battelle Labs Benjie Loop, PC Krause & Associates, Inc Sean McGervey, Johns Hopkins University/ APL (invited) Panel 2: Sustainability and Complexity in Energy Systems This panel will focus on a comprehensive review of the current Panel 2: Examining Energy System Risks and Power Grid state of alternative, sustainable energy sources and their Vulnerability projected evolution for providing effective solutions for current and future energy needs. A key element will be focusing on the The energy infrastructure in many countries is aging and realities of what is possible, both technically and economically. vulnerable to a variety of threats, both man-made and natural On one hand, the release of new IPCC reports is once again phenomena. The risks of widespread, sustained outage of igniting the debate on anthropogenic causes for climate change, electricity on modern society could be more devastating than and the resulting need to massively change our energy systems. anything that has been experienced in human civilization. This On the other hand, the development of enhanced techniques panel will examine the risks and discuss an assessment of various for directional drilling and hydraulic fracturing is opening threat scenarios and the current state of power grid challenges for up vast new reserves of natural gas, driving down prices far maintaining security and availability. It will also explore possible below the levels where many renewable energy technologies can recovery strategies in the event of grid failure and an action plan currently compete. Finally, energy production, distribution, and for national leadership. consumption must be viewed as an extremely complex system of Moderator: Frank Gaffney, Center for Security Policy systems. Panelists: Moderator: Neil Snyder, National Renewable Energy Laboratory Larry Bugh, Reliability First Corp. Panelists: James Stevens, Software Engr Institute/CMU Susan Raftery, AGROWN LLC Thom Pearce, Public Utilities Commission of Ohio (invited) Neil Snyder, National Renewable Energy Laboratory Tom Popik, Foundation for Resilient Societies (invited) Mike Pizcor, NASA Glenn Research Center

www.aiaa-propulsionenergy.org 17 #aiaaPropEnergy IntroSpecial Sessions – IEEE/INCOSE EnergyTech

Wednesday, 30 July

0930–1200 hrs Room 24 1500–1800 hrs Room 24 Regulation & Reliability in the Energy Sector Systems Engineering Electric Utilities for Resiliency Panel 1: Measuring Regulatory Impact of Recent Trends in Power and Energy Resiliency Systems Engineering Resilient Electric Utilities in a Rapidly This panel session will examine and summarize power and Changing Environment energy trends and policy outlook at the federal and state levels This panel continues the discussions from the Regulatory Panel, for the development of future domestic and global needs. The looking more deeply into the systems engineering models focus will be on resiliency in power and energy, including required to facilitate public policy success, and help measure the discussions of the impact in Ohio and nationally of hot and cold regulatory impact of measures aimed at making electric utilities weather events, plant closures, demand-response advances, and more resilient. The panelists will discuss future interoperability distributed generation in a rapidly changing market. How can of classic power systems tools with emerging risk communication a systems approach define suitable measures of policy success, models, reliability models, ecosystem impact models, maturity exposing potential unintended consequences including reduced models, and social complexity models. The ability for these tools resiliency? Panelists will also address means of providing to offset the loss of design capabilities in the power industry, ongoing assessment of actual outcomes versus regulatory intent, coupled with the new complex resiliency skills required to restore thereby establishing a framework of accountability for energy the aging infrastructure will also be examined. sector policies, using tools like value metrics and maturity modeling. Moderator: Carl Dister, Reliability First Corp. Moderator: Carl Dister, Reliability First Corp. Panelists: Rajeev Rajaram, Kent State University Panelists: Dan Kovacs, Decision Partners Beth Trumbold, Public Utilities Commission of Ohio Thom Pearce, Public Utilities Commission of Ohio Theresa Cunniff, Reliability First Corp. Brian Keaveny, NESCAUM Paul Centolella, Analysis Group Matthew Butkovic, Carnegie Mellon James Stevens, Software Engr Institute/CMU

Panel 2: Using Systems Thinking to Improve the Reliability of Power Delivery Electric power is delivered by a complex system. Occasionally, outages occur unexpectedly and can include whole regions, even in good weather! The North American Power Industry is currently working to improve service reliability by adding focus to strengthening management practices. One approach being used is to formally appraise key management practices by reviewing them through the lens of holistic Systems Thinking. This roundtable discussion will explore the application of systems thinking to improve the reliability of power delivery. Moderator: Michael Ahern, WPI / Power Systems Panelists: Don Gelosh, WPI / Systems Engineering Tim Gallagher, Reliability First Corp. Yee Chou, American Electric Power

www.aiaa-propulsionenergy.org 18 #aiaaPropEnergy IntroSpecial Events

Wednesday, June 30

0930–1130 hrs Room 13 Joint AIAA Foundation/ASME.IGTI Student Design Competition AIAA Foundation and ASME.IGTI have again teamed up to sponsor a design competition. In its third year, students from universities all over the world were asked to prepare a design report to respond to a Request for Proposal (RFP). This RFP asked students to design an engine for a supersonic business jet. To make the RFP as similar to a real-world industry as possible, a base engine was selected as a starting point for the teams. The teams then had to prepare or redesign the engine and prepare a basic airframe for the supersonic business jet. All of the responses were reviewed by technical experts from AIAA and ASME. The top three proposals are invited to the AIAA Propulsion and Energy Forum to make an oral presentation to a panel of judges. These judges will assess the design, presentation, and responses to questions. They will add their scores to those provided by the technical judges to come up with a final 1st-3rd place ranking. The final rankings will be announced at the conclusion of the session, and the teams will receive their monetary prizes after the conference has concluded. Prizes will be $2,500, $1,500, and $1,000. Please join us on Wednesday from 0930-1130 hrs in Room 13 to hear the finalists.

While you are at AIAA Propulsion and Energy 2014, don’t forget to stop by the AIAA Region III Display. This display highlights some of the Region III achievements and activities, reasons to be an AIAA member, and demonstrates the importance of involvement in your AIAA local section. We hope you stop by to check out Region III.

www.aiaa-propulsionenergy.org 19 #aiaaPropEnergy IntroNetworking Events

As the old adage says, “It’s not just what you know, it’s who you know.” Connect with those who may become your future colleagues and collaborators, employers or employees. Exchange ideas with the companies you want to partner with, and interact with the leaders who are shaping the future of aerospace.

Morning Coffee and Pastries Welcome Reception A great way to start the day and interact with colleagues A welcome reception will be held on Monday, 28 July, old and new, networking breakfasts will be offered on 1800–1930 hrs, in the Exposition Hall. Take this opportunity Monday–Wednesday, 0900–0930 hrs, in the Exposition Hall to engage new contacts and refresh old ones. A ticket for the at the Cleveland Convention Center. reception is required, and is included in the registration fee where indicated. Additional tickets may be purchased upon registration or on site, as space is available. Networking Coffee Breaks Networking coffee breaks allow even more time for making new contacts, continuing discussions from sessions, visiting the exposition hall, or checking emails and voicemails to keep in touch with the office. Networking coffee breaks will be located in the Exposition Hall on Monday and Tuesday, and in the Exposition Foyer on Wednesday at the following times: Monday, 28 July 1430–1500 hrs Tuesday, 29 July 1430–1500 hrs Wednesday, 30 July 1500–1530 hrs

www.aiaa-propulsionenergy.org 20 #aiaaPropEnergy IntroEducational Events

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

Tuesday, 29 July 0800–1700 hrs Room 25 C

1300–1700 hrs Grand Ballroom C Missile Propulsion Design, Technologies, and System Engineering Energize Tomorrow’s Engineers Today! Launch Course registration is required to attend. Students to Their STEM Future! This course is oriented toward the needs of missile engineers, Join the Northern Ohio Section at a STEM outreach event for a system engineers, system analysts, marketing personnel, group of pre-college women in Grand Ballroom C on Tuesday, program managers, university professors, and others July 29, from 1300–1700 hrs. The student participants will face working in the area of missile propulsion systems and missile a variety of engineering challenges during this outreach event, propulsion technology development. Attendees will gain an designed to energize and propel them toward STEM careers. The understanding of missile propulsion design, missile propulsion event is an open house; conference attendees are encouraged to technologies, launch platform integration, missile propulsion stop by during the afternoon program to inspire, encourage, or system measures of merit, and missile propulsion system guide the students. Or just come to observe the activities and development process. take ideas back to your own section! Stop in for a few minutes or hang out for the afternoon. 0800–1700 hrs Room 26 A Sponsored and organized by AIAA’s Northern Ohio Section. 2nd AIAA Propulsion Aerodynamics Workshop Join us at this Propulsion and Energy 2014 outreach event! Workshop registration is required to attend. The focus of the workshop will be on assessing the accuracy of Thursday, 31 July – Friday, 1 August CFD in obtaining multi-stream air breathing jet performance and flow structure to include nozzle force, vector, and moment; 0800–1700 hrs Room 25 B nozzle thrust (Cv) and discharge (Cd) coefficients; and surface pressure prediction accuracy. Experimental data are available Hybrid Rocket Propulsion for each test case, but the CFD studies will be performed as a blind trial and compared with the experimental data during Course registration is required to attend. the workshop. This short course is aimed at bringing together professionals with a mutual interest in chemical combustion and propulsion, including modern techniques for measuring hybrid rocket performance, flame and flow field modeling, testing, and stability analysis. The purpose is to present and discuss fundamental theory alongside research findings with emphasis on unsolved problems, open questions, and benchmark tests. The course will provide a platform for learning and exchanging hybrid rocket experiences in the hope of stimulating further interactions and future collaborations.

www.aiaa-propulsionenergy.org 21 #aiaaPropEnergy Recognition Events

For over 75 years, AIAA has been a champion to make sure that aerospace professionals are recognized for their contributions. AIAA salutes the very best in our industry: those individuals and teams who have taken aerospace technology to the next level…who have advanced the quality and depth of the aerospace profession…who have leveraged their aerospace knowledge for the benefit of society. Their achievements have inspired us to dream and to explore new frontiers. AIAA celebrates our industry’s discoveries and achievements from the small but brilliantly simple innovations that affect everyday lives to the major discoveries and missions that fuel our collective human drive to explore and accomplish amazing things. The following awards will be presented: Wednesday, 30 July Propellants and Combustion Award Frederick L. Dryer Professor Emeritus, Senior Scholar 1200–1330 hrs Grand Ballroom B Mechanical and Aerospace Engineering Princeton University Awards Luncheon Celebrating Achievements in Princeton, New Jersey Propulsion and Energy “For a distinguished record of technical contributions to combustion kinetics, Join with AIAA in recognizing technical and scientific surrogate fuel models, droplet combustion, excellence at the AIAA Awards Luncheon on Wednesday, 30 flow reactors, and fire safety.” July, 1200–1330 hrs, in Grand Ballroom B. A ticket for the luncheon is required, and is included in the registration fee Wyld Propulsion Award where indicated. Additional tickets may be purchased upon registration or on site, as space is available. Roger Myers Executive Director Air Breathing Propulsion Award Advanced In Space Programs Ashwani Gupta Aerojet Rocketdyne Redmond, Washington Distinguished University Professor Department of Mechanical Engineering “For sustained high-value contributions to University of Maryland propulsion for U.S. and international space College Park, Maryland systems and services to aerospace “For outstanding contributions to the propulsion communities.” understanding and development of advanced high intensity combustors for Air Breathing Propulsion Systems Integration Best Paper near zero emission high performance air breathing propulsion.” “Optimal Inlet Shape Design of N2B Hybrid Wing Body Configuration” AIAA 2012-3917, Hyoung Jin Kim, SAIC; and Energy Systems Award Meng-Sing Liou, NASA Glenn Research Center. William E. Lear Associate Professor Department of Mechanical and Electric Propulsion Best Paper Aerospace Engineering “Conducting Wall Hall Thrusters” AIAA 2013-4117, Daniel University of Florida Goebel, Richard Hofer, Ioannis Mikellides, Ira Katz, James Gainesville, Florida Polk, and Brandon Dotson, Jet Propulsion Laboratory. “For distinguished significant contributions in the energy systems field over many years, most notably in distributed generation, High Speed Air Breathing Propulsion Best Paper direct methanol fuel cells, and combustion.” “Unsteady Three-Dimensional Phenomena in Mode- Transition Simulations of the HIFiRE-2 Scramjet Flowpath,” AIAA 2013-3753, Robert Yentsch and Datta Gaintonde, The Ohio State University.

(continued) www.aiaa-propulsionenergy.org 22 #aiaaPropEnergy IntroRecognition Events

Hybrid Rockets Best Paper Nuclear and Future Flight Propulsion Best Paper “Development and Flight Testing of a Hybrid Rocket Booster “A One-Year Round Trip Crewed Mission to Mars Using for UAV Assisted Take Off,” AIAA Paper 2013-4140, Alberto Bimodal Nuclear Thermal and Electric Propulsion (BNTEP)” Bettella, Federico Moretto, Enrico Geremia, Nicolas Bellomo, AIAA 2013-4076, Laura Burke and Stanley Borowski, NASA Daniele Pavarin, and Dino Petronio, University of Padua. Glenn Research Center; and David McCurdy and Thomas Packard, Vantage Partners LLC.

Hybrid Rockets Best Student Paper Propellants and Combustion Best Paper “Mass Flow Rate and Isolation Characteristics of Injectors for Use with Self-Pressurizing Oxidizers in Hybrid Rockets,” “Thermo-Acoustic Coupling in Swirl-Stabilized Flames with AIAA 2013-3636, Benjamin S. Waxman, Brian J. Cantwell, and Helical Vortices” AIAA 2013-3650, Vincent Caux-Brisebois Jonah E. Zimmerman, Stanford University; and Greg Zilliac, and Adam Steinberg, University of Toronto; and Christophy NASA Ames Research Center. Arndt and Wolfgang Meier, DLR.

Liquid Propulsion Best Paper Solid Rockets Best Paper “Passive Phase Separation in Cryogenic Upper Stage Tanks,” “Electric Solid Propellants: A Safe, Micro to Macro Propulsion AIAA 2013-3905, Philipp Behruzi, Jorg Klatte, and Gaston Technology,” AIAA 2013-4168, Wayne Sawka and Netter, Astrium Space Transportation. Michael McPherson, Digital Solid State Propulsion.

www.aiaa-propulsionenergy.org 23 #aiaaPropEnergy IntroExposition Hall

Corporate AIAA Members & AIAA Sales Ofﬁce Exhibitors Pavilion Lounge

Corporate Member / Small Business Showcase

Wyle ZIN North Star University of Tech Imaging Notre Dame GE Aviation 516 Cobham 616 715 716815 816 Keystone Cambridge Marotta Stanford Sierra University Engineering NTS Controls Mu Nevada Company Press 414 514 613 614 713 714813 814

Dunmore BETA Metal Intelligent Desktop Worthington JASC CAE Technology Light Aero Industries Controls VACCO Boeing Posters 409 510609 709 710809 810 L-3 General Pointwise Valcor Rolls- NASA Dynamics Royce dSpace 408 407 508607 608 707 708807 808

Aerojet Moog NASA NASA ATK Rocketdyne

404504 604704 804

ENTRANCE

Exhibitors by Booth Number

504 Aerojet Rocketdyne 604 Moog, Inc. 404 ATK 704, 804, NASA 510 BETA CAE Systems USA, Inc. 808 608 Boeing Company 614 National Technical Systems (NTS) 714 Cambridge University Press 715 North Star Imaging Inc. 613 Cobham 607 Pointwise, Inc. 710 Desktop Aeronautics 708 Rolls-Royce 807 dSpace 814 Sierra Nevada Corporation 409 Dunmore Corporation 813 Stanford Mu Corporation 414 GE Aviation 716 University of Notre Dame 508 General Dynamics - OTS 408 VACCO Industries 709 Intelligent Light 707 Valcor Engineering Corporation 810 JASC-Controls 809 Worthington Industries (SCI) 514 Keystone Engineering Company 516 Wyle 407 L-3 Electron Technologies, Inc. 616 ZIN Tech 713 Marotta Controls, Inc. 609 Metal Technology

www.aiaa-propulsionenergy.org 24 #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 30% Off All Books at Propulsion and Energy 2014 Monday, 28 July 0900–1600 hrs AIAA Publications is offering a special discount on all titles Reception* 1800–1930 hrs featured at AIAA Propulsion and Energy 2014. Attendees can Tuesday, 29 July 0900–1130 hrs take advantage of a 30% discount off the list price of all books Networking Luncheon* 1200–1300 hrs for sale at the AIAA Bookstore located in the AIAA Pavilion. 1300–1600 hrs This special offer will only be available during the forum! Take advantage of these super savings and visit the AIAA Bookstore! Wednesday, 30 July 0900–1200 hrs

*A ticket is required to attend the reception and the networking Meet the Author luncheon Monday, 28 July, 1815-1900 hrs AIAA Pavilion Eugene L. Fleeman AIAA Pavilion Missile Design and System Engineering Stop by the AIAA Pavilion, located in the exposition hall, Opening Reception to browse publications and merchandise, learn about your membership benefits, and meet AIAA staff.

www.aiaa-propulsionenergy.org 25 #aiaaPropEnergy Exhibitors Aerojet Rocketdyne 504 Cambridge University Press 714 2001 Aerojet Road 32 Avenue of the Americas Rancho Cordova, CA 95742 New York, NY 10013-2473 www.aerojet.com www.cambridge.org/us [email protected] [email protected] Aerojet Rocketdyne is a world-recognized aerospace and Cambridge’s publishing in books and journals combines state- defense leader providing propulsion and energetics to its space, of-the-art content with the highest standards of scholarship, missile defense, strategic, tactical missile and armaments writing and production. Visit our stand to browse new titles, customers throughout the world. For more information, visit available at a 20% discount, and to pick up sample issues of www.rocket.com our journals. Visit our website to see everything we do: www. cambridge.org/us/. ATK 404 Business Development Cobham 613 UT03-DSBD 10 Cobham Drive PO Box 98 Orchard Park, NY 14127 Magna, UT 84044-0098 www.cobham.com www.atk.com [email protected] [email protected] Cobham offers an innovative range of technologies and ATK is on the forefront of R&D and manufacture of solid services to solve challenging problems across commercial, rocket propulsion, aircraft structures, missile components, defense and security markets, on space, air, land, and maritime small sats, solar arrays, satellite components, and flares and platforms. Cobham Life Support specializes in high pressure decoys. ATK provides affordable solutions to meet emerging pneumatic controls and actuation for space propulsion, life needs. support systems, electro-explosively actuated devices, restraint systems, and inflation products. BETA CAE Systems 510 29800 Middlebelt Road, Suite 100 Desktop Aeronautics 710 Farmington Hills, MI 48334 1900 Embarcadero Way www.ansa-usa.com Palo Alto, CA 94303 [email protected] www.desktop.aero BETA CAE Systems is an engineering services company that [email protected] distributes and supports the industry leading ANSA and Founded in 1994, Desktop Aeronautics has grown into a META software. ANSA is a CAE pre-processing tool for FE well established consulting firm dedicated to advancing and CFD analysis, for full-model build, from CAD to solver the state of the art in aerodynamics and aircraft design. We input file, in one integrated environment. META is a post- have significant experience and recognized expertise in processor for analyzing results from ANSYS, NASTRAN, aerodynamics, aircraft design, computational fluid dynamics, ABAQUS, LS-DYNA, PAMCRASH, RADIOSS, MADYMO, and multidisciplinary optimization. We have worked with and other solvers. leading aerospace organizations on some of the most difficult challenges in aerospace industry. The Boeing Company 608 6861 Sperryville Lane dSPACE 807 Moorpark, CA 93021 50131 Pontiac Trail www.boeing.com Wixom, MI 48393 [email protected] www.dspaceinc.com Boeing is the world’s largest aerospace company and leading [email protected] manufacturer of commercial jetliners and defense, space dSPACE is the world’s leading provider of hardware and and security systems. Its broad range of capabilities includes software tools for developing and testing sophisticated creating new, more efficient members of its commercial electronic control systems. dSPACE’s high-quality, off-the- airplane family, creating advanced technology solutions for shelf tools have played a vital role in product innovation across military customers, and integrating aircraft, defense systems, the industries. Learn more at www.dspaceinc.com. and warfighters through network-enabled solutions.

www.aiaa-propulsionenergy.org 26 #aiaaPropEnergy Exhibitors DUNMORE Corporation 409 JASC-Controls 810 145 Wharton Road 2303 W. Alameda Drive Bristol, PA 19007 Tempe, AZ 85282 www.dunmore.com R www.jasc-controls.com [email protected] [email protected] DUNMORE is a manufacturer of engineered films and tapes The JASC Corporation specializes in the design and for aerospace, supplying multilayer insulation materials to production of high-reliability components for pneumatic, the aerospace industry for over twenty-five years. With a hydraulic, and fuel systems. Since its inception in 1990, JASC highly technical product base of over 400 certified products, has been providing fluid control solutions and advanced DUNMORE is the trusted source for engineered aerospace products for the aircraft, spacecraft, and power generation films and tapes. industries.

GE Aviation 414 Keystone Engineering Company 514 One Neumann Way, MD G414 4401 Donald Douglas Drive Cincinnati, OH 45215 Long Beach, CA 90808 www.ge.com/aviation www.keyengco.com [email protected] [email protected] GE Aviation, an operating unit of GE (NYSE: GE), is a world- Keystone Engineering Company is a privately owned, small leading provider of jet, turboprop, and turboshaft engines, business. Keystone’s core competencies include the design, components, and integrated systems for commercial, military, qualification and production of light-weight propellant and business, and general aviation aircraft. GE Aviation has a pressure storage tanks, and unique fabrication and design global service network to support these offerings. For more technologies for propellant storage assemblies with propellant information, visit us at www.ge.com/aviation. Follow GE management device requirements. Aviation on Twitter at http://twitter.com/GEAviation and YouTube at http://www.youtube.com/user/GEAviation. L-3 Electron Technologies, Inc 407 3100 W Lominta Boulevard General Dynamics 508 Torrance, CA 90505 300 Industrial Avenue www.L-3com.com/eti Lincoln, NE 68504 [email protected] www.gdatp.com [email protected] L-3 Electron Technologies, Inc. (ETI) is a leading provider of electric propulsion systems for both commercial and scientific General Dynamics Armament and Technical Products, located spacecraft. ETI has delivered 13cm and 25cm Xenon Ion in Charlotte, NC, provides a broad range of system solutions Propulsion Systems or XIPS®. ETI also delviered the 30cm for military and commercial applications. The Lincoln, NE XIPS® for NASA’s Deep Space 1 and DAWN spacecraft. ETI has facility develops and produces composite: rocket motor cases, developed an 8cm xenon thruster for small sat application. overwrapped pressure vessels, launch tubes and fuel tanks. Marotta Controls, Inc 713 Intelligent Light 709 78 Boonton Avenue 301 Rt. 17 North, 7th Floor Montville, NJ 07045 Ruthorford, NJ 07070 www.marotta.com www.ilight.com [email protected] [email protected] Marotta Controls, Inc. has 50+ years of experience in designing Intelligent Light provides post-processing, data management control systems for spacecraft. Our engineered propulsion and big data visualization capability for CFD. Thousands of controls are compact, lightweight, use minimal power and are users rely on the industry leading FieldView software and our ready for integration into your system. Let our experienced custom engineering services to maximize their productivity engineering team work with you to overcome your control and effectiveness. Let us help you eliminate bottlenecks and system challenges. Visit us at booth 713. achieve breakthrough results.

www.aiaa-propulsionenergy.org 27 #aiaaPropEnergy ExhibitorsIntro

Metal Technology 609 North Star Imaging 715 173 Queen Avenue SE 19875 South Diamond Lake Road. Albandy, OR 97322 Rogers, MN 55374 www.mtialbany.com www.xrayinspectionservice.com [email protected] [email protected] With more than forty years of experience, Metal Technology North Star Imaging is the largest 3D X-Ray Inspection service (MTI) leads the way in additive manufacturing, precision provide in North America. Send us your samples for failure machining, forming and forging of exotic metals. MTI analysis, reverse engineering and R&D. works with materials such as Tantalum, Niobium, Titanium, Molybdenum, Tungsten and their alloys. MTI is ISO9001 registered and ITAR compliant. Pointwise 607 213 South Jennings Avenue Fort Worth, TX 76104 Moog 604 www.pointwise.com 300 Jamison Road, Plant 20 [email protected] East Aurora, NY 14052 Pointwise, Inc. is solving the top problem facing engineering www.moog.com/space analysts today: mesh generation for computational fluid [email protected] dynamics. Manufacturing firms and research organizations use Moog supplies critical components, subsystems and systems Pointwise’s mesh generation software to seamlessly bridge the for access to and operation in space, including: thrust vector gap between CAD and computational fluid dynamics analysis. control, flight control actuators, electronic controllers, avionics, payload electronics, fluid control systems, propulsion components, subsystems and systems, antenna and solar array Rolls-Royce 708 positioners, reaction wheels, vibration isolation and electronic 2001 South Tibbs Avenue assemblies for satellites. Indianapolis, IN 46241 www.Rolls-Royce.com [email protected] NASA 704/804/808 LibertyWorks® vision is: Trusted to deliver the future by 300 E St. SW defining and demonstrating technologies and power-systems Washington, D.C. 20024 enabling customer-focused solutions. LibertyWorks® focuses www.nasa.gov on increased capability and reduced fuel burn in advanced From Earth, to Mars and Beyond: NASA’s Technology Drives propulsion and power technologies and systems. Emphasis Exploration. NASA highlights its advanced technology areas include highly efficient subsonic, supersonic and high development and capabilities in aeronautics, science, and Mach turbine propulsion systems, highly integrated inlet and human and space operations that also have real world benefits exhaust systems, and innovative integrated power and thermal here on Earth, today. Discover NASA’s current and future management systems. missions to Mars and beyond, and learn about the Agency’s contributions to innovation. Sierra Nevada Corporation 814 1722 Boxelder Street NTS – National Technical Systems 614 Louisville, CO 80027 24007 Ventura Boulevard www.sncorp.com Calabasas, CA 91302 [email protected] www.nts.com Sierra Nevada Corporation’s Space Systems business [email protected] area, headquartered in Louisville, Colorado, designs and NTS is a diversified engineering services company, providing manufactures advanced spacecraft, space vehicles, rocket a wide range of product design consulting services, testing and motors and spacecraft subsystems and components for the certifications, and supply chain management solutions. U.S. government and commercial customers, as well as for the international market.

www.aiaa-propulsionenergy.org 28 #aiaaPropEnergy TM IntroExhibitors

Stanford Mu Corporation 813 Worthington Industries 809 20725 Annalee Avenue 336 Enterprise Place Carson, CA 90746-3503 Pomona, CA 91768 www.stanfordmu.com www.worthingtoncylinders.com [email protected] [email protected] An internationally recognized leader in the design, Manufacturer of Composite Overwrapped Pressure Vessels development and production of propulsion systems and other and Structures. Formerly known as Structural Composites fluid control components for satellites, spacecrafts and space Industries. vehicles. Space Components is ISO9001:2008 and AS9100:0029 Reve. C Certified and has delivered over 800 regulators of which 312 have successfully flown; the balance are awaiting Wyle 516 launch. 22309 Exploration Drive Lexington Park, MD 20653 www.wyle.com University of Notre Dame 716 [email protected] The Contents of this Package are Stanford Mu Corporation Confidential. University of Notre Dame Wyle, a leading provider of specialized engineering, Notre Dame, IN 46556 scientific, technical and test-related services, engineering, www.nd.edu acoustics research and consulting services to DoD, NASA [email protected] and commercial customers. Services include, independent The Notre Dame Turbomachinery Laboratory conducts acquisition, analysis, engineering and technical expertise to applied research for technology development. Govt. program offices, test teams and aircraft depots.

VACCO Industries 408 ZIN Technologies 616 10350 Vacco Street 6745 Engle Road South El Monte, CA 91733 Middle Heights, OH 44130 www.vacco.com www.zin-tech.com [email protected] [email protected] VACCO is a leading designer and manufacturer of specialty ZIN Technologies is an experienced developer of ground valves, filters and advanced fluid control products—offering and flight systems for manned and unmanned aerospace innovative engineered solutions to critical missions for defense, applications. Expertise includes providing scientific, technical, space, and commercial markets for 60 years. Reliable heritage. operational, and program management resources. ZIN Intelligent solutions. specializes in the progression between concept, detailed design, engineering, manufacturing, and operations. Valcor Engineering Corporation 707

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 and drain valves, pressure regulators, actuators) for liquids (propellants, fuel, hydraulic fluid) and gases in critical aerospace (aircraft, launch vehicle, missile, spacecraft, etc.) applications.

www.aiaa-propulsionenergy.org 29 #aiaaPropEnergy IntroGeneral Information

AIAA Registration and Information Center Hours Conference Proceedings The AIAA Registration and Information Center will be located Proceedings for the forum will be available online. The cost on the ballroom level of the Convention Center. is included in the registration fee where indicated. Online Sunday, 27 July 1500–1900 hrs proceedings will be available on 28 July 2014. Attendees who register in advance for the online proceedings will be provided Monday, 28 July 0700–1800 hrs with instructions on how to access them. Those registering on Tuesday, 29 July 0700–1700 hrs site will be provided with instructions at that time. Wednesday, 30 July 0700–1700 hrs Proceedings: 1. To view proceedings, visit www.aiaa.org >ARC>Meeting Papers. AIAA ITAR Registration and Information a. Log in with the link at the top right of the page. Center Hours b. Select the appropriate conference from the list. Monday, 28 July 0930–1800 hrs c. Search for individual papers with the Quick Search toolbar Tuesday, 29 July 0700–1800 hrs in the upper-right corner of the page: Wednesday, 30 July 0700–1100 hrs i. By paper number: Click the Paper Number link, select the conference year, and enter the paper number. ii. Use the Search textbox to find papers by author, title, or Wi-Fi Internet Access On Site keyword. The Advanced Search link provides additional Wi-Fi service for attendees is available in the foyer space of the search information and options. Convention Center outside session rooms and the exposition 2. All manuscript files submitted by four days prior to the hall (see page 5). To keep this service available and optimized conference are currently in the proceedings. Files submitted for all attendees, please do not download files larger than 2MB, after that date, both original and revised manuscripts, will create multiple sessions across multiple devices, or download not be available until the final proceedings update, which multiple files in one session. If you receive an error message may take up to 15 business days after the last day of the that an AIAA server is blocking your current IP address, please conference. inform the AIAA Registration and Information Center. 3. Direct any questions concerning access to proceedings and/ or ARC to [email protected].

Manuscript Revisions 1. Manuscript revision is open for all presenting authors from 0900 hrs Eastern Time, 28 July, through 2000 hrs Eastern Time, 8 August. 2. Revisions submitted for manuscripts already online will not refresh until after the proceedings have been updated, which may take up to 15 business days after the last day of the conference.

www.aiaa-propulsionenergy.org 30 #aiaaPropEnergy IntroGeneral Information

Certiﬁcate of Attendance Young Professional Guide for Gaining Certificates of Attendance are available for attendees who Management Support request documentation at the forum itself. Please request your Young professionals have the unique opportunity to meet and copy at the AIAA Registration and Information Center. AIAA learn from some of the most important people in the business offers this service to better serve the needs of the professional by attending conferences and participating in AIAA activities. community. Claims of hours or applicability toward A detailed online guide, published by the AIAA Young professional education requirements are the responsibility of Professional Committee, is available to help you gain support the participant. and financial backing from your company. The guide explains the benefits of participation, offers recommendations and provides an example letter for seeking management support Employment Opportunities and funding, and shows you how to get the most out of your participation. The online guide can be found on the AIAA AIAA assists members who are searching for employment website at www.aiaa.org/YPGuide. by providing a bulletin board at forums. This bulletin board is solely for “open position” and “available for employment” postings. Employers are encouraged to have personnel who are attending an AIAA forum bring “open position” job Nondiscriminatory Practices postings. Individual AIAA members may post “available for AIAA accepts registrations irrespective of race, creed, gender, employment” notices. AIAA cannot assume responsibility for color, sexual orientation, physical handicap, and national or notices forwarded to AIAA Headquarters. AIAA reserves the ethnic origin. right to remove inappropriate notices. AIAA members can post and browse resumes, browse job listings, and access other online employment resources by visiting the AIAA Career Center at http://careercenter.aiaa.org. Restrictions Photography or the video or audio recording of sessions or exhibits, as well as the unauthorized sale of AIAA-copyrighted Membership material, is prohibited. AIAA is your vital lifelong link to the collective creativity and brainpower of the aerospace profession and a champion International Trafﬁc in Arms Regulations (ITAR) for its achievements – and nonmembers who pay the full nonmember registration fee will receive their first year’s AIAA AIAA speakers and attendees are reminded that some topics membership at no additional cost! Students who are not yet discussed at the forum could be controlled by the International members may apply their registration fee toward their first Traffic in Arms Regulations (ITAR). U.S. nationals (U.S. year’s student member dues. (Free membership is not included citizens and permanent residents) are responsible for ensuring in discounted group-rate registration.) 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 31 #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 30-minute LCD projector, one screen, one microphone and sound briefing on the day of their sessions to exchange bios and system (if necessitated by room size), and one laser pointer. review final details prior to the session. Please attend on the day Laptop computers will also be provided. You may also use of your session(s). Laptops preloaded with the Speaker Briefing your own computer. Any additional audiovisual equipment preparation slides will be provided in each session room. requested onsite will be at cost to the presenter. Please note Speaker’s Briefing schedule is as follows: that AIAA does not provide security in the session rooms and Monday, 28 July 0900–0930 hrs recommends that items of value not be left unattended. Tuesday, 29 July 0900–0930 hrs “No Paper, No Podium” and “No Podium, No Wednesday, 30 July 0900–0930 hrs Paper” Policy Speakers’ Practice Room If a written paper is not submitted by the final manuscript deadline, authors will not be permitted to present the paper at Speakers who wish to practice their presentations may do the forum. Also, if the paper is not presented at the forum, it so in Room 19. A sign-up sheet will be posted on the door. will be withdrawn from the proceedings. It is the responsibility In consideration of others, please limit practice time to of those authors whose papers or presentations are accepted to 30-minute increments. ensure that a representative attends the conference to present the paper. These policies are intended to improve the quality Session Chair Reports of the program for attendees. All session chairs are asked to complete a session chair report to evaluate their session for future planning. AIAA has partnered Journal Publication with Canvas Solutions to provide an electronic Session Chair AIAA has prior publication rights to any paper presented Report form. You can download the FREE mobile app in at its conferences. Authors who are seeking the opportunity your App Store, AppWorld, or Marketplace by searching for for peer-reviewed publication are encouraged to submit their “Canvas Solutions, Inc.” The mobile app is free, so please be papers for consideration by one of the Institute’s archival sure to download it. Detailed instructions will be provided in journals: AIAA Journal; Journal of Aircraft; Journal of the session rooms. If you do not have a tablet or a smartphone, Guidance, Control, and Dynamics; Journal of Propulsion simply use the report form as a guide and enter your session and Power; Journal of Spacecraft and Rockets; Journal of chair report information at the session chair reporting computer Thermophysics and Heat Transfer; or Journal of Aerospace station located on site near the AIAA registration area. Report Information Systems. Journal scopes and author guidelines data will be collected and used for future planning purposes, and instructions can be found in Aerospace Research Central including session topics and room allocations. Please submit at http://arc.aiaa.org/page/authorresources. You may now your session chair report electronically by 5 August. submit your paper to a journal for review before the conference presentation date: http://mc.manuscriptcentral.com/aiaa.

AIAA is the world’s largest technical society dedicated to the global aerospace profession. With more than 35,000 individual members worldwide, and 100 corporate members, AIAA brings together industry, academia, and government to advance engineering and science in aviation, space, and defense. American Institute of Aeronautics and Astronautics 1801 Alexander Bell Drive, Suite 500 Reston, VA 20191-4344 703.264.7500 or 800.639.AIAA (2422) Fax: 703.264.7657 [email protected] www.aiaa.org www.aiaa-propulsionenergy.org 32 #aiaaPropEnergy IntroITAR Information

ITAR Restricted Sessions Availability of Manuscripts from ITAR- On Tuesday and Wednesday, a limited number of papers will be Restricted Sessions presented in “U.S.-Only” technical sessions. In addition to your A DVD containing the manuscripts from the ITAR sessions will forum registration, a separate registration process is required be available for purchase on site at the forum, by those who are to attend these restricted sessions. Please see the detailed registered to attend the ITAR sessions, for $25. There will be no information on the ITAR Registration Grid to determine your sale or distribution of these papers after the event. individual requirements.

Access to ITAR Sessions: Presenting a Paper, ITAR Electronics Policy Chairing a Session, or Attending an ITAR- Restricted Presentation No phones, computers (other than the presenter), ipads, cameras, and other electronic devices with cameras or recording Admittance to the restricted technical papers is controlled by capabilities will be permitted into the ITAR session room. There the U.S. International Traffic in Arms Regulations (ITAR). All will be a check-in desk in front of the room where you can check attendees, presenters, and session chairs will need to register these devices during the time you are in the sessions. for the conference and then visit the ITAR Registration Desk to complete additional registration procedures. Anyone wising to enter the restricted session room MUST abide by the procedures and submittal of verification documents mandated by the DoD. No Exceptions!

Important session information for all attendees wishing to present or attend ITAR papers

AIAA Restricted Papers – ITAR Regulations Session Admittance Policy (Revised 10/19/2012)

Several papers scheduled to be presented at this conference will be restricted papers governed by ITAR (U.S. International Traffic in Arms Regulations). If you plan to attend any presentations restricted by ITAR, you must bring proof of 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 at these restricted presentations. Admittance to restricted sessions and access to restricted technical papers is implemented and controlled by ITAR . All restricted session attendees (including speakers and session chairs for these sessions) MUST abide by the procedures and submittal of verification documents as noted below – NO EXCEPTIONS: ATTENDEE CLASSIFICATION IDENTIFICATION & PROOF OF EMPLOYMENT REQUIREMENTS U.S. Government Employees 1. Proof of U.S. Citizenship (for example, passport, birth certificate, voters registration card, naturalization papers), AND 2. Personal photographic identification: U.S. Government/Military Photo ID badge, such as CAC card U.S. Citizens 1. Proof of U.S. Citizenship (for example, passport, birth certificate, voters registration card, naturalization papers), AND 2. Personal photographic identification (passport, driver’s license, etc.), AND 3. Certification credentials based on DD Form 2345 (see below for details) Resident Aliens (U.S.) 1. Resident Alien Card, AND 2. Personal photographic identification (passport, driver’s license, etc.), AND 3. Certification credentials based on DD Form 2345 (see below for details)

DD Form 2345 individual certification credentials (required for U.S. & Resident Aliens) MUST be from one of the following: 1. Copy of an approved and active DD2345 for the individual, OR 2. Copy of an approved and active DD2345 for the individual’s employer PLUS evidence of current employment status with that employer (corporate ID, business card, etc.), OR 3. A listing of the individual’s employer in the most recent DoD quarterly Qualified U.S. Contractor Access List PLUS evidence of current employment status with that employer (corporate ID, business card, etc.). DD Form 2345 may be downloaded and completed online in order to apply for approval to be listed on the Qualified U.S. Contractor List, www.dlis.dla.mil/jcp. Allow at least 4-6 week (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.

How to get your ITAR Clearance: Bring all of the above listed identification, proof of employment and certification credentials to the AIAA ITAR Registration Desk in the AIAA Registration area. Your documents will be verified and you will be provided with a stamp indicating your ITAR clearance. Photo ID will be checked against your ITAR badge before admittance is granted to any ITAR presentation.

Please be advised that all policies and procedures MUST be followed or admittance to restricted sessions will not be permitted.

10/19/2012

www.aiaa-propulsionenergy.org 33 #aiaaPropEnergy IntroCommittee Meetings

Time Title Location Sunday, 27 July 2014 1500–1600 hrs TAC P&E Rockets, Space and Advanced Propulsion Group Room 10 (Convention Center) 1600–1700 hrs SRTC Awards and Communications Subcommittee Room 11 (Convention Center) 1600–1700 hrs SRTC Education and History Subcommittee Room 12 (Convention Center) 1700–2000 hrs TAC Propulsion and Energy Group Room 10 (Convention Center) Monday, 28 July 2014 0900–1000 hrs ABPTCs Steering Committee Huron 1000–1030 hrs HSABPTC Steering Committee Ontario 1030–1100 hrs ABPTCs New Member Orientation Huron 1100–1200 hrs ABPSITC Meeting Erie 1100–1200 hrs GTETC Meeting Salon A/B 1100–1200 hrs HSABPTC Meeting Salon C 1200–1500 hrs Nuclear and Future Flight Propulsion TC Salon G/H 1300–1400 hrs ABPTCs Conference Subcommittees (ASM/JPC) Huron 1300–1400 hrs TAC P&E Operations Group Salon C 1400–1500 hrs ABPTCs Honors and Awards Subcommittee Ontario 1500–1600 hrs ABPTCs Education Subcommittee Huron 1600-1700 hrs ABPTCs Communications Subcommittee Ontario 1700–1800 hrs ABPTCs PAW Committee Huron 1700–1800 hrs ABPTCs Working Groups Salon C 1700–1800 hrs Executive Steering Committee Room 17 (Convention Center) 1700–1900 hrs GEPC Leadership Team Superior 1900–2130 hrs Propellants and Combustion TC Salon A/B 1900–2200 hrs ABPTCs Dinner Meeting Salon D 1900–2200 hrs Solid Rockets TC Salon G/H 1900–2200 hrs Electric Propulsion TC Salon E 1900–2200 hrs Terrestrial Energy Systems TC Salon F Tuesday, 29 July 2014 1100–1200 hrs Forum Organizing Committee Huron 1300–1400 hrs TAC P&E Products Group Huron 1300–1430 hrs Pressure Gain Combustion PC Erie/Superior 1530–1700 hrs 2015 Technical Program Committee Erie/Superior 1730–1930 hrs Green Engineering PC Erie/Superior 1800–2100 hrs Aerospace Power Systems TC Huron 1900–2200 hrs Energetic Components and Systems TC Room 12 (Convention Center) 1900–2200 hrs Hybrid Rockets TC Room 7 (Convention Center) Wednesday, 30 July 2014 1330–1430 hrs TAC P&E Energy Group Ontario 1900–2230 hrs Liquid Propulsion TC Room 7 (Convention Center)

All meetings held at the Cleveland Marriott, unless otherwise specified. www.aiaa-propulsionenergy.org 34 #aiaaPropEnergy IntroSessions at a Glance

Sessions at a Glance Overview

Energy-Focused Topic Areas Propulsion-Focused Topic Areas Aerospace Power Systems (APS) Advanced Propulsion Concepts (APC) Energy Conversion (EC) Air Breathing Propulsion Systems Integration (ABPSI) Energy Policy/Systems (EPOL/ESYS) Electric Propulsion (EP) Energy Storage Technology (EST) Energetic Components and Systems (ECS) EnergyTech (ET) Gas Turbine Engines (GTE) ITAR (ITAR) High Speed Air Breathing Propulsion (HSABP) Terrestrial Energy Systems (TES) Hybrid Rockets (HR) Thermal Management Technology (TM) ITAR (ITAR) Liquid Propulsion (LP) Nuclear and Future Flight (NFF) Propellants and Combustion (PC) Propulsion Education (EDU) Solid Rockets (SR) Space Transportation (ST) System Concepts and Supporting Propulsion Technologies (SCP)

Abbreviation Title Date Start Time End Time Location Advanced Propulsion Concepts (APC) 80-APC-1 Advanced Space Transportation Concepts 29-Jul 0930 hrs 1200 hrs Room 21 108-APC-2 Advanced Vehicle Propulsion Concepts 29-Jul 1430 hrs 1800 hrs Room 21 168-APC-4 Unique Propulsion Concepts II 30-Jul 1500 hrs 1830 hrs Room 21 Advanced Propulsion Concepts (APC) 21-APS-1 Radioisotope and Fission Power Systems 28-Jul 0930 hrs 1200 hrs Room 21 78-APS-2 Aircraft Electrical Power Systems 29-Jul 0930 hrs 1200 hrs Room 2 132-APS-3 Spacecraft Power Concepts 30-Jul 0930 hrs 1200 hrs Room 12 138-APC-3 Unique Propulsion Concepts I 30-Jul 0930 hrs 1200 hrs Room 21 Air Breathing Propulsion Systems Integration (ABPSI) 33-ABPSI-1/GTE-4 Hybrid Propulsion 28-Jul 0930 hrs 1200 hrs Room 6 59-ABPSI-2 Inlets I 28-Jul 1430 hrs 1800 hrs Room 6 92-ABPSI-3/GTE-13 Integrated Performance I 29-Jul 0930 hrs 1200 hrs Room 6 104-GTE-15/ABPSI-4 Inlet Engine Compatibility and Aeroelasticity 29-Jul 1430 hrs 1800 hrs Room 14 105-GTE-16/ABPSI-5 Jet Noise 29-Jul 1430 hrs 1800 hrs Room 15 111-ABPSI-7 Integrated Performance II 29-Jul 1430 hrs 1800 hrs Room 25 A 117-ABPSI-6 Inlets II 29-Jul 1430 hrs 1800 hrs Room 6 136-HSABP-7/ High-Speed Inlets 30-Jul 0930 hrs 1200 hrs Room 2 ABPSI-8 150-ABPSI-9 Propellers, Small Engines, & Alternative Fuels 30-Jul 0930 hrs 1200 hrs Room 6 180-ABPSI-10 Nozzles 30-Jul 1500 hrs 1830 hrs Room 6

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Abbreviation Title Date Start Time End Time Location Education (EDU) 35-EDU-1 Propulsion Education I 28-Jul 0930 hrs 1200 hrs Room 8 61-EDU-2 Propulsion Education II 28-Jul 1430 hrs 1800 hrs Room 8 Electric Propulsion (EP) 12-EP-2 Ion Thrusters 28-Jul 0930 hrs 1200 hrs Room 10 13-EP-3 Hall - Plume Modeling 28-Jul 0930 hrs 1200 hrs Room 11 18-EP-9 Hall/Ion/Erosion Diagnostics Poster Presentation 28-Jul 0930 hrs 1200 hrs Room 16 Session 29-EP-1 Helicon and Advanced Concepts 28-Jul 0930 hrs 1200 hrs Room 26 C 36-EP-4 Arcjets and Low Thrust EP 28-Jul 0930 hrs 1200 hrs Room 9 41-EP-6 Hall Thruster - Oscillations 28-Jul 1430 hrs 1800 hrs Room 10 47-EP-5 Electrospray and Micropropulsion 28-Jul 1430 hrs 1800 hrs Room 16 62-EP-8 Qualification and Flight Programs 28-Jul 1430 hrs 1800 hrs Room 9 72-EP-10 NEXT Ion Thruster 29-Jul 0930 hrs 1200 hrs Room 10 73-EP-11 Hall Thrusters - Modeling 29-Jul 0930 hrs 1200 hrs Room 11 94-EP-12 Micro-Propulsion 29-Jul 0930 hrs 1200 hrs Room 8 95-EP-13 MPD and Helicon 29-Jul 0930 hrs 1200 hrs Room 9 100-EP-14 Vacuum Facility Effects 29-Jul 1430 hrs 1800 hrs Room 10 101-EP-15 SEP Technology Demonstration Missions 29-Jul 1430 hrs 1800 hrs Room 11 120-EP-16 Hall Thruster 29-Jul 1430 hrs 1800 hrs Room 9 130-EP-17 Cathodes 30-Jul 0930 hrs 1200 hrs Room 10 131-EP-18 Ion Thrusters - Modeling 30-Jul 0930 hrs 1200 hrs Room 11 153-EP-19 Hall - Magnetic Shielded Thrusters 30-Jul 0930 hrs 1200 hrs Room 9 158-EP-20 Mission Concepts 30-Jul 1500 hrs 1830 hrs Room 10 159-EP-21 Micro-Thrusters 30-Jul 1500 hrs 1830 hrs Room 11 164-EP-24 Effects of Ground Test Facilities on Electric Propulsion 30-Jul 1500 hrs 1830 hrs Room 16 Thruster Characteristics - ITAR Panel Session 183-EP-22 Advanced Concepts 30-Jul 1500 hrs 1830 hrs Room 9 Energetic Components Systems (ECS) 119-ECS-1 Energetic Component Modeling, Porous Explosives 29-Jul 1430 hrs 1800 hrs Room 8 and Composites, Technical Roadmaps and Margin Assessments in Testing 152-ECS-2 Metal Composite Powders, Nanosize Fuels, Additives, 30-Jul 0930 hrs 1200 hrs Room 8 Oxidizers Effects and Experimental Methods Energy Conversion (EC) 22-EC-1 Energy Harvesting, Renewable Energy, and Photovoltaic 28-Jul 0930 hrs 1200 hrs Room 22 Systems 51-EC-2 Magnetohydrodynamic Systems and Other Advanced 28-Jul 1430 hrs 1800 hrs Room 22 Concepts 81-EC-3 Thermoelectric Conversion Systems 29-Jul 0930 hrs 1200 hrs Room 22 139-EC-4 Stirling Convertor Analysis and Simulation 30-Jul 0930 hrs 1200 hrs Room 22 169-EC-5 Stirling Power System Analysis and Testing 30-Jul 1500 hrs 1830 hrs Room 22

www.aiaa-propulsionenergy.org 36 #aiaaPropEnergy IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Energy Storage Technology (EST) 50-EST-1 Energy Storage Technology 28-Jul 1430 hrs 1800 hrs Room 21 Energy Systems (ESYS) 109-EPOL-1/ESYS-1 EPOL and ESYS 29-Jul 1430 hrs 1800 hrs Room 22 Energy Tech (ET) 24-ET-1 Advancing Technology Impacts in Energy and 28-Jul 0930 hrs 1200 hrs Room 24 Transportation 63-ET-2 Meeting Education Demands of Future Energy Systems 28-Jul 1500 hrs 1800 hrs Room 24 83-ET-3 Energy Evolution - Achieving Control and 29-Jul 0930 hrs 1200 hrs Room 24 Sustainability 121-ET-4 Energy Life Cycle Vulnerability and Life Cycle 29-Jul 1500 hrs 1800 hrs Room 24 Management 141-ET-5 Regulation & Reliability in the Energy Sector 30-Jul 0930 hrs 1200 hrs Room 24 171-ET-6 Systems Engineering Electric Utilities for Resiliency 30-Jul 1500 hrs 1800 hrs Room 24 Gas Turbine Engine (GTE) 15-GTE-1 Combustors I 28-Jul 0930 hrs 1200 hrs Room 13 16-GTE-2 Compressors I 28-Jul 0930 hrs 1200 hrs Room 14 17-GTE-3 Engine Design & Optimization 28-Jul 0930 hrs 1200 hrs Room 15 33-ABPSI-1/GTE-4 Hybrid Propulsion 28-Jul 0930 hrs 1200 hrs Room 6 44-GTE-6 Turbines I 28-Jul 1430 hrs 1800 hrs Room 13 45-GTE-7 Combustors II 28-Jul 1430 hrs 1800 hrs Room 14 46-GTE-8 Distributed Engine Controls 28-Jul 1430 hrs 1800 hrs Room 15 48-HSABP-2/GTE-9 Pulsed Detonation Engines 28-Jul 1430 hrs 1800 hrs Room 2 55-GTE-5 Gas Turbine Engine 28-Jul 1430 hrs 1800 hrs Room 26 C 75-GTE-10 Combustors III 29-Jul 0930 hrs 1200 hrs Room 13 76-GTE-11 Compressors II 29-Jul 0930 hrs 1200 hrs Room 14 77-GTE-12 Engine Controls 29-Jul 0930 hrs 1200 hrs Room 15 92-ABPSI-3/GTE-13 Integrated Performance I 29-Jul 0930 hrs 1200 hrs Room 6 103-GTE-14/PC-7 Wave Rotors and Pulse Combustors for Gas Turbine 29-Jul 1430 hrs 1800 hrs Room 13 Engines 104-GTE-15/ABPSI-4 Inlet Engine Compatibility and Aeroelasticity 29-Jul 1430 hrs 1800 hrs Room 14 105-GTE-16/ABPSI-5 Jet Noise 29-Jul 1430 hrs 1800 hrs Room 15 133-GTE-17 AIAA/ASME Student Engine Design Competition 30-Jul 0930 hrs 1130 hrs Room 13 134-GTE-18 Turbines II 30-Jul 0930 hrs 1200 hrs Room 14 135-GTE-19 Engine Icing 30-Jul 0930 hrs 1200 hrs Room 15 161-GTE-20 Vehicle Integrated Propulsion Research (VIPR) 30-Jul 1500 hrs 1830 hrs Room 13 162-GTE-21 Engine Cycle Simulation & Modeling 30-Jul 1500 hrs 1830 hrs Room 14 163-GTE-22 Variable Speed Power Turbine (VSPT) 30-Jul 1500 hrs 1830 hrs Room 15

www.aiaa-propulsionenergy.org 37 #aiaaPropEnergy IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location High Speed Air Breathing Propulsion (HSABP) 19-HSABP-1 Advanced Topics in High-Speed Propulsion 28-Jul 0930 hrs 1200 hrs Room 2 48-HSABP-2/GTE-9 Pulsed Detonation Engines 28-Jul 1430 hrs 1800 hrs Room 2 88-HSABP-3 High-Speed Airbreathing Propulsion I 29-Jul 0930 hrs 1200 hrs Room 26 C 106-HSABP-5 Numerical Investigations in High-Speed Propulsion 29-Jul 1430 hrs 1800 hrs Room 2 113-HSABP-4 High-Speed Airbreathing Propulsion II 29-Jul 1430 hrs 1730 hrs Room 26 C 136-HSABP-7/ High-Speed Inlets 30-Jul 0930 hrs 1200 hrs Room 2 ABPSI-8 146-HSABP-6 High-Speed Airbreathing Propulsion III 30-Jul 0930 hrs 1200 hrs Room 26 C 157-HSABP-8/PC-9 Rotating Detonation Engines 30-Jul 1500 hrs 1830 hrs Room 1 165-HSABP-9 Special Session on Supersonic Combustion Simulation 30-Jul 1500 hrs 1830 hrs Room 19 (Invited) 166-HSABP-10 Experimental Investigations in High-Speed Propulsion 30-Jul 1500 hrs 1830 hrs Room 2 Hybrid Rockets (HR) 20-HR-1 Internal Ballistics of Hybrid Rocket Motors 28-Jul 0930 hrs 1200 hrs Room 20 79-HR-3 Novel Fuel Oxidizer Formulations 29-Jul 0930 hrs 1200 hrs Room 20 107-HR-4 Regression Rate Studies in Hybrid Rockets 29-Jul 1430 hrs 1800 hrs Room 20 137-HR-5 Investigations into Fundamental Physical Processes in 30-Jul 0930 hrs 1200 hrs Room 20 Hybrid Rocket Motors 143-HR-6 Current Programs in Hybrid Rocket Motor 30-Jul 0930 hrs 1200 hrs Room 25 B Development 167-HR-7 New Hybrid Motor Concepts 30-Jul 1500 hrs 1830 hrs Room 20 Liquid Propulsion (LP) 11-LP-1 Centaur Upper Stage at 50 Years: Selected Program 28-Jul 0930 hrs 1200 hrs Room 1 Management Topics 30-LP-2 Liquid Rocket Engines 28-Jul 0930 hrs 1200 hrs Room 3 31-LP-3 Green Propellant Infusion Mission (GPIM) 28-Jul 0930 hrs 1200 hrs Room 4 32-LP-4 Combustion Dynamics I 28-Jul 0930 hrs 1200 hrs Room 5 56-LP-5 Cryogenic Propellant Storage and Transfer (CPST) 28-Jul 1430 hrs 1800 hrs Room 3 57-LP-6 Injectors I 28-Jul 1430 hrs 1800 hrs Room 4 58-LP-7 Spacecraft Propulsion Systems I 28-Jul 1430 hrs 1800 hrs Room 5 89-LP-8 Centaur Upper Stage at 50 Years: Selected Technical 29-Jul 0930 hrs 1200 hrs Room 3 Topics 90-LP-9 Combustion Devices I 29-Jul 0930 hrs 1200 hrs Room 4 91-LP-10 Combustion Dynamics II 29-Jul 0930 hrs 1200 hrs Room 5 99-LP-11 LP History: Start and Evolution of Spacecraft 29-Jul 1430 hrs 1800 hrs Room 1 Propulsion 114-LP-12 Propellant Feed Systems & Fluid Management 29-Jul 1430 hrs 1800 hrs Room 3 Technology 115-LP-13 Injectors II 29-Jul 1430 hrs 1800 hrs Room 4 116-LP-14 Spacecraft Propulsion Systems II 29-Jul 1430 hrs 1800 hrs Room 5 147-LP-15 Modeling and Simulation of Engines and Propulsion 30-Jul 0930 hrs 1200 hrs Room 3 Systems

www.aiaa-propulsionenergy.org 38 #aiaaPropEnergy IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Liquid Propulsion (LP) (continued) 148-LP-16 MPCV European Service Module Propulsion System 30-Jul 0930 hrs 1200 hrs Room 4 149-LP-17 Non-Toxic Propellants and Related Technologies 30-Jul 0930 hrs 1200 hrs Room 5 176-LP-18 Combustion Devices II 30-Jul 1500 hrs 1830 hrs Room 26 C 177-LP-19 Propellant Storage and Management 30-Jul 1500 hrs 1830 hrs Room 3 178-LP-20 Rocket Nozzles 30-Jul 1500 hrs 1830 hrs Room 4 179-LP-21 Combustion Chamber Heat Transfer 30-Jul 1500 hrs 1830 hrs Room 5 Nuclear and Future Flight (NFF) 14-NFF-1 Nuclear Thermal Propulsion I - Engine Modelling 28-Jul 0930 hrs 1200 hrs Room 12 43-NFF-2 Fusion and Alternative Nuclear Concepts 28-Jul 1430 hrs 1800 hrs Room 12 74-NFF-3 Nuclear Thermal Propulsion II - Missions, Vehicles & 29-Jul 0930 hrs 1200 hrs Room 12 Architectures 102-NFF-4 Nuclear Thermal Propulsion III - Fuels Development 29-Jul 1430 hrs 1800 hrs Room 12 and Engine Testing 126-NFF-5 Future Flight Propulsion Systems 29-Jul 1900 hrs 2100 hrs Room 6 Propellants and Combustion (PC) 25-PC-1 Propellant and Fuel Development I 28-Jul 0930 hrs 1200 hrs Room 25 A 26-PC-2 Combustion Modeling and Simulation I 28-Jul 0930 hrs 1200 hrs Room 25 B 53-PC-3 Propellant and Fuel Development II 28-Jul 1430 hrs 1800 hrs Room 25 A 54-PC-4 Spray Combustion 28-Jul 1430 hrs 1800 hrs Room 25 B 84-PC-5 Combustion Diagnostics I 29-Jul 0930 hrs 1200 hrs Room 25 A 85-PC-6 Combustion Modeling and Simulation II 29-Jul 0930 hrs 1200 hrs Room 25 B 103-GTE-14/PC-7 Wave Rotors and Pulse Combustors for Gas Turbine 29-Jul 1430 hrs 1800 hrs Room 13 Engines 112-PC-8 Combustion Dynamics and Detonations 29-Jul 1430 hrs 1800 hrs Room 25 B 157-HSABP-8/PC-9 Rotating Detonation Engines 30-Jul 1500 hrs 1830 hrs Room 1 160-PC-11 Combustion Modeling and Simulation III 30-Jul 1500 hrs 1830 hrs Room 12 173-PC-10 Combustion Diagnostics II 30-Jul 1500 hrs 1830 hrs Room 25 B Solid Rockets (SR) 34-SR-1 Solid Rocket Motor Combustion and Acoustic 28-Jul 0930 hrs 1200 hrs Room 7 Instabilities I 40-SR-2 Overview of the Orion Launch Abort System 28-Jul 1430 hrs 1730 hrs Room 1 71-SR-5 Solid Rocket Motor Combustion and Acoustic 29-Jul 0930 hrs 1230 hrs Room 1 Instabilities II 93-SR-3 Solid Rocket Motor Nozzles, Ignition Systems and 29-Jul 0930 hrs 1200 hrs Room 7 Propellants 118-SR-4 Solid Rocket Motor Modeling, Simulation and Analysis I 29-Jul 1430 hrs 1830 hrs Room 7 151-SR-6 Solid Rocket Motor Systems - Historical and Current 30-Jul 0930 hrs 1200 hrs Room 7 Developments 181-SR-7 Solid Rocket Motor Modeling, Simulation and Analysis II 30-Jul 1500 hrs 1830 hrs Room 7

www.aiaa-propulsionenergy.org 39 #aiaaPropEnergy IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Space Transportation 182-ST-1 Space Transportation 30-Jul 1500 hrs 1830 hrs Room 8 System Concepts and Supporting Propulsion Technologies (SCP) 60-SCP-1 Advanced Seal Technology 28-Jul 1430 hrs 1800 hrs Room 7 142-SCP-2 Integrated Modeling, Design, Simulation and 30-Jul 0930 hrs 1200 hrs Room 25 A Diagnostics in Systems. 172-SCP-3 Engineering, Sensing, Measuring and Distributed 30-Jul 1500 hrs 1830 hrs Room 25 A Technologies for Propulsion Systems Terrestrial Energy Systems (TES) 52-TES-1 Experiments and Characterizations 28-Jul 1430 hrs 1800 hrs Room 23 140-TES-2 Numerical Modeling and Simulations 30-Jul 0930 hrs 1200 hrs Room 23 Thermal Management Technology (TM) 82-TM-2 Heating and Cooling of Buildings 29-Jul 0930 hrs 1200 hrs Room 23 110-TM-3 Spacecraft and Lunar/Mars/Venus Surface Thermal 29-Jul 1430 hrs 1800 hrs Room 23 Management 170-TM-4 Aerospace and Terrestrial Energy Systems Thermal 30-Jul 1500 hrs 1830 hrs Room 23 Management

www.aiaa-propulsionenergy.org 40 #aiaaPropEnergy Monday Monday, 28 July 2014 1-PLENARY-1 Perspectives on the Future of Propulsion & Energy - The Art of the Possible Grand Ballroom A 0800 - 0900 hrs Senior P&E leaders will discuss some of the most pressing future challenges and share their thoughts on where propulsion and energy technology is headed in the coming decades. The group will also address how increasing interdependencies between propulsion and energy systems will impact future developments. Moderator: James Free, Center Director, NASA John H. Glenn Research Center Panelists: Richard Parker, Director of Research & Technology, Rolls-Royce plc Eric Bachelet, Executive Vice President, Research and Technology, SAFRAN James Maughan, Technical Director for Aero Thermal and Mechanical Technologies, GE Global Research Monday, 28 July 2014 2-NW-1 Networking Coffee and Pastries in Exposition Hall Exhibit Hall C 0900 - 0930 hrs Monday, 28 July 2014 3-SB-1 Speaker Brieﬁng Session Rooms 0900 - 0930 hrs Please meet your session chairs at 0900 hrs in your session room to load presentations for both the morning and afternoon sessions Monday, 28 July 2014 4-PSTR-1 Technical Poster Display Exhibit Hall C Chaired by: D. JACOBSON, NASA Glenn Research Center

41 0930 hrs 0930 hrs 0930 hrs 0930 hrs 0930 hrs 0930 hrs 0930 hrs AIAA-2014-3400 AIAA-2014-3401 AIAA-2014-3402 AIAA-2014-3403 AIAA-2014-3404 AIAA-2014-3405 AIAA-2014-3406 Coordination of Inverter-Based Analysis of Hypersonic Flow Using Theoretical Investigation and Pulsed Plasma Thrusters for Modelling and Optimization of Improved Superconducting Magnet Daily Volt/VAr control in Distributed Generation Units and Three Dimensional Navier-Stokes Modeling of Current Extraction Atmospheric Operation Electrode-less Helicon Plasma System to Reduce Upstream distribution system in presence of Reactive Power Compensators in Equations From a Radio-Frequency Cathode I. Johnson, R. Winglee, B. Roberson, Thruster with Different Propellants Boundary Power Losses in a Distributed generators considering Power Systems M. Ozgun, S. Eyi, Middle East Technical S. Jahanbakhsh, M. Celik, Bogazici University of Washington, Seattle, F. Bosi, F. Trezzolani, A. Lucca Fabris, Helicon Plasma Thruster voltage security constraints F. Rezaei, S. Esmaeili, Shahid Bahonar University, Ankara, Turkey University, Istanbul, Turkey Seattle, WA M. Manente, D. Melazzi, D. Pavarin, J. Vitucci, R. Sedwick, University of G. Meamarzadeh, S. Esmaeili, Shahid University, Kerman, Iran; H. Mohammadi- University of Padua, Padua, Italy Maryland, College Park, College Park, MD Bahonar University, Kerman, Iran; H. Abdar, Case Western Reserve University, Mohammadi-Abdar, Case Western Reserve Cleveland, OH University, Cleveland, OH 0930 hrs 0930 hrs 0930 hrs 0930 hrs 0930 hrs 0930 hrs 0930 hrs AIAA-2014-3407 AIAA-2014-3408 AIAA-2014-3409 AIAA-2014-3410 AIAA-2014-3411 AIAA-2014-3412 AIAA-2014-3413 Integrated Design Tools for RF Plasma Source Optimization for Study about Ablative Carbon Effect of novel alternative fuels and Measurement of Film Thickness A Study of Ion Thruster Optics Flow Regimes and Combustion Antennas for Helicon Plasma Thrusters Multispecies Helicon Plasma Thruster Materials applied on Chambers compositions on vibrations of a gas in Gas-Centered Swirl Coaxial through Particle Simulations and Characteristics of Swirling Turbulent F. Trezzolani, University of Padua, Padua, D. Melazzi, University of Padua, of LRE turbine engine Injectors Evaluation of the Near Plume Flames in Furnaces Italy; A. Selmo, RESIA, Albaredo d’Adige, Padua, Italy; V. Lancellotti, Eindhoven O. Loureda, Acrux Aerospace Technologies, B. Khandelwal, S. Roy, C. Lord, University G. Park, I. Lee, J. Lee, Y. Yoon, Seoul Plasma Properties A. Ibrahim, E. Bialy, M. Hassan, E. Khalil, Italy; D. Melazzi, University of Padua, University of Technology, Eindhoven, São José dos Campos, Brazil; A. Pimenta, of Sheffield, Sheffield, United Kingdom National University, Seoul, South Korea E. Turkoz, F. Sik, M. Celik, Bogazici Cairo University, Cairo, Egypt Padua, Italy; V. Lancellotti, Eindhoven The Netherlands; F. Trezzolani, F. Bosi, Technological Institute of Aeronautics University, Istanbul, Turkey University of Technology, Eindhoven, The University of Padua, Padua, Italy; M. (ITA), São José dos Campos, Brazil Netherlands; M. Manente, A. Lucca Fabris, Manente, HIT09, Padua, Italy; D. Pavarin, University of Padua, Padua, Italy; et al. University of Padua, Padua, Italy Monday, 28 July 2014 4-PSTR-1 Technical Poster Display -- Continued Exhibit Hall C Chaired by: D. JACOBSON, NASA Glenn Research Center 0930 hrs 0930 hrs 0930 hrs 0930 hrs 0930 hrs 0930 hrs 0930 hrs AIAA-2014-3414 AIAA-2014-3415 AIAA-2014-3416 AIAA-2014-3417 AIAA-2014-3418 AIAA-2014-3419 AIAA-2014-3420 Modeling and hydrodynamic Impulse vector characteristics of a Time-domain numerical simulation Flow Characterization of High Analysis of Self-field MPD Thrusters Azidonation derivatives of Performance evaluation of Electric analysis of a tension leg platform laser-driven vehicle of high frequency combustion Velocity Oxy-Fuel Thermal Sprays for Designing a Megawatt-class 1,1’,4,4’-tetramethyl-2-tetrazene Double Layer Capacitor as energy floating support structure for T. Oyama, H. Horisawa, Tokai University, instability in liquid propellant D. Mohamed, L. Sanchez, L. Cabrera, N. In-space Propulsion System as nitrogen-rich compounds for storage component of micro/ offshore wind turbine Hiratsuka, Japan rocket engines Love, A. Choudhuri, University of Texas, El I. Funaki, Japan Aerospace Exploration NTO/MMH replacement - Synthesis, nano satellite on the imposition of J. Li, X. Wang, Case Western Reserve M. Chu, X. Xu, Beihang University, Beijing, Paso, El Paso, TX Agency (JAXA), Sagamihara, Japan; K. characterization and properties varied temperature and vacuum University, Cleveland Heights, OH; Y. Tang, China Kubota, Japan Aerospace Exploration T. Gilloux, C. Darwich, L. Joucla, Claude conditions Tianjin University, Tianjin, China Agency (JAXA), Chofu, Japan; A. Bernard University Lyon 1, Villeurbanne, M. Alkali, Kyushu Institute of Technology, Kawasaki, Y. Okuno, Tokyo Institute France; G. Jacob, Safran Group, Herakles, Kitakyushu, Japan of Technology, Yokohama, Japan; K. Vert-Le-Petit, France; E. Labarthe, French Miyazaki, S. Takenaka, Tokai University, Space Agency (CNES), Paris, France; H. Hiratsuka, Japan; et al. Delalu, Claude Bernard University Lyon 1, Villeurbanne, France Monday, 28 July 2014 11-LP-1 Centaur Upper Stage at 50 Years: Selected Program Management Topics Room 1 0930 - 1200 hrs Chaired by: M. HEIL, Ohio Aerospace Institute and C. WILLIAMS, NASA Glenn Research Center Monday, 28 July 2014 12-EP-2 Ion Thrusters Room 10 42 Chaired by: G. SOULAS, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3421 AIAA-2014-3422 AIAA-2014-3423 AIAA-2014-3424 AIAA-2014-3425 Results from the RIT-22 Technology Development Status of High-Thrust Neutralizer-free gridded ion Development and test of the Design and Preliminary Testing Maturity Demonstration Activity Density Electrostatic Engines thruster negative and positive ion thruster Plan of Electronegative Ion Thruster H. Leiter, R. Kukies, J. Porst, J. Kuhmann, M. Patterson, NASA Glenn Research D. Rafalskyi, A. Aanesland, National PEGASES T. Liu, N. Schloeder, M. Walker, Georgia M. Berger, M. Rath, Airbus, Heilbronn, Center, Cleveland, OH; J. Foster, University Center for Scientific Research (CNRS), A. Aanesland, D. Rafalskyi, T. Lafleur, P. Institute of Technology, Atlanta, GA; K. Germany of Michigan, Ann Arbor, Ann Arbor, MI; Palaiseau, France Grondein, P. Chabert, National Center for Polzin, J. Dankanich, NASA Marshall Space J. Young, M. Crofton, The Aerospace Scientific Research (CNRS), Palaiseau, Flight Center, Huntsville, AL; A. Aanesland, Corporation, El Segundo, CA France; S. Mazouffre, National Center National Center for Scientific Research for Scientific Research (CNRS), Orleans, (CNRS), Palaiseau, France France; et al. Monday, 28 July 2014 13-EP-3 Hall - Plume Modeling Room 11 Chaired by: I. MIKELLIDES, Jet Propulsion Laboratory and J. MENART, Wright State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3426 AIAA-2014-3427 AIAA-2014-3428 AIAA-2014-3429 Parametric Kinetic Simulation of an Numerical Simulation of the Numerical Momentum Tracking for On the Ionization Cross-Sections in IHI High Specific Impulse SPT-Type Cathode Plume of a Hall Thruster a Hall Thruster Plume an Established Hybrid-PIC Code Hall Thruster M. Choi, I. Boyd, University of Michigan, I. Boyd, University of Michigan, Ann Arbor, B. Smith, I. Boyd, University of Michigan, S. Cho, H. Watanabe, K. Kubota, Japan Ann Arbor, Ann Arbor, MI Ann Arbor, MI; M. Crofton, The Aerospace Ann Arbor, Ann Arbor, MI; H. Kamhawi, Aerospace Exploration Agency (JAXA), Corporation, El Segundo, CA NASA Glenn Research Center, Cleveland, Tokyo, Japan; S. Iihara, K. Honda, IHI OH Corporation, Tokyo, Japan; K. Fuchigami, IHI Corporation, Yokohama, Japan; et al. Monday, 28 July 2014 14-NFF-1 Nuclear Thermal Propulsion I - Engine Modelling Room 12 Chaired by: S. BOROWSKI, NASA Glenn Research Center and A. QUALLS, Oak Ridge National Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3430 AIAA-2014-3431 Oral Presentation Oral Presentation Isotopic Inventories in Thermal Parametric Analyses of a 75 kN Thermal, Fluid, and Structural Bimodal Nuclear Thermal Rocket Neutron Spectrum Reactor Designs Thrust Class Composite Fuel Based Analysis of a Bimodal Fuel Element System Simulation Suitable for Direct Nuclear Thermal NTR Engine M. Stewart, NASA Glenn Research Center, M. Belair, T. Lavelle, NASA Glenn Research Propulsion J. Fittje, Vantage Partners, LLC, Cleveland, Cleveland, OH; B. Schnitzler, Oak Ridge Center, Cleveland, OH B. Schnitzler, Oak Ridge National OH; B. Schnitzler, Oak Ridge National National Laboratory, Oak Ridge, TN; C. Laboratory, Oak Ridge, TN Laboratory, Oak Ridge, TN Joyner, Aerojet Rocketdyne, West Palm Beach, FL Monday, 28 July 2014 15-GTE-1 Combustors I Room 13 Chaired by: H. HUO, General Electric and N. JOSHI, GE 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3432 AIAA-2014-3433 AIAA-2014-3434 AIAA-2014-3435 AIAA-2014-3436 Experimental Investigation of Combustion Dynamics Behavior A Second Generation Swirl-Venturi Fundamental study of a single Flow Field and Liner Heat Transfer Spray Formation in a Hybrid in a Single-Element Lean Direct Lean Direct Injection Combustion point lean direct injector. Part I: for a Model Annular Combustor Atomizer Injection (LDI) Gas Turbine Concept effect of air swirler angle and Equipped with Radial Swirlers S. Chatterjee, M. Das, A. Mukhopadhyay, Combustor K. Tacina, C. Chang, Z. He, NASA Glenn injector tip location on spray D. Gomez Ramirez, V. Kumar, S. Ekkad, S. Sen, Jadavpur University, Kolkata, India R. Gejji, C. Huang, V. Laskhmanan, Purdue Research Center, Cleveland, OH; P. Lee, characteristics D. Tafti, Virginia Polytechnic Institute and University, West Lafayette, IN; C. Yoon, Woodward FST, Inc., Zeeland, MI; H. S. Tedder, K. Tacina, R. Anderson, Y. State University, Blacksburg, VA; Y. Kim, General Electric Company, Niskayuna, Mongia, Purdue University, Lafayette, IN; Hicks, NASA Glenn Research Center, H. Moon, Solar Turbines, Inc., San Diego, B. Dam, Woodward FST, Inc., Zeeland, MI CA; et al. 43 NY; W. Anderson, Purdue University, West Cleveland, OH Lafayette, IN Monday, 28 July 2014 16-GTE-2 Compressors I Room 14 Chaired by: D. FOUTCH 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3437 AIAA-2014-3438 AIAA-2014-3439 AIAA-2014-3440 AIAA-2014-3441 Phase Resolved Hot-wire Surge Margin Extension and Performance Impact of Tip Pre-Stall Pressure Measurements Parametric Study of the Bleed Measurements for High-speed Circumferential Groove Interaction Clearance Variation on a Transonic, of a Low-Speed Single-Stage Axial- Position in a Tip Blowing Casing Turbomachinery Flows with the Rotor Tip Clearance Flow Low Aspect Ratio, Axial Compressor Flow Compressor Treatment N. Jaffa, J. Cameron, S. Morris, University Field Stage B. Butler, University of Kentucky, C. Guinet, V. Bettrich, Technical University of Notre Dame, Notre Dame, IN M. Ross, J. Cameron, S. Morris, M. R. Howard, S. Puterbaugh, Air Force Lexington, Lexington, KY; V. Capece, of Munich, Munich, Germany; V. Gümmer, Bennington, University of Notre Dame, Research Laboratory, Wright-Patterson University of Kentucky, Paducah, Paducah, Rolls-Royce Group plc, Blankenfelde, Notre Dame, IN AFB, OH KY Germany Monday, 28 July 2014 17-GTE-3 Engine Design & Optimization Room 15 Chaired by: D. JENSEN, Rolls-Royce Corporation and G. BOBULA, U. S. Army AMRDEC 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3442 AIAA-2014-3443 AIAA-2014-3444 AIAA-2014-3445 Exploring advanced technology Common Core Engine Design Optimization of Variable Cycle Design Optimization of a Variable- gas turbine engine design and for Multiple Applications using Engines by Using an Improved Speed Power-Turbine performance for the Large Civil a Concurrent Multi-Design Point Differential Evolution E. Hendricks, S. Jones, NASA Glenn Tiltrotor (LCTR) Approach H. Zhou, Z. Wang, X. Zhang, M. Cao, Research Center, Cleveland, OH C. Snyder, NASA Glenn Research Center, M. Hughes, C. Perullo, D. Mavris, Georgia Northwestern Polytechnical University, Cleveland, OH Institute of Technology, Atlanta, GA Xi’an, China Monday, 28 July 2014 18-EP-9 Hall/Ion/Erosion Diagnostics Poster Presentation Session Room 16 Chaired by: M. CROFTON, The Aerospace Corporation and M. NAKLES, AFRL/RZSS 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3446 AIAA-2014-3447 AIAA-2014-3448 Study on Specific Mass of Nuclear Three Dimensional Coupled PIC and Development of a Direct Thrust Electric Propulsion System with DSMC Simulations of Ion Thruster Balance for Low Power Hollow Closed Cycle MHD Generator Plumes with SUGAR Cathode Thruster K. Miyazaki, K. Takahashi, T. Sasaki, T. B. Korkut, D. Levin, Pennsylvania State D. Frollani, University of Southampton, Kikuchi, N. Harada, Nagaoka University University, University Park, PA Southampton, United Kingdom; M. of Technology, Nagaoka, Japan; S. Coletti, Mars Space, Ltd., Southampton, Takeshita, Wakayama National College of United Kingdom; S. Gabriel, University Technology, Gobo, Japan of Southampton, Southampton, United Kingdom Monday, 28 July 2014 19-HSABP-1 Advanced Topics in High-Speed Propulsion Room 2 Chaired by: H. HASSAN, North Carolina State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3449 AIAA-2014-3450 AIAA-2014-3451 AIAA-2014-3452 AIAA-2014-3453 Propulsion System Design for a High-g Field Combustor of a Rim- Numerical Investigation on Numerical Investigation on Numerical and Experimental Martian Atmospheric Breathing Rotor Rotary Ramjet Engine Self-ignition and Flammability Influence on the Regression Rate of study on the Solid Fuel Scramjet Supersonic Retropropulsion Engine D. Rancourt, M. Picard, J. Plante, M. Characteristics in Solid Fuel the Inlet Parameters in Solid Fuel Combustor with a cavity flame K. Gonyea, Georgia Institute of Technology, Brouillette, University of Sherbrooke, Scramjet Combustor Scramjet Combustor holder Atlanta, GA; A. Auslender, NASA Langley Sherbrooke, Canada H. Chi, Z. Wei, L. Biao, L. Wang, Beijing C. Liu, Z. Wei, H. Chi, L. Wang, Beijing L. Wang, H. Chi, C. Liu, H. Tao, Q. Wang, 44 Research Center, Hampton, VA; R. Institute of Technology, Beijing, China Institute of Technology, Beijing, China Beijing Institute of Technology, Beijing, Braun, Georgia Institute of Technology, China Atlanta, GA Monday, 28 July 2014 20-HR-1 Internal Ballistics of Hybrid Rocket Motors Room 20 Chaired by: A. CHANDLER, Jet Propulsion Laboratory and J. MAJDALANI, Auburn University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3454 AIAA-2014-3455 AIAA-2014-3456 AIAA-2014-3457 Internal Ballistics of Hybrid Rocket Linear Combustion Stability Combined Analysis of Reactive Hybrid Rocket Transient Flow and with a Diaphragm Analysis of Uni-directional Vortex Flow and Heat Transfer for Hybrid Combustion Analysis C. Lee, K. Mon, C. Park, G. Choi, Konkuk Injection Hybrid Rocket Engines Rocket Design Engineering A. Gad, Cairo University, Cairo, Egypt; University, Seoul, South Korea K. Ozawa, University of Tokyo, Y. Funami, University of Tokyo, Tokyo, P. Penko, Baldwin Wallace University, Sagamihara, Japan; T. Shimada, Japan Japan; T. Shimada, Japan Aerospace Berea, OH Aerospace Exploration Agency (JAXA), Exploration Agency (JAXA), Sagamihara, Sagamihara, Japan Japan Monday, 28 July 2014 21-APS-1 Radioisotope and Fission Power Systems Room 21 Chaired by: D. ALLEN 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3458 AIAA-2014-3459 AIAA-2014-3460 AIAA-2014-3461 AIAA-2014-3462 Kilopower, NASA’s Small Fission Non-Cooled Power System for Watt Scale Thermophotovoltaic Parametric System Model of NASA’s Radioisotope Power Systems Power System for Science and Venus Lander Power System Testing Results- Stirling Radioisotope Generators Program Status Human Exploration D. Salazar, University of Texas, Austin, Consider for ITAR Session P. Schmitz, Power Computing Solutions, L. Dudzinski, NASA Headquarters, M. Gibson, L. Mason, C. Bowman, NASA Austin, TX; G. Landis, NASA Glenn J. Strauch, PE, A. Klein, General Atomics, Inc., Avon, OH Washington, DC; J. Hamley, P. McCallum, Glenn Research Center, Cleveland, OH; D. Research Center, Cleveland, OH; A. San Diego, CA; C. Murray, L3 Power C. Sandifer, T. Sutliff, J. Zakrajsek, NASA Poston, P. McClure, Los Alamos National Colozza, Vantage Partners, LLC, Cleveland, Paragon, Anaheim, CA; P. Charles, General Glenn Research Center, Cleveland, OH Laboratory, Los Alamos, NM; J. Creasy, OH Atomics, San Diego, CA Y-12 National Security Complex, Oak Ridge, TN; et al. Monday, 28 July 2014 22-EC-1 Energy Harvesting, Renewable Energy, and Photovoltaic Systems Room 22 Chaired by: D. WOLFORD, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3463 AIAA-2014-3464 AIAA-2014-3465 AIAA-2014-3466 Validation and Assesment of Lower Advanced Solar Energy Conversion Solar Probe Plus (SPP) Dynamic Neutron Degradation of TPV Cells- Order Aerodynamics Based Design Technologies Enabled by Novel Solar Array Simulator Consider for ITAR Session of Ram Air Turbines (Nano)Materials and Processing A. Baisden, T. Parker, H. Nguyen, Johns J. Strauch, PE, A. Klein, General Atomics, A. Renganathan, R. Denney, Georgia for Space Power with Potential for Hopkins University Applied Physics San Diego, CA; C. Murray, L3 Power Institute of Technology, Atlanta, GA; A. Terrestrial Applications Laboratory, Laurel, MD Paragon, Anaheim, CA; M. Du, Oak Ridge National Laboratory, Oak Ridge, TN 45 Duquerrois, SAFRAN, Atlanta, GA; D. A. Hepp, S. Bailey, J. McNatt, NASA Glenn Mavris, Georgia Institute of Technology, Research Center, Cleveland, OH; J. Harris, Atlanta, GA Northwest Nazarene University, Nampa, ID; M. Chandrashekhar, University of South Carolina, Columbia, Columbia, SC; P. Hari, University of Tulsa, Tulsa, OK; et al. Monday, 28 July 2014 24-ET-1 Advancing Technology Impacts in Energy and Transportation Room 24 0930 - 1200 hrs Panel 1: Advancing Terrestrial and Space Power Generation This panel plans to cover thermal energy and electric power production issues facing our nation and the world over the next decades, with relevant technologies ranging from near term to mid-and far term. Although the main focus will be on ground based plants to provide baseload electric power, energy conversion systems (ECS) for space, with solar- or nuclear energy sources for output power levels ranging tens of Watts to kilo-Watts for unmanned spacecraft, and eventual mega-Watts for lunar outposts and planetary surface colonies, are also included. Implications of these technologies on future terrestrial energy systems, combined with advanced fracking, Thorium based reactors, and nuclear fusion - will also be considered by the panelists. The characteristics of the above mentioned ECS will be described, both in terms of their overall energy utilization effectiveness and also with regard to climactic effects due to exhaust emissions. Moderator: Al Juhasz , NASA GRC Panelists: Bill Thesling, Energy From Thorium Foundation. Roger Dyson , NIRVANA Jason Mallinak, Babcock/Wilcox Al Juhasz , NASA GRC Panel 2: Exponential technology development driving future vehicle system complexity Due to the regulatory landscape, driving complexity, rapidly developing technological solutions, and societal/human factors, the potential production options for future road vehicle integrated solutions comes with heightened risk. Whether viewed from the perspective of consumers, government agencies, industry, or investors, the uncertainties and ambiguities make decision-making very difficult. This panel provides attendees with an overview of the current state, the latest thinking and analysis about the future vehicle system landscape from the perspective of leaders in key sectors. Moderator: Andrew Smart , SAE International Panelists: Paul Luskin, Ricardo Defense Systems Rick Kline , Cummins Diesel Greg Pannone, Control TEC

46 Monday, 28 July 2014 25-PC-1 Propellant and Fuel Development I Room 25 A Chaired by: M. COIL, Orbital Technologies Corporation 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3468 AIAA-2014-3469 AIAA-2014-3470 “Virtual” Smoke Point Characterization of Global Ignition and Combustion of Gelled Determination of Alternative Combustion Properties with Simple Hydrocarbon Fuels with Hydrogen Aviation Kerosenes by Threshold Fuel Property Measurements for Peroxide using Impinging Jets Sooting Index TSI) Methods Alternative Jet Fuels T. Connell, G. Risha, R. Yetter, F. Haas, A. Qin, F. Dryer, Princeton S. Won, S. Dooley, P. Veloo, J. Santner, Pennsylvania State University, University University, Princeton, NJ Y. Ju, F. Dryer, Princeton University, Park, PA; B. Natan, Technion--Israel Princeton, NJ Institute of Technology, Haifa, Israel Monday, 28 July 2014 26-PC-2 Combustion Modeling and Simulation I Room 25 B Chaired by: J. OEFELEIN, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation AIAA-2014-3471 AIAA-2014-3472 AIAA-2014-3473 Effect of Acoustic Oscillations on Filtered Mass Density Function Soot Predictions in an Aero-Engine Unsteady RANS for Simulation Change in Curvature and Lift-off for Use in Discontinuous Spectral Model Combustor at Elevated of High Swirling Non-Premixed Height of Triple Flame Element Method Pressure Using URANS and Finite- Methane-Air Flame M. Saito, N. Sugiu, Y. Yamamoto, M. J. Komperda, Z. Ghiasi, F. Mashayek, Rate Chemistry M. Solmaz, Scientific and Technological Tanabe, Nihon University, Chiba, Japan University of Illinois, Chicago, Chicago, C. Eberle, German Aerospace Center Research Council of Turkey (TÜBITAK), IL; A. Irannejad, F. Jaberi, Michigan State (DLR), Stuttgart, Germany; P. Gerlinger, Ankara, Turkey; S. Uslu, TOBB University University, East Lansing, MI University of Stuttgart, Stuttgart, of Economics and Technology, Ankara, Germany; M. Aigner, German Aerospace Turkey; O. Uzol, Middle East Technical Center (DLR), Stuttgart, Germany University, Ankara, Turkey Monday, 28 July 2014 27-PANEL-1 A Future with Hybrid Electric Propulsion Systems—Opportunities and Challenges Room 26 A 0930 - 1200 hrs This panel session will review recent progress and future prospects for hybrid electric propulsion systems for aircraft applications. Topics to be addressed will include discussion on nearer term opportunities for ground and small-scale flight demonstrations leading to longer term applicability of the technology for larger commercial transports. Moderators: Ruben Del Rosario, NASA Glenn Research Center Nateri Madavan, NASA Glenn Research Center Panelists: Kevin Daffey, Global Head of Electrical Power and Control Systems, Rolls-Royce plc Marty Bradley, Technical Fellow, Boeing Commercial Airplanes John Nairus, Chief Engineer, Power and Controls Division, Air Force Research Laboratory Neil Garrigan, Executive Manager, Aviation Advanced Technology, GE Aviation Monday, 28 July 2014 28-PANEL-6 Compressing the Technology Development and Transition Timeline Room 26 B 0930 - 1200 hrs This session will discuss ways to expedite technology development, maturation, and transition via a series of interviews and audience Q&A sessions. Topics will address tomorrow’s key technologies, technology maturation and validation, and rapid transition to products. Interviewer: Alan Epstein, Vice President Technology and Environment, Pratt & Whitney Interviewees: Ed Greitzer, H.N. Slater Professor of Aeronautics and Astronautics, Massachusetts Institute of Technology Thomas Irvine, Deputy Associate Administrator, NASA Headquarters Interviewer: Anthony Dean, GE Global Research Interviewees: Scott Cruzen, Vice President Advanced Design/Technology, Williams International Co., LLC Tom Fetterhoff, Technical Director for Test Operations, AEDC Interviewer: Ted Fecke, Retired USAF Senior Leader for Propulsion, Universal Technologies Corp 47 Interviewee: Keith Leverkuhn, Vice President, Boeing Commercial Airplanes Monday, 28 July 2014 29-EP-1 Helicon and Advanced Concepts Room 26 C Chaired by: K. LEMMER, Western Michigan University 0930 hrs 1000 hrs AIAA-2014-3474 AIAA-2014-3475 Thrust Performance of High Investigation of Plasma-wave Magnetic Field Permanent Magnet Interaction in Helicon Antenna Type Helicon Plasma Thruster Thrusters T. Nakamura, S. Ito, H. Nishida, S. B. Tian, E. Ahedo, Charles III University Shinohara, Tokyo University of Agriculture of Madrid, Madrid, Spain; J. Navarro, and Technology, Tokyo, Japan; I. Funaki, Technical University of Madrid, Madrid, Japan Aerospace Exploration Agency Spain (JAXA), Kanagawa, Japan; T. Tanikawa, Tokai University, Kanagawa, Japan; et al. Monday, 28 July 2014 30-LP-2 Liquid Rocket Engines Room 3 Chaired by: J. SCHNACKEL, United Launch Alliance and T. KMIEC, Kord Technologies 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3476 AIAA-2014-3477 AIAA-2014-3478 AIAA-2014-3479 AIAA-2014-3480 Update on Risk Reduction Activities Summary of Antares First Stage The VINCI propulsion system: new The VINCI Engine Vibration Test Development status of LOX/LCH4 for an F-1-Based Advanced Booster Development Test steps toward qualification campaign rocket engine for NASA’s Space Launch System T. Gaio, K. Ertmer, Orbital Sciences P. Alliot, J. Delange, Safran Group, A. Sternchuss, A. Bossaert, P. Manfredi, K. Taya, Y. Ishikawa, K. Kimoto, S. A. Crocker, K. Doering, R. Meadows, Corporation, Dulles, VA Snecma, Vernon, France; A. Lekeux, B. N. David, P. Alliot, Safran Group, Snecma, Ishizaki, IHI Corporation, Tokyo, Japan Dynetics, Inc., Huntsville, AL; B. Lariviere, Vieille, French Space Agency (CNES), Vernon, France; A. Grillenbeck, IABG, Aerojet Rocketdyne, DeSoto, CA Paris, France; V. DeKorver, E. Edeline, Ottobrunn, Germany Safran Group, Snecma, Vernon, France Monday, 28 July 2014 31-LP-3 Green Propellant Infusion Mission (GPIM) Room 4 Chaired by: T. POURPOINT, Purdue University and D. SARGENT, Federal Aviation Administration 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3481 AIAA-2014-3482 AIAA-2014-3483 Green Propellant Infusion Mission GPIM Propulsion System Green Propellant Infusion Mission Program Development and Development Status Thruster Performance Testing for Technology Maturation R. Spores, Aerojet Rocketdyne, Redmond, Plume Diagnostics C. McLean, Ball Aerospace & Technologies WA M. Deans, B. Reed, NASA Glenn Research Corporation, Boulder, CO Center, Cleveland, OH; C. McLean, Ball Aerospace & Technologies Corporation, Boulder, CO; G. Williams, J. Kojima, Ohio Aerospace Institute, Cleveland, OH; L. 48 Arrington, NASA Glenn Research Center, Cleveland, OH; et al. Monday, 28 July 2014 32-LP-4 Combustion Dynamics I Room 5 Chaired by: T. HINERMAN, Aerojet Rocketdyne Corporation and D. LINEBERRY, UAH Propulsion Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3484 AIAA-2014-3485 AIAA-2014-3486 AIAA-2014-3487 AIAA-2014-3488 Effect of Swirl on an Unstable Low-order model studies of Forced Nonlinear Acoustic Damping Receptivity of a Cryogenic Steepened Tangential Waves: DC Single-Element Gas-Gas Rocket combustion instabilities in a DVRC in a Rijke Tube and its Application Coaxial Gas-Liquid Jet to Acoustic Offset and Pressure “Valleys” Engine combustor to Combustion Instability Control Disturbances E. Jacob, J. Batterson, GTL Company, M. Harvazinski, V. Sankaran, D. Talley, M. Frezzotti, A. Terracciano, F. Nasuti, E. Jacob, GTL Company, Tullahoma, TN J. Wegener, University of California, Los Tullahoma, TN; A. Wilson, Wave CPC, Inc., Air Force Research Laboratory, Edwards University of Rome “La Sapienza’’, Rome, Angeles, Los Angeles, CA; D. Forliti, Sierra Tullahoma, TN AFB, CA Italy; S. Hester, W. Anderson, Purdue Lobo, Inc., Edwards AFB, CA; I. Leyva, University, West Lafayette, IN D. Talley, Air Force Research Laboratory, Edwards AFB, CA Monday, 28 July 2014 33-ABPSI-1/GTE-4 Hybrid Propulsion Room 6 Chaired by: C. PERULLO, Georgia Institute of Technology and N. HERRING, United Technologies Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3489 AIAA-2014-3490 AIAA-2014-3492 Assessment of Vehicle Performance A Simplified Method To Calculate Sensitivity of TeDP Microgrid Using Integrated NPSS Hybrid The Fuel Burn Of A Hybrid-Electric System Weight and Efficiency to Electric Propulsion Models Airplane Operating Voltage C. Perullo, D. Mavris, Georgia Institute of R. Jagannath, S. Bane, Purdue University, M. Armstrong, M. Blackwelder, C. Ross, Technology, Atlanta, GA West Lafayette, IN; M. Nalim, Indiana Rolls-Royce Group plc, Indianapolis, IN University-Purdue University Indianapolis, Indianapolis, IN; J. Khan, Tuskegee University, Tuskegee, AL Monday, 28 July 2014 34-SR-1 Solid Rocket Motor Combustion and Acoustic Instabilities I Room 7 Chaired by: H. CIEZKI, DLR - German Aerospace Center and E. CAVALLINI, University of Roma “La Sapienza” 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3493 AIAA-2014-3494 AIAA-2014-3495 AIAA-2014-3496 AIAA-2014-3497 Use of Reactive Particles for Solid Modeling Effects of Generalized Scaling Technique for Dual-Mode Combustion Acoustic Oscillations Induced by Rocket Combustion Instability Initial Temperatures on a the Solution of the Vortical Wave Characteristic of a Self-Quenched Shear Layer Oscillations Due to Suppression Propellant's Pressure- Eigenfunction Equation Solid Propellant in a Rocket Motor Flow Past Single Axisymmetric ‘ V’ D. Greatrix, Ryerson University, Toronto, Coupled Response Using a Psedo J. Batterson, GTL Company, Tullahoma, M. Tanaka, National Defense Academy, Slot in a Duct Canada Propellant Model TN; J. Majdalani, Auburn University, Yokosuka, Japan T. Manickavelu, C. Satyanarayana, Indian J. Spurling, Naval Air Warfare Center, Auburn, AL Institute of Technology Madras, Chennai, 49 China Lake, CA India Monday, 28 July 2014 35-EDU-1 Propulsion Education I Room 8 Chaired by: E. FLEEMAN, University of Heidelberg, Germany and R. FREDERICK, University of Alabama @ Huntsville 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3498 AIAA-2014-3499 AIAA-2014-3500 AIAA-2014-3501 AIAA-2014-3502 Design of a 3-D Printed Unified Design and Analysis of a High Design and Analysis of a High- The Effect of Liquid Jet Breakup 3D Printing: A Cost Effective and Hybrid Motor Speed, High Pressure Peroxide/ Performance Hydrogen Peroxide Length upon the Spray Dynamics of Timely Approach to Manufacturing M. Hitt, University of Alabama, Huntsville, RP-1 Turbopump Thrust Chamber Assembly Like-Doublet Impinging Injectors of Low-Thrust Engines Huntsville, AL; T. Taylor, USASMDC/ W. Murray, M. Steiner, J. Neal, S. Hunt, D. Stechmann, D. Lim, S. Rotella, S. B. Sweeney, R. Frederick, University of T. Zhang, NASA Marshall Space Flight ARSTRAT, Huntsville, AL; R. Frederick, Purdue University, West Lafayette, IN Menon, B. Nirudhoddi, Purdue University, Alabama, Huntsville, Huntsville, AL Center, Huntsville, AL; H. Yang, Students University of Alabama, Huntsville, West Lafayette, IN for the Exploration and Development of Huntsville, AL Space, San Diego, CA; C. Miyamoto, University of California, San Diego, San Diego, CA Monday, 28 July 2014 36-EP-4 Arcjets and Low Thrust EP Room 9 Chaired by: K. POLZIN, NASA Marshall Space Flight Center and K. KOMURASAKI, The University of Tokyo 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3503 AIAA-2014-3504 AIAA-2014-3505 AIAA-2014-3506 AIAA-2014-3507 Testing of Diode-Clamping in an Al-water Fed Chemically Thrust of a Hollow Cathode Performance Characteristics of Low- Preliminary Study of High Power Inductive Pulsed Plasma Thruster Augmented DC Arcjet Thrusters: Influence of the Applied Power Arcjet Thrusters Using Green Hydrogen Electric Propulsion for Circuit Characteristics Magnetic Field Propellants of HAN and Water the Space Exploration A. Toftul, K. Polzin, NASA Marshall Space N. Yanagida, H. Horisawa, Tokai D. Frollani, University of Southampton, F. Inoue, H. Tahara, Osaka Institute of K. Kinefuchi, K. Okita, Japan Aerospace Flight Center, Huntsville, AL; J. Hudgins, University, Hiratsuka, Japan Southampton, United Kingdom; M. Technology, Osaka, Japan Exploration Agency (JAXA), Tsukuba, University of Nebraska, Lincoln, Lincoln, Coletti, Mars Space, Ltd., Southampton, Japan; H. Kuninaka, Japan Aerospace NE United Kingdom; S. Gabriel, University Exploration Agency (JAXA), Sagamihara, of Southampton, Southampton, United Japan; D. Nakata, Muroran Institute of Kingdom Technology, Muroran, Japan; H. Tahara, Osaka Institute of Technology, Osaka, Japan Monday, 28 July 2014 37-LNCH-1 Lunch on Your Own On Own 1200 - 1300 hrs Monday, 28 July 2014 38-PLENARY-2 Perspectives on the Future of Propulsion & Energy - The View from Users Grand Ballroom A 1300 - 1430 hrs Executives from leading aircraft and space vehicle manufacturers will build off the morning plenary to discuss how advances in future propulsion and energy systems will benefit next generation aerospace platforms. 50 Moderator: Graham Warwick, Managing Editor, Technology, Aviation Week Panelists: Sebastien Remy, Senior Vice President, Head of Airbus Group Innovations, Airbus Group James Petersen, Vice President/Senior Chief Engineer, Boeing Commercial Airplanes John Henderson, Lockheed Martin Fellow, Space Propulsion, Lockheed Martin Corporation Leslie J. Kovacs, Director, Washington Operations, United Launch Alliance (ULA) Monday, 28 July 2014 39-NW-2 Networking Break in Exposition Hall Exhibit Hall C 1430 - 1500 hrs Monday, 28 July 2014 40-SR-2 Overview of the Orion Launch Abort System Room 1 1430 - 1730 hrs Chaired by: D. MCGRATH, Alliant Techsystems, Inc. (ATK) and J. PAISLEY, Lockheed Martin Space Systems Come hear about the most capable launch abort system in the world, used on the NASA Orion capsule should the launch vehicle fail anywhere between the launch pad and 300,000 feet. The program and propulsion progress from requirements through development, future qualification and flight activities will be discussed by the individuals involved in the progress to-date. Key topics include: 1. The Orion Launch Abort System Performance and Requirements - Jonathan Paisley, Lockheed Martin; Rachel McCauley, NASA 2. Abort Motor Progress and Future Activities - Heather McKay, Lockheed Martin; Steve Sara, Eric Malloy & Brad Johnson, ATK Utah 3. Jettison Motor Progress and Future Activities - Tim Larson, Lockheed Martin; David Daniewicz & Scott Cunningham, Aerojet Rocketdyne 4. Attitude Control Motor Progress and Future Activities - Jonathan Paisley, Lockheed Martin; Dave McGrath, Jake Williams, Matt Porter & Tim Dominick, ATK Elkton 5. The Launch Abort System Role in the EFT-1 Flight and LAS Path Forward - Jonathan Paisley, Lockheed Martin; Rachel McCauley, NASA Monday, 28 July 2014 41-EP-6 Hall Thruster - Oscillations Room 10 Chaired by: H. KAMHAWI, NASA Glenn Research Center and E. CHOUEIRI, Princeton University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3508 AIAA-2014-3509 AIAA-2014-3510 AIAA-2014-3511 AIAA-2014-3512 AIAA-2014-3513 An Investigation of Low Frequency Driving Low Frequency Breathing Low-Voltage Hall Thruster Mode Mode Transitions in Magnetically Analysing the Azimuthal Spoke Development and characterization Plasma Instabilities in a Cylindrical Oscillations in a Hall Thruster Transitions Shielded Hall Effect Thrusters Oscillation of Hall Thrusters via of a wall-less Hall thruster Hollow Cathode Discharge S. Keller, Y. Raitses, A. Diallo, Princeton D. Brown, Air Force Research Laboratory, M. Sekerak, B. Longmier, A. Gallimore, Numerical Simulation S. Mazouffre, S. Tsikata, J. Vaudolon, T. Matlock, D. Goebel, R. Wirz, University Plasma Physics Laboratory, Princeton, NJ Edwards AFB, CA; J. Blakely, R. Lobbia, University of Michigan, Ann Arbor, Ann D. Escobar Anton, Technical University of National Center for Scientific Research of California, Los Angeles, Los Angeles, CA ERC, Inc., Edwards AFB, CA Arbor, MI; W. Huang, H. Kamhawi, NASA Madrid, Madrid, Spain; E. Ahedo, Charles (CNRS), Orleans, France Glenn Research Center, Cleveland, OH; R. III University of Madrid, Leganés, Spain Hofer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; et al. Monday, 28 July 2014 43-NFF-2 Fusion and Alternative Nuclear Concepts Room 12 Chaired by: G. MEHOLIC, The Aerospace Corporation and R. SEDWICK, University of Maryland 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3516 AIAA-2014-3517 AIAA-2014-3518 AIAA-2014-3520 A Hybrid Particle-in-cell Simulation A Cohesive Model to Predict Practical realisation of the nuclear Developing the Pulsed Fission- for a Multiple Grid Magnetic Core Mechanical Responses in Novel pulse propulsion Fusion (PuFF) Engine Inertial Electrostatic Confinement Nuclear Fusion Materials and A. Olah, Self, Budapest, Hungary R. Adams, NASA Marshall Space Flight Device Designs Using a Combined Center, Huntsville, AL; J. Cassibry, K. A. Chap, R. Sedwick, University of Computational and Empirical Schillo, University of Alabama, Huntsville, 51 Maryland, College Park, College Park, MD Approach Huntsville, AL M. Rodriguez, J. Cassibry, C. Marlar, J. Evans, University of Alabama, Huntsville, Huntsville, AL Monday, 28 July 2014 44-GTE-6 Turbines I Room 13 Chaired by: J. SMITH, QuEST Global, Inc. and S. LYNCH, Penn State 1430 hrs 1500 hrs 1530 hrs AIAA-2014-3521 AIAA-2014-3522 AIAA-2014-3523 Turbine Blade Aerothermal Long Hole Film Cooling Dataset for Numerical Investigations of Slot- Optimization Using Evolution CFD Development - Flow and Film type Film Cooling of HPT Rotor for Strategies Effectiveness Small Engines D. Curriston, R. Hartfield, Auburn V. Shyam, NASA Glenn Research Center, K. Shi, A. Jemcov, J. Cameron, S. Morris, University, Auburn, AL Cleveland, OH; D. Thurman, Army University of Notre Dame, Notre Dame, Research Laboratory, Cleveland, OH; P. IN; S. Gogineni, Spectral Energies, LLC, Poinsatte, NASA Glenn Research Center, Dayton, OH Cleveland, OH; A. Ameri, Ohio State University, Columbus, OH; P. Eichele, Gilcrest Electric and Supply Company, Cleveland, OH Monday, 28 July 2014 45-GTE-7 Combustors II Room 14 Chaired by: W. ACOSTA, Army Research Laboratory and M. HARRIS, National University Singapore 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630hrs 1600 hrs AIAA-2014-3524 AIAA-2014-3525 AIAA-2014-3526 AIAA-2014-3528 AIAA-2014-3529 AIAA-2014-3527 Simulations of NOx Emissions from Exit Temperature Profile Numerical Prediction of liquid jet in Gas Turbine Fuel Nozzle Durability CFD Computations of Emissions for The Premixed Conditional Moment Low Emissions Discrete Jet Injector Measurement and CFD cross flow using Ω-Y model Assessment Using Detached Eddy LDI-2 Combustors with Simplex and Closure Method with Large Eddy Combustor Tests Comparisons on Small Scale S. Kumar, ANSYS, Inc., Pune, India; K. Simulations and Structural Dynamic Airblast Injectors Simulation of a Backward Facing K. Ajmani, Vantage Partners, LLC, Turbojet Combustor with Air Blast Kurbatskii, ANSYS, Inc., Lebanon, NH; V. Response Analysis K. Ajmani, CFD Nexus, LLC, Cleveland, Reacting Step Cleveland, OH; K. Breisacher, NASA Glenn Atomizer Configuration Kumar, ANSYS, Inc., Pune, India H. Feiz, M. Huffman, General Electric OH; H. Mongia, Purdue University, West C. Velez, University of Central Florida, Research Center, Cleveland, OH C. Catori, A. Topal, TUSAS Engine Company, Greenville, SC Lafayette, IN; P. Lee, Woodward FST, Inc., Orlando, FL Industries, Inc., Eskisehir, Turkey; S. Zeeland, MI Uslu, TOBB University of Economics and Technology, Ankara, Turkey; O. Tuncer, Istanbul Technical University, Istanbul, Turkey; L. Cagan, S. Ozkan, TUSAS Engine Industries, Inc., Eskisehir, Turkey; et al. Monday, 28 July 2014 46-GTE-8 Distributed Engine Controls Room 15 Chaired by: A. BEHBAHANI, Air Force Reseach Laboratory and D. CULLEY, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3530 AIAA-2014-3531 AIAA-2014-3532 AIAA-2014-3533 AIAA-2014-3534 AIAA-2014-3535 A Modular Framework for Modeling Extending the Capabilities of Developing an Integration High-Temperature Sensor and A Review of Fiber Optic Technology Predictive Control Strategy in Hardware Elements in Distributed Closed-Loop Distributed Engine Infrastructure for Distributed Electronics Packaging Technologies for Turbine Engine Instrumentation Distributed Networked Control 52 Engine Control Systems Control Simulations using LAN Engine Control Technologies for Distributed Engine Controls Channel: Control, PHM, and Test Systems for Turbine Engine Under A. Zinnecker, N&R Engineering, Inc., Communication D. Culley, NASA Glenn Research Center, A. Behbahani, Air Force Research Cell Applications Faulty Communication Network Parma Heights, OH; D. Culley, E. Aretskin- E. Aretskin-Hariton, NASA Glenn Research Cleveland, OH; A. Zinnecker, N&R Laboratory, Wright-Patterson AFB, OH; M. Pakmehr, Intelligent Fiber Optic M. Zein-Sabatto, M. Bodruzzaman, Hariton, NASA Glenn Research Center, Center, Cleveland, OH; A. Zinnecker, Engineering, Inc., Parma Heights, OH; E. M. Usrey, Y. Liu, B. Schaible, K. Harsh, Systems Corporation (IFOS), Santa Clara, Tennessee State University, Nashville, TN Cleveland, OH N&R Engineering, Inc., Cleveland, OH; Aretskin-Hariton, NASA Glenn Research Sporian Microsystems, Lafayette, CO CA; A. Behbahani, Air Force Research D. Culley, NASA Glenn Research Center, Center, Cleveland, OH Laboratory, Wright-Patterson AFB, OH; Cleveland, OH B. Moslehi, J. Costa, R. Black, Intelligent Fiber Optic Systems Corporation (IFOS), Santa Clara, CA Monday, 28 July 2014 47-EP-5 Electrospray and Micropropulsion Room 16 Chaired by: H. LEITER, Astrium, an EADS Company and W. Huang, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3536 AIAA-2014-3537 AIAA-2014-3538 AIAA-2014-3539 AIAA-2014-3540 Short Pulse Operation of a Laser- A Short Pulse Laser-Assisted Pulsed Plasma Acceleration Characteristic Characterization of an Ionic Liquid Performance evaluation of Assisted Pulsed Plasma Thruster Plasma Thruster of a Rectangular Laser- Ferrofluid Electrospray Emission micropropulsion systems with H. Hosokawa, N. Akashi, Y. Oigawa, H. Y. Oigawa, N. Akashi, H. Hosokawa, H. Electromagnetic Hybrid Thruster Pattern the application of Active Debris Horisawa, Tokai University, Hiratsuka, Horisawa, Tokai University, Hiratsuka, N. Akashi, Y. Oigawa, H. Hosokawa, H. B. Jackson, L. King, Michigan Removal Japan Japan Horisawa, Tokai University, Hiratsuka, Technological University, Houghton, MI A. Daykin-Iliopoulos, R. Desai, Queen Japan Mary University of London, London, United Kingdom Monday, 28 July 2014 48-HSABP-2/GTE-9 Pulsed Detonation Engines Room 2 Chaired by: D. PAXSON, NASA Glenn Research Center and F. MALO-MOLINA, Air Force Reseach Laboratory 1430 hrs 1500 hrs 1530 hrs AIAA-2014-4033 AIAA-2014-3541 AIAA-2014-3542 Study on Pulse Detonation Unsteady Thrust Measurement for Performance Estimation of Rocket Engine Using Flight Test Pulse Detonation Engine Hydrazine-based PDEs for Demonstrator “Todoroki II” D. Joshi, F. Lu, University of Texas, Spacecraft Applications S. Takagi, Nagoya University, Nagoya, Arlington, Arlington, TX T. Kim, J. Kim, W. Hwang, D. Cho, J. Japan; T. Morozumi, Tsukuba University, Choi, Pusan National University, Busan, Tsukuba, Japan; K. Matsuoka, J. South Korea Kasahara, Nagoya University, Nagoya, Japan; A. Matsuo, Keio University, Tokyo, Japan; I. Funaki, Institute of Space and Astronautical Science, Sagamihara, Japan Monday, 28 July 2014 49-HR-2 Numerical Modeling Approaches in Hybrid Rocket Motor Development Room 20 Chaired by: T. SHIMADA, Japan Aerospace Exploration Agency-Institute of Space Technology and Aeronautics and D. PASTRONE, Politecnico di Torino 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3543 AIAA-2014-3544 AIAA-2014-3545 AIAA-2014-3546 AIAA-2014-3548 Computational Simulation of a HTPB Hybrid Propulsion with Numerical Modeling of GOX/ Development and Three- Development Program for An Counter-Rotating Vortex Pair Mixer Multiple Vortical-Flow Chamber HTPB Hybrid Rocket Flowfields and dimensional Numerical Simulation Advanced In-Line Reusable Launch for Aerospace Applications Designs Comparison with Experiments of a Double-tube Hybrid Rocket Vehicle Concept Using a Small-scale D. Steen, S. Heister, Purdue University, Y. Chen, National Space Organization, D. Bianchi, B. Betti, F. Nasuti, University Motor End-Burning Solid and Hybrid 53 West Lafayette, IN Hsinchu, Taiwan; A. Lai, J. Lin, T. Chou, of Rome “La Sapienza’’, Rome, Italy; C. A. Pons Lorente, N. Yu, P. Zeng, B. Zhao, Rocket Glider Demonstrator S. Wei, J. Wu, National Chiao Tung Carmicino, A. Russo Sorge, University of Beihang University, Beijing, China Approach University, Hsinchu, Taiwan Naples “Federico II”, Naples, Italy A. Baran, C. Blanchard, P. Spyridon, S. Hollander, S. McBride, J. Stewart, Louisiana State University, Baton Rouge, LA Monday, 28 July 2014 50-EST-1 Energy Storage Technology Room 21 Chaired by: S. LIU, The Aerospace Corporation 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3549 AIAA-2014-3551 AIAA-2014-3552 AIAA-2014-3554 The opportunity of energy storage Prediction of Shunt Currents and Lithium-Air Battery Cell IEEE Power & Energy Society Rural in magnetic field by combining Corrosion of Bipolar Plates in PEM Development Electrification Initiative: Community flywheel and ultracapacitor tools Fuel Cell Stacks C. Reid, NASA Glenn Research Center, Solutions Initiative in Africa A. Olah, Self, Budapest, Hungary W. Bennett, NASA Glenn Research Center, Cleveland, OH (Update) Cleveland, OH S. Myers, SD Myers, Tallmadge, OH Monday, 28 July 2014 51-EC-2 Magnetohydrodynamic Systems and Other Advanced Concepts Room 22 Chaired by: E. LEWANDOWSKI, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3556 AIAA-2014-3557 AIAA-2014-3558 AIAA-2014-3559 AIAA-2014-3560 Application of Numerical Simulation of Performance of a Liquid Metal Numerical and Experimental Characteristics of a Loop-type Magnetohydrodynamic Energy Performance of a High MHD Power Generation System for Investigation on the Traveling Thermoacoustic Refrigerator with a Generation to Planetary Entry Temperature Inert Gas Plasma Various External Forces Wave Direct Energy Converter Sound Generator Vehicles Faraday-type MHD Generator with L. Hu, Tokyo Institute of Technology, Concept N. Maruyama, Y. Iwasaki, M. Saito, H. Ali, R. Braun, Georgia Institute of Segmented Electrodes Yokohama, Japan; H. Kobayashi, Keio A. Chap, University of Maryland, College Y. Kitaide, Mie University, Tsu, Japan; Technology, Atlanta, GA M. Tanaka, T. Murakami, Y. Okuno, Tokyo University, Yokohama, Japan; Y. Okuno, Park, College Park, MD; A. Tarditi, Electric K. Takiguchi, S. Ishida, Fuji Electric, Institute of Technology, Yokohama, Japan Tokyo Institute of Technology, Yokohama, Power Research Institute, Inc., Knoxville, Yokkaichi, Japan; et al. Japan TN; J. Scott, NASA Johnson Space Center, Houston, TX Monday, 28 July 2014 52-TES-1 Experiments and Characterizations Room 23 Chaired by: M. PISZCZOR, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3561 AIAA-2014-3562 AIAA-2014-3563 AIAA-2014-3564 Distributed Wind Generator Laminar Flame Properties of Effects of Additives on the Flame On The Mathematical Modeling J. Gieras, United Technologies Pre-Vaporized Palm Methyl Extinction Limits of Propane Flames Of Flow Regimes And Thermal Corporation, Rockford, IL; L. Ribarov, Ester/Diesel Blends at Fuel Rich M. Smeltzer, R. Parthasarathy, S. Characteristics Of Turbulent Flames United Technologies Corporation, Windsor Conditions Gollahalli, University of Oklahoma, In Industrial Furnaces Locks, CT D. Romero, R. Parthasarathy, S. Gollahalli, Norman, Norman, OK E. Khalil, E. Bialy, M. Hassan, A. Ibrahim, 54 University of Oklahoma, Norman, Cairo University, Cairo, Egypt Norman, OK Monday, 28 July 2014 53-PC-3 Propellant and Fuel Development II Room 25 A Chaired by: O. HAIDN, Technische Universität München 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3565 AIAA-2014-3566 AIAA-2014-3567 AIAA-2014-3568 Oral Presentation Reacting Opposed Jets of Effects of Nano-Scale Additives and HTV Numerical Simulation Model Decomposition of Ionic Liquid A Static Combustion Study on Fuel Hypergolic Propellants MMH and Methanol on the Linear Burning of the Helium Solubility in the Ferrofluids for Multi-Mode Rich Propellant for Ducted Rocket RFNA Rates of Aqueous HAN Solutions Propellant Spacecraft Propulsion Gas Generator S. Sardeshmukh, S. Heister, Purdue K. McCown, G. Homan-Cruz, E. Petersen, Y. Kurishita, Mitsubishi, Komaki, Japan S. Berg, B. Coleman, J. Rovey, Missouri K. Shin, J. Won, H. Tak, S. Choi, W. Lee, University, West Lafayette, IN Texas A&M University, College Station, TX University of Science and Technology, Hanwha Corporation, Daejeon, South Rolla, MO Korea; C. Lee, Konkuk University, Seoul, South Korea Monday, 28 July 2014 54-PC-4 Spray Combustion Room 25 B Chaired by: B. CHEHROUDI, European Research Council (ERC) 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3569 AIAA-2014-3570 AIAA-2014-3571 AIAA-2014-3572 AIAA-2014-3573 On The TFNS Sub-Grid Models for Experimental study on the droplet Supercritical Pseudo-Boiling and its Performance Prediction of Agglomeration characteristics of Liquid-Fueled Turbulent Combustion evaporation process and influence Relevance for Transcritical Injection Apogee Attitude and Orbit Control aluminum particles with changing N. Liu, T. Wey, NASA Glenn Research factors D. Banuti, K. Hannemann, German Thruster for MMH/NTO Hypergolic pressure in AP/AN composite Center, Cleveland, OH Y. Ting, Academy of Equipment, Beijing, Aerospace Center (DLR), Göttingen, Bipropellant propellants China Germany Z. Lianbo, X. Xu, Beihang University, K. Takahashi, S. Sakai, M. Nakagaki, T. Beijing, China Sasaki, T. Kuwahara, Nihon University, Funabashi, Japan; T. Shimada, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Monday, 28 July 2014 55-GTE-5 Gas Turbine Engine Room 26 C Chaired by: G. WELCH, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs AIAA-2014-3574 AIAA-2014-3575 AIAA-2014-3576 Study on the optimization design of Experiments in a Heated, Rotating Computational Investigation of a civil turbofan engine Test Rig Simulating a Fuel Cooled Novel Tip Leakage Mitigation M. Cao, Northwestern Polytechnical Turbine Methods for High Pressure Turbine University, Xi’an, China R. Wills, Air Force Research Laboratory, Blades Wright-Patterson AFB, OH; J. Sebastian, A. Gupta, M. Ibrahim, Cleveland State

55 A. Cole, University of Dayton Research University, Cleveland, OH; V. Shyam, NASA Institute, Dayton, OH; S. Panzardi, Glenn Research Center, Cleveland, OH Air Force Research Laboratory, Wright- Patterson AFB, OH Monday, 28 July 2014 56-LP-5 Cryogenic Propellant Storage and Transfer (CPST) Room 3 Chaired by: M. MEYER, NASA Glenn Research Center and H. KAGAWA, JAXA 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3577 AIAA-2014-3578 AIAA-2014-3579 AIAA-2014-3580 AIAA-2014-3581 AIAA-2014-3582 The Cryogenic Propellant Self-Pressurization and Spray Cryogenic Boil-Off Reduction Recent Rapid Depressurization Tank Applied Testing of Load- An RF Sensor for Gauging Screen- Storage and Transfer Technology Cooling Simulations of the System Testing Testing of Multilayer Systems Bearing Multilayer Insulation Channel Liquid Acquisition Devices Demonstration Mission: Progress Multipurpose Hydrogen Test Bed D. Plachta, R. Christie, J. Feller, W. W. Johnson, NASA Kennedy Space Center, (LB-MLI) for Cryogenic Propellants and Transition (MHTB) Ground-Based Experiment Johnson, NASA Glenn Research Center, Cape Canaveral, FL W. Johnson, NASA Kennedy Space Center, G. Zimmerli, NASA Glenn Research Center, M. Meyer, S. Motil, C. Ginty, M. Melis, O. Kartuzova, M. Kassemi, J. Moder, Cleveland, OH Cape Canaveral, FL; D. Plachta, NASA Cleveland, OH; S. Metzger, Vantage NASA Glenn Research Center, Cleveland, J. Agui, NASA Glenn Research Center, Glenn Research Center, Cleveland, OH; J. Partners, LLC, Brook Park, OH; M. OH Cleveland, OH Valenzuela, NASA Marshall Space Flight Asipauskas, NASA Glenn Research Center, Center, Huntsville, AL; J. Feller, NASA Cleveland, OH Ames Research Center, Moffett Field, CA Monday, 28 July 2014 57-LP-6 Injectors I Room 4 Chaired by: I. LEYVA and S. CHIANESE, SpaceX 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3583 AIAA-2014-3584 AIAA-2014-3585 AIAA-2014-3586 AIAA-2014-3587 Computational Characterization of Mixing Analysis of Like Doublet Effects of Wall-injection Length Numerical Study on the The Preliminary Study of Oxygen- the Feedback Free Fluidic Oscillator Injectors in High Pressure on Spray Core and Combustion Atomization Characteristics of Centered Kerosene-Swirl Coaxial E. Meier, S. Heister, Purdue University, Environments for Gelled Propellant Performance in a Coaxial Porous Double-Swirl Coaxial Injector Injector West Lafayette, IN Simulants Injector Z. Gang, N. Wan-sheng, F. Wei, Q. Ye, L. Xuan, L. Tian, Beihang University, J. Lee, C. Ramasubramanian, V. Notaro, D. Kim, J. Koo, Korea Aerospace Academy of Equipment, Beijing, China Beijing, China; H. Jinli, China Aerospace University of Cincinnati, Cincinnati, OH University, Goyang, South Korea Science and Industry Corporation (CASIC), Beijing, China; Z. Shaohua, X. Xu, Beihang University, Beijing, China Monday, 28 July 2014 58-LP-7 Spacecraft Propulsion Systems I Room 5 Chaired by: C. GATTO, Jet Propulsion Laboratory and C. KIRCHBERGER 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3588 AIAA-2014-3589 AIAA-2014-3590 AIAA-2014-3885 AIAA-2014-3591 AIAA-2014-3592 Design, Integration, Certiﬁcation Development and Flight Operation On-Orbit Propulsion System Basic Characteristics of Discharge Dawn Spacecraft Reaction Control Development of a Small Green and Testing of the Orion Crew of a 5 lbf to 20 lbf O2/CH4 Performance of ISS Visiting Vehicles Plasma Ignition System for System Flight Experience Bipropellant Rocket Engine Using Module Propulsion System Roll Control Engine for Project M. Martin, R. Swanson, U. Kamath, 1N-class RCS Thruster with Green M. Mizukami, B. Nakazono, Jet Propulsion Hydrogen Peroxide as Oxidizer H. McKay, R. Freeman, G. Cain, Lockheed Morpheus The Boeing Company, Houston, TX; F. Monopropellant Laboratory, California Institute of A. Okninski, B. Bartkowiak, K. Sobczak, Martin Corporation, Littleton, CO; J. J. McManamen, E. Hurlbert, D. Kroeger, Hernandez, V. Spencer, NASA Johnson T. Iizuka, T. Shindo, A. Wada, S. Technology, Pasadena, CA D. Kublik, P. Surmacz, G. Rarata, Institute Albright, R. Schoenberg, NASA Johnson NASA Johnson Space Center, Houston, TX Space Center, Houston, TX Kawabata, Y. Sato, J. Aoyagi, Tokyo of Aviation, Warsaw, Poland; et al.

56 Space Center, Houston, TX; R. Delventhal, Metropolitan University, Hino, Japan; et al. NASA Glenn Research Center, Cleveland, OH Monday, 28 July 2014 59-ABPSI-2 Inlets I Room 6 Chaired by: A. Delot, ONERA and R. Scharnhorst, Boeing Defense, Space & Security 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3593 AIAA-2014-3594 AIAA-2014-3595 AIAA-2014-3596 Methodology for the Design Approach for an Optimized CFD Investigations on the Influence Sensitivity Analysis of a Highly of Streamline-Traced External- Evaluation of Pressure and Swirl of varying Inflow Conditions on Loaded Turboprop S-Duct Intake by Compression Supersonic Inlets Distortion in S-Shaped Engine Inlet the Aerodynamics in an S-Shaped CFD Methods J. Slater, NASA Glenn Research Center, Configurations Inlet Duct C. Atalayer, D. Wulff, J. Friedrichs, Cleveland, OH R. Rademakers, T. Kächele, S. Bindl, R. S. Brehm, T. Kächele, R. Niehuis, Technical University of Braunschweig, Niehuis, University of the German Federal University of the German Federal Armed Braunschweig, Germany Armed Forces, Munich, Germany Forces, Munich, Germany Monday, 28 July 2014 60-SCP-1 Advanced Seal Technology Room 7 Chaired by: P. DUNLAP, NASA Glenn Research Center; B. STEINETZ, NASA Glenn Research Center and N. SARAWATE, GE Global Research 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs Oral Presentation AIAA-2014-3597 AIAA-2014-3598 Oral Presentation Oral Presentation AIAA-2014-3599 AIAA-2014-3600 Seals Past, Present, and Future Rotating Brush Seal Aggregation of Experimental and Development of Laminated Seals An Overview of High Temperature An Overview of Advanced Implementation of Statistical R. Chupp, Self, Simpsonville, SC X. Zheng, M. Mack, D. Trivedi, N. Theoretical Data for Brush Seal for Stator-Stator Sealing in Gas Seal Development and Testing Elastomeric Seal Development and Process Control: Evaluating the Sarawate, C. Wolfe, General Electric Leakage Evaluation Turbines Capabilities at the NASA Glenn Testing Capabilities at NASA Glenn Mechanical Performance of a Company, Schenectady, NY A. Pugachev, Technical University of N. Sarawate, General Electric Company, Research Center Research Center Candidate Silicone Elastomer Munich, Garching, Germany Niskayuna, NY; V. Morgan, D. Weber, J. Demange, University of Toledo, Toledo, P. Dunlap, NASA Glenn Research Center, Docking Seal General Electric Company, Greenville, SC OH; P. Dunlap, J. Finkbeiner, M. Proctor, Cleveland, OH H. Oravec, C. Daniels, University of Akron, NASA Glenn Research Center, Cleveland, Akron, OH OH Monday, 28 July 2014 61-EDU-2 Propulsion Education II Room 8 Chaired by: J. MILLER, George C. Marshall Space Flight Center and M. HITT, The University of Alabama in Huntsville 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3601 AIAA-2014-3602 AIAA-2014-3603 AIAA-2014-3604 Texas Center for Undergraduate Dimensioning a Simplex Swirl Multi-Disciplinary Design of Strategies for Successful University, Research in Energy and Propulsion: Injector a Supersonic, Long-Range, Industry, and Government An NSF REU Site at Texas A&M R. Nardi, S. Neto, A. Pimenta, Air-Superiority Missile Through Collaborations University Technological Institute of Aeronautics Parametric Design Space R. Frederick, University of Alabama, E. Petersen, T. Sammet, D. Ranjan, Texas (ITA), São José dos Campos, Brazil; Exploration and Physics-Based Huntsville, Huntsville, AL A&M University, College Station, TX V. Perez, Inotech Ltda, São José dos Modeling 57 Campos, Brazil A. Sanders, C. Jenista, S. Gordon, R. Donnan, J. Goodman, R. Arrowood, Georgia Institute of Technology, Atlanta, GA; et al. Monday, 28 July 2014 62-EP-8 Qualification and Flight Programs Room 9 Chaired by: D. GOEBEL, Jet Propulsion Laboratory 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3605 AIAA-2014-3606 AIAA-2014-3607 AIAA-2014-3608 AIAA-2014-3609 AIAA-2014-3610 Status of propulsion technology Qualification of the SPT-140 for In-Flight Operation of the Dawn Ion Development, Qualification and R&D, Launch and Initial Operation Development of Electrothermal development under the NASA use on Western Spacecraft Propulsion System Through Year Integration of the VENµS PPU of the Osaka Institute of Pulsed Plasma Thruster Systems In-Space Propulsion Technology J. Delgado, Space Systems/Loral, Palo Two of Cruise to Ceres A. Davidson, P. Gontmacher, J. Herscovitz, Technology 1st PROITERES Nano- onboard Osaka Institute of program Alto, CA M. Rayman, C. Garner, California Institute I. Tidhar, Rafael, Haifa, Israel Satellite with Electrothermal Pulsed Technology PROITERES Nano- D. Anderson, NASA Glenn Research Center, of Technology, Pasadena, CA Plasma Thrusters and Development Satellites Cleveland, OH; J. Dankanich, NASA of the 2nd and 3rd Satellites R. Fujita, H. Tahara, Osaka Institute of Marshall Space Flight Center, Huntsville, T. Kamimura, H. Tahara, Osaka Institute of Technology, Osaka, Japan AL; H. Kamhawi, M. Patterson, E. Pencil, Technology, Osaka, Japan L. Pinero, NASA Glenn Research Center, Cleveland, OH; et al. Monday, 28 July 2014 63-ET-2 Meeting Education Demands of Future Energy Systems Room 24 1500 - 1800 hrs Panel 1: Power & Energy Systems: A Transformative Approach to Education Students working on undergraduate and graduate degrees in the area of power and energy systems have been taught the same way for decades. With the movement toward more diverse, distributed and advanced power generation such as liquid fluoride thorium nuclear reactors, fracking, geothermal, solar, wind, and in conjunction with smart grids, the entire educational process needs to be assessed and revised. This panel will explore this and respond with suggested changes that need to be made. An example of a change that needs to occur is the addition of one or more required courses in systems engineering at both the undergraduate and graduate levels that can better prepare students for future engineering challenges. The panel will include representative from industry and government, as well as academics. Moderator: Chuck Alexander , Cleveland State University Panelists: Michael Ahern, WPI / Power Systems Sridhar Kota, FlexSys Inc. / U of M (invited) Timothy Croshore, First Energy (invited) Panel 2: Power & Energy Future Directions Ongoing developments in photovoltaic and wind generation, electro-chemical and flywheel energy storage, geothermal through fracking, increased use of natural gas for electrical power generation, Brayton and Stirling conversion, and micro-grid and smart grid technologies are all of interest when considering the future state of the electric utility power system. Technology infusion in the electric power grid will encompass some of these technologies through evolution, but others are far more disruptive and will require significant changes for the electric power industry. This panel will explore the state of these technologies and the challenges for the utility industry and the barriers for the technology companies advocating their usage. Moderator: Ray Beach, NASA GRC Panelists: Jeff Landis, NASA GRC Joe Beno , U of T / CEM Neil Snyder, NREL Larry Viterna , Nautica Wind Power Monday, 28 July 2014

58 64-PANEL-2 Assuring Critical System Behavior in an Era of Increasing Complexity and Change Room 26 A 1500 - 1800 hrs As power and energy systems continue to increase in complexity, the challenges of meeting full stakeholder objectives of achieving desirable “system behavior,” while assuring compliance with safety and environmental laws, continue to grow. This panel will focus on the critical aspect of system behavior, examining the relevance and interaction of each component within a system to influence overall behavior and achieve desired outcomes. Such an “integrated” perspective is at the core of systems engineering methodology, essential to avoid risks and exploit opportunities throughout the system life cycle. Moderator: John Thomas, John A. Thomas & Associates, LLC Panelists: David Long, President and CEO, Vitech Corp Paul Nielson, CEO, Software Engineering Institute Eric Gebhardt, Chief Technology Officer and Vice President Engineering, GE Oil & Gas John Wade, Professor, Stevens Institute of Technology Don Burns, Head of Innovation Systems Engineering, Rolls-Royce Corporation Monday, 28 July 2014 65-PANEL-7 JPC 50th Anniversary Pioneers Session: Celebrating the Past, Influencing the Future Room 26 B 1500 - 1800 hrs In this session we will celebrate 50 years of the Joint Propulsion Conference. Pioneers from industry, government, and academia will share their experiences and discuss how their achievements will influence the next generation of aerospace history. Following this portion of the program, several young professionals will interview the speakers and take questions from the audience. Moderator/Emcee: Ted Fecke, Retired USAF Senion Leader for Propulsion,Universal Technologies Corporation Participants: Mike Benzakein, Director, Executive Partnerships in Aerospace, Aviation, and Flight, The Ohio State University Tony Strazisar, NASA (retired) Thomas Curran, Universal Technologies Corp. Lawrence Ross, NASA (retired) Joe Nieberding, NASA (retired) James Day, USAF (retired) Ed Greitzer,H.N. Slater Professor of Aeronautics and Astronautics, Massachusetts Institute of Technology Jim Johnson, Belcan Interviewers: Lance Foster, NASA Glenn Research Center Zachary Grunder, Lockheed Martin Corporation Monday, 28 July 2014 66-NW-3 Exposition Reception Exhibit Hall C 1800 - 1930 hrs Monday, 28 July 2014 67-PANEL-13 Rising Leaders in Aerospace: Town Hall: Where’s MY Apollo Vision for the Future? Room 5

59 1930 - 2130 hrs These professionals will be fielding YOUR questions: What is the future of propulsion? What are the cutting-edge technologies in space propulsion? What is happening that can motivate me or my colleagues? Come prepared with questions as the panel will have a 60- minute Q&A session dedicated solely to answering your questions. If you would like, or prefer, you may forward your questions ahead of time. Questions can be sent to [email protected] or [email protected]. Moderator: Christine Pastor-Barsi, Sierra-Lobo, Inc. Panelists: Jeff Thornburg, SpaceX Mike Kynard, NASA Marshall Space Flight Center Curtis Johnson, Blue Origin Robyn Ringuette, Virgin Galactic Tuesday Tuesday, 29 July 2014 68-PLENARY-3 Future Trends, Opportunities and Challenges at the Nexus of Aviation, Aerospace and Energy Grand Ballroom A 0800 - 0900 hrs Alton Romig will share his ideas on the future of high energy and power technologies and how the growing demands on these systems will influence the design of future aerospace vehicles. Alton Romig, Vice President, Engineering and Advanced Systems, Lockheed Martin Aeronautics Tuesday, 29 July 2014 69-NW-4 Networking Coffee and Pastries in Exposition Hall Exhibit Hall C 0900 - 0930 hrs Tuesday, 29 July 2014 70-SB-2 Speaker Briefing Session Rooms 0900 - 0930 hrs Please meet your session chairs at 0900 hrs in your session room to load presentations for both the morning and afternoon sessions Tuesday, 29 July 2014 71-SR-5 Solid Rocket Motor Combustion and Acoustic Instabilities II Room 1 Chaired by: E. CAVALLINI, University of Roma “La Sapienza” and W. RYAN, United Launch Alliance, LLC 0930 hrs 1000 hrs AIAA-2014-3611 AIAA-2014-3612 Two-Phase Flow Stability of High-order computation of burning Cylindrically-Shaped Hybrid propellant surface and simulation and Solid Rockets with Particle of fluid flow in solid rocket Entrainment chamber T. Elliott, J. Majdalani, Auburn University, D. Gueyffier, F. Roux, Y. Fabignon, ONERA, Auburn, AL Palaiseau, France; G. Chaineray, N. Lupoglazoff, F. Vuillot, ONERA, Châtillon, France; et al. Tuesday, 29 July 2014 72-EP-10 NEXT Ion Thruster Room 10 Chaired by: J. SNYDER, Jet Propulsion Laboratory and G. WILLIAMS, Ohio Aerospace Institute 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3613 AIAA-2014-3615 AIAA-2014-3617 Computational Speed-Up Molybdenum Density and Flux in End-of-test Performance and Techniques for a PIC-MCC Computer NEXT Ion Engine Plume Wear Characterization of NASA’s Model for Use in Modeling the M. Crofton, M. Smith, The Aerospace Evolutionary Xenon Thruster Plasma in an Ion Engine Discharge Corporation, El Segundo, CA; M. Patterson, (NEXT) Long-Duration Test Chamber NASA Glenn Research Center, Cleveland, R. Shastry, D. Herman, G. Soulas, M. J. Menart, T. Godar, J. Ren, Wright State OH Patterson, NASA Glenn Research Center,

60 University, Dayton, OH; S. Mahalingam, P. Cleveland, OH Stoltz, Tech-X Corporation, Boulder, CO Tuesday, 29 July 2014 187-ITAR-1 Topics In Electric and Solid Propulsion Room 16 Chaired by: T. SWANSON, AEDC and J. HANSEN, United Launch Alliance 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3614 AIAA-2014-3616 AIAA-2014-3618 AIAA-2014-3619 Verification of Electromagnetic Flexible, Self-Addressable and A Reacting Multi-phase Flow Model A One-Dimensional Global-Scaling Acceleration in Electric Solid Directional Microplasma Thrusters for Solid Rocket Motor Analysis Erosive Burning Model Informed by Propellant Microthrusters (consider Using Hollow-Core Optical Fibers (consider for ITAR Session) Blowing Wall Turbulence for ITAR session) and Jet-to-Jet Coupling Effect D. Black, A. Eaton, ATK, Brigham City, UT T. Kibbey, Jacobs, Huntsville, AL S. Williams, W. Sawka, J. Thrasher, Digital (consider for ITAR Session) Solid State Propulsion, LLC, Reno, NV C. Park, D. Kim, S. Kim, J. Ballato, T. Hawkins, Clemson University, Clemson, SC Tuesday, 29 July 2014 73-EP-11 Hall Thrusters - Modeling Room 11 Chaired by: V. KHAYMS, Lockheed Martin Space Systems and M. WALKER, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3620 AIAA-2014-3621 AIAA-2014-3622 Power dependence of the electron A New Cell-Centered Implicit Modeling of Electron Fluids in mobility profile in a Hall thruster Numerical Scheme for Ions in the Hall Thrusters Using a Hyperbolic B. Jorns, R. Hofer, I. Mikellides, Jet 2-D Axisymmetric Code Hall2De System Propulsion Laboratory, California Institute A. Lopez Ortega, I. Mikellides, Jet R. Kawashima, K. Komurasaki, H. of Technology, Pasadena, CA Propulsion Laboratory, California Institute Koizumi, University of Tokyo, Tokyo, Japan of Technology, Pasadena, CA Tuesday, 29 July 2014 74-NFF-3 Nuclear Thermal Propulsion II - Missions, Vehicles & Architectures Room 12 Chaired by: J. WARREN, NASA Headquarters and B. SCHNITZLER, Oak Ridge National Lab 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3623 AIAA-2014-3624 AIAA-2014-3625 AIAA-2014-3626 Copernicus-B: A Bimodal NTR Integrated System Modeling for A Crewed Mission to Apophis Using Missions to Sun-Mars L1 Lagrange Artificial Gravity MTV Option for Nuclear Thermal Propulsion (NTP) a Hybrid Bimodal Nuclear Thermal Point Using Bimodal Nuclear Future NASA Mars Exploration S. Ryan, S. Borowski, NASA Glenn Electric Propulsion (BNTEP) System Thermal Electric Propulsion Missions Research Center, Cleveland, OH D. McCurdy, Vantage Partners, LLC, B. Cassenti, University of Connecticut, S. Borowski, NASA Glenn Research Center, Cleveland, OH; S. Borowski, L. Burke, Storrs, Storrs, CT; D. McCurdy, Vantage Cleveland, OH; D. McCurdy, T. Packard, NASA Glenn Research Center, Cleveland, Partners, LLC, Cleveland, OH; S. Borowski, Vantage Partners, LLC, Brook Park, OH OH; T. Packard, Vantage Partners, LLC, NASA Glenn Research Center, Cleveland, Cleveland, OH OH Tuesday, 29 July 2014 75-GTE-10 Combustors III Room 13 Chaired by: K. TACINA, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3627 AIAA-2014-3628 AIAA-2014-3629 AIAA-2014-3630 NASA Numerical and Experimental Demonstration of an Automatic Intermediate Pressure Combustion Experimental Characterization Evaluation of UTRC Low Emissions Meshing Approach for Simulation Research of a Multipoint Low NOx of the Reaction Zone in an Ultra- Injector of a Liquid Fueled Gas Turbine with Combustion System Compact Combustor Y. Hicks, S. Tedder, R. Anderson, A. Detailed Chemistry G. Zink, S. Pack, J. Ryon, J. Goeke, T. Erdmann, D. Burrus, J. Gross, Innovative Iannetti, NASA Glenn Research Center, S. Drennan, Convergent Science, Inc., United Technologies Corporation, West Des Scientific Solutions, Inc., Dayton, OH; D. Cleveland, OH; L. Smith, Z. Dai, United New Braunfels, TX Moines, IA Shouse, C. Neuroth, A. Lynch, Air Force

61 Technologies Corporation, East Hartford, CT Research Laboratory, Wright-Patterson AFB, OH; et al. Tuesday, 29 July 2014 76-GTE-11 Compressors II Room 14 Chaired by: G. WELCH, NASA Glenn Research Center and M. HATHAWAY, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3631 AIAA-2014-3632 AIAA-2014-3633 AIAA-2014-3634 RANS Simulations for Sensitivity Aerodynamic Performance of Analysis of Stable Rotating Stall in Research on Mechanical Analysis of Compressor Transition a High Efﬁciency Centrifugal a High Speed Axial Compressor Characteristics of Structure for Duct Compressor at the Stage and J. Dantonio, S. Morris, J. Cameron, Compressor Disc with Similarity I. Milanovic, University of Hartford, West Subcomponent Level University of Notre Dame, Notre Dame, IN Scaling Features Hartford, CT; J. Whiton, R. Florea, S. E. Braunscheidel, G. Welch, NASA Glenn D. Tian, AVIC Shenyang Engine Design Lynch, G. Tillman, M. Stucky, United Research Center, Cleveland, OH; G. and Research Institute, Shenyang, China; Technologies Corporation, East Hartford, CT Medic, O. Sharma, United Technologies L. Jin, Shenyang Jianzhu University, Corporation, East Hartford, CT Shenyang, China Tuesday, 29 July 2014 77-GTE-12 Engine controls Room 15 Chaired by: J. LITT, NASA Glenn Research Center and A. BEHBAHANI, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3635 AIAA-2014-3636 AIAA-2014-3637 AIAA-2014-3638 AIAA-2014-3639 Adaptive Life Extending Control of Towards Run-time Assurance of Application and Evaluation of Air Breathing Propulsion Controls A Riccati Equation based Robust Aircraft Engine Advanced Propulsion Algorithms Control Modes for Risk-Based and Diagnostics Research at NASA Control Design with Application to a G. YingQing, C. Xiaolei, X. Du, E. Wong, NASA Glenn Research Engine Performance Enhancements Glenn under NASA Aeronautics Gas Turbine Engine Leading Toward Northwestern Polytechnical University, Center, Cleveland, OH; J. Schierman, Y. Liu, N&R Engineering, Inc., Parma Research Mission Programs Distributed Control Xi’an, China T. Schlapkohl, Barron Associates, Inc., Heights, OH; J. Litt, NASA Glenn Research S. Garg, NASA Glenn Research Center, J. Kratz, R. Yedavalli, Ohio State Charlottesville, VA; A. Chicatelli, Vantage Center, Cleveland, OH; T. Sowers, Vantage Cleveland, OH University, Columbus, OH Partners, LLC, Brook Park, OH Partners, LLC, Cleveland, OH; A. Owen, Self, Cleveland, OH; T. Guo, NASA Glenn Research Center, Cleveland, OH Tuesday, 29 July 2014 78-APS-2 Aircraft Electrical Power Systems Room 2 Chaired by: D. ALLEN 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3640 AIAA-2014-3641 AIAA-2014-3642 AIAA-2014-3643 AIAA-2014-3644 High Power Density Modular A 200 °C Custom CMOS Chipset for Numerical Analysis of Large-Scale Aerospace Fuel Cell Rapid Propulsion Electric Grid Simulator Electric Power System for Distributed Control Applications Tip-Driving Electric Motors for Prototyping Power System Concept (PEGS) for Future Turboelectric Aerospace Applications S. Majerus, Case Western Reserve Thrust Fan S. Okaya, Japan Aerospace Exploration Distributed Propulsion Aircraft S. Steffan, G. Semrau, Moog, East University, Cleveland, OH; W. Merrill, K. Okai, T. Himeno, T. Watanabe, Agency (JAXA), Kanagawa, Japan B. Choi, G. Brown, C. Morrison, T. Dever, Aurora, NY Bluberry, LLC, Columbia Station, OH; D. University of Tokyo, Bunkyo, Japan; H. NASA Glenn Research Center, Cleveland, Goff, S. Garverick, Case Western Reserve

62 Nomura, Nihon University, Narashino, OH University, Cleveland, OH Japan; T. Tagashira, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Tuesday, 29 July 2014 79-HR-3 Novel Fuel Oxidizer Formulations Room 20 Chaired by: S. WHITMORE, Utah State University and A. KARABEYOGLU, Space Propulsion Group Inc. 0930 hrs 1000 hrs AIAA-2014-3646 AIAA-2014-3647 Evaluation of Parafﬁn-based Fuels Evaluation of Fuel Additives for for Hybrid Rocket Engines Hybrid Rockets and SFRJ Systems M. Kobald, German Aerospace Center A. Karabeyoglu, KOC University, Istanbul, (DLR), Hardthausen, Germany; E. Toson, Turkey; U. Arkun, ROKETSAN Missiles Technical University of Milan, Milano, Italy Industries, Inc., Ankara, Turkey Tuesday, 29 July 2014 80-APC-1 Advanced Space Transportation Concepts Room 21 Chaired by: R. CHASE, ANSER and J. ROBINSON, Retired f/Boeing 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3648 AIAA-2014-3649 AIAA-2014-3650 AIAA-2014-3651 AIAA-2014-3652 Choices for Long Term Sustainable An Analysis and Review of Mostly-Reusable LOX/H2 Space Supersonic Sub-Orbital Aircraft for Space Billets - How to fund manned Space Exploration and Habitation Measures and Relationships in Transportation Concept Enabled Earth to Orbit mission lunar missions with current NASA with Recommended Near Term Space Transportation Affordability through Advanced Technologies D. Thorpe, R. Rhodes, J. Robinson, Budget Focus C. McCleskey, E. Zapata, R. Rhodes, NASA J. Robinson, Propellant Supply Technology, Space Propulsion Synergy Team, Mount D. Thorpe, Space Propulsion Synergy R. Rhodes, E. Henderson, J. Robinson, Kennedy Space Center, Cape Canaveral, FL Seal Beach, CA; R. Rhodes, NASA Kennedy Sterling, KY Team, Mount Sterling, KY Space Propulsion Synergy Team, Mount Space Center, Cape Canaveral, FL; E. Sterling, KY Henderson, NASA Johnson Space Center, Houston, TX Tuesday, 29 July 2014 81-EC-3 Thermoelectric Conversion Systems Room 22 Chaired by: J. FLEURIAL, Jet Propulsion Lab 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3653 Oral Presentation Oral Presentation

An Improved Simulation Model for Thermoelectric properties of CoxNi4- Skutterudite-based Advanced Thermoelectric Power Generator xSb12-ySny Ternary Skutterudites Thermoelectric Couples for Element J. Mackey, University of Akron, Akron, Integration into an Enhanced- G. Wu, X. Yu, Case Western Reserve OH; F. Dynys, NASA Glenn Research MMRTG University, Cleveland, OH Center, Cleveland, OH; A. Sehirlioglu, Case T. Caillat, S. Firdosy, B. Li, C. Huang, D. Western Reserve University, Cleveland, OH Uhl, K. Smith, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; et al. Tuesday, 29 July 2014 82-TM-2 Heating and Cooling of Buildings Room 23 Chaired by: E. KHALIL, Cairo University and J. DARKWA, University of Nottingham-Ningbo 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3654 AIAA-2014-3655 AIAA-2014-3656 AIAA-2014-3657 AIAA-2014-3658 Numerical Investigations of Effect of Ventilation Rate and Numerical Investigations of the Thermal management of an Air- Thermal Enhancement of Solid Thermal management in Places of Gaseous Contaminant Density on Air Flow Patterns and Temperature Conditioned Open-air Cafe’: Wind Desiccant Packed Bed Dehumidiﬁer Worship Indoor Air Quality in a Chemical Distribution in a Museum Effects Under Forced Convection in E. Khalil, Cairo University, Cairo, Egypt Laboratory Showroom, King Tutankhamuns’S E. Bialy, E. Khalil, Cairo University, Cairo, Subsonic Flow Regime A. A. Shaaban, E. Khalil, M. Fouad, S. Gallery, Egyptian Museum Egypt S. Yeboah, J. Darkwa, University of Morcos, Cairo University, Cairo, Egypt A. Zaki, E. Khalil, E. Bialy, W. Nottingham, Ningbo, China

63 AbdelMaksoud, Cairo University, Cairo, Egypt Tuesday, 29 July 2014 83-ET-3 Energy Evolution - Achieving Control and Sustainability Room 24 0930 - 1200 hrs Panel 1: The Evolving Smart Grid: Managing Risk with Hybrid Controls and Advanced Technology The emergence of distributed energy resources, increases in renewables, long distance transmission, and retirements of coal plants are changing the fundamental operating assumptions that seasoned operators have relied on to keep the grid running. Combined with the retirement of the most experienced operators, the risk of blackouts is increasing, perhaps dramatically. This panel will discuss the likely extent of these emerging issues, as well as potential solutions, including “smart: grid” technologies. The panel will look at several opportunities for coordination across the segments of the grid (end use, distribution, transmission, and generation) to provide continued reliability and enhanced resiliency by utilizing hybrid control schemes that allow for autonomous local actions to support central grid management functions. Moderator: Jason Black, Battelle Labs Panelists: Fred DiCenzo, Rockwell Automation Dr Ankur Ganguli, Eaton Corp Jason Black, Battelle Labs Panel 2: Sustainability and Complexity in Energy Systems This panel will focus on a comprehensive review of the current state of alternative, sustainable energy sources and their projected evolution for providing effective solutions for current and future energy needs. A key element will be focusing on the realities of what is possible, both technically and economically. On one hand, the release of new IPCC reports is once again igniting the debate on anthropogenic causes for climate change, and the resulting need to massively change our energy systems. On the other hand, the development of enhanced techniques for directional drilling and hydraulic fracturing is opening up vast new reserves of natural gas, driving down prices far below the levels where many renewable energy technologies can currently compete. Finally, energy production, distribution, and consumption must be viewed as an extremely complex system of systems. Moderator: Neil Snyder, NREL Panelists: Susan Raftery, AGROWN LLC Neil Snyder, NREL Mike Piszczor, NASA GRC Tuesday, 29 July 2014 84-PC-5 Combustion Diagnostics I Room 25 A Chaired by: C. CADOU, University of Maryland 0930 hrs 1000 hrs AIAA-2014-3659 AIAA-2014-3660 Gas Phase Velocity Measurements Chemiluminescence as a diagnostic in a Swirled Air/Kerosene Burning in studying combustion instability Spray downstream from an Actual in a practical combustor Turbojet Injection System M. Bedard, Purdue University, West R. Lecourt, L. Rossoni, S. Goyer, ONERA, Lafayette, IN; M. Tanabe, Nihon University, Mauzac, France; G. Linassier, ONERA, Tokyo, Japan; T. Fuller, W. Anderson, Toulouse, France Purdue University, West Lafayette, IN Tuesday, 29 July 2014 85-PC-6 Combustion Modeling and Simulation II Room 25 B Chaired by: M. ANAND, Rolls-Royce Corp 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3661 AIAA-2014-3662 Oral Presentation AIAA-2014-3663 AIAA-2014-3664 Development of Reduced Kinetic A Reduced Mechanism for Jet-Stirred Reactor Studies of Jet Incorporation of Path Flux and Ignition Characteristics of Models for Petroleum-Derived and Combustion of Jet-A in LDI Fuels and a Reduced Mechanism Steepest Descent Methods in Alternative Jet Fuels under Vitiated Alternative Jet Fuels Combustor CFD Calculations for a Jet Fuel Kinetic Model Reduction for CFD Conditions S. Dooley, University of Limerick, Limerick, K. Ajmani, Vantage Partners, LLC, K. Kundu, R. Chapek, K. Ajmani, NASA Applications P. Gokulakrishnan, C. Fuller, M. Klassen, Ireland; S. Won, F. Haas, J. Santner, Y. Cleveland, OH; K. Kundu, NASA Glenn Glenn Research Center, Cleveland, OH A. Abdulrahman, J. Leylegian, Manhattan Combustion Science & Engineering, Inc., Ju, Princeton University, Princeton, NJ; Research Center, Cleveland, OH; S. College, Riverdale, NY Columbia, MD; B. Kiel, Air Force Research T. Farouk, University of South Carolina, Yungster, Ohio Aerospace Institute, Brook Laboratory, Wright-Patterson AFB, OH

64 Columbia, Columbia, SC; et al. Park, OH Tuesday, 29 July 2014 86-PANEL-3 Educating The Next Generation of Propulsion Engineers - Are Changes Needed to Better Prepare the Future Workforce? Room 26 A 0930 - 1200 hrs With the advent of new technologies, the college engineering curriculum has always changed to keep up with the demands placed on young engineers. But as the curriculum has changed, have we forgotten something important? A panel of educators and leaders from government, industry, and universities will discuss the skills that are needed to be successful in today’s environment and identify critical shortfalls or areas that they see as lacking in the preparation of young engineers. Moderator: Nicholas Garafolo, Assistant Professor, Mechanical Engineering, University of Akron Panelists: Lisa Teague, Director, Research and Technology, Rolls-Royce Corporation Dimitri Mavris, Director, ASDL, Georgia Tech Mike Benzakein, Director, Executive Partnerships in Aerospace Aviation, and Flight, The Ohio State University Jose Camberos, Senior Research Aerospace Engineer, Air Force Research Laboratory Paul Orkwis, Department Head and Professor of Aerospace Engineering and Engineering Mechanics, University of Cincinnati Tuesday, 29 July 2014 87-PANEL-8 Advanced Terrestrial Energy Technologies: Generation, Storage, Distribution Room 26 B 0930 - 1200 hrs Recent years have seen enormous shifts in energy usage, generation and outlooks. Renewables have increased in penetration dramatically, led by photovoltaics. Low cost natural gas is reaching the market, offsetting pollutants from traditional generation. The greater penetration of renewables leads to several technological challenges, including the widescale generation, distribution, and storage of energy and efﬁcient usage on the next grid. Moderator: Timothy J. Peshek, Research Professor of Materials Science and Engineering, Case Western Reserve University Panelists: Robert Savinell, George Dively Professor of Chemical Engineering at Case Western Reserve University Ina T. Martin, Director of Operations, Materials for Optoelectronic Research and Education (MORE) Center at Case Western Reserve University James Soeder, Senior Technologist for Power, NASA Glenn Research Center Emily Pentzer, Professor of Chemistry at Case Western Reserve University Tuesday, 29 July 2014 88-HSABP-3 High-Speed Airbreathing Propulsion I Room 26 C Chaired by: W. O’BRIEN, Virginia Tech and D. MACINNIS, Raytheon Missile Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3665 AIAA-2014-3666 AIAA-2014-3667 AIAA-2014-3668 Numerical investigation on the One-dimensional impulse analysis Boundary Layer Combustion for Computational Analysis of Existing supersonic combustion of liquid on the scramjet combustor Skin Friction Drag Reduction in and Altered Rotating Detonation kerosene in a dual-staged strut Z. Yongsheng, Beihang University, Beijing, Scramjet Combustors Engine Inlet Designs based scramjet combustor China R. Clark, S. Bade Shrestha, Western W. Stoddard, A. St. George, R. Driscoll, L. Gang, Beihang University, Beijing, China Michigan University, Kalamazoo, MI E. Gutmark, University of Cincinnati, Cincinnati, OH Tuesday, 29 July 2014 89-LP-8 Centaur Upper Stage at 50 Years: Selected Technical Topics Room 3 Chaired by: C. WILLIAMS, NASA Glenn Research Center and S. BUSHMAN, JHU/Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3669 AIAA-2014-3670 AIAA-2014-3671 AIAA-2014-3672 AIAA-2014-3673 RL10 Engine Ability to Transition Reﬂections on Centaur Upper Stage DUKSUP: A Computer Program ADDJUST-A NASA View of the Early Three Orbital Burns to Molniya from Atlas to Shuttle Centaur Integration by the NASA Lewis for High Thrust Launch Vehicle Years Orbit via Shuttle/Centaur G Upper Program (Glenn) Research Center Trajectory Design & Optimization J. Nieberding, Self, Westlake, OH Stage J. Baumeister, NASA Glenn Research S. Graham, NASA Glenn Research Center, F. Spurlock, Self, Brooklyn, OH; C. C. Williams, NASA Glenn Research Center, Center, Cleveland, OH Cleveland, OH Williams, NASA Glenn Research Center, Cleveland, OH Cleveland, OH Tuesday, 29 July 2014

65 90-LP-9 Combustion Devices I Room 4 Chaired by: W. MARSHALL, NASA-Glenn Research Center and J. SAUER, Orbital Technologies Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3674 AIAA-2014-3675 AIAA-2014-3884 AIAA-2014-3676 AIAA-2014-3677 Chamber Volume Effects on Chemical Reaction Effects on Wall Combustion Characterization New Exact Solution of the Uniﬁed Framework for Modeling Hypergolic Pulse Detonation Rocket Heat Flux in Liquid Rocket Thrust of Amine Borane Hypergolic Bidirectional Vortex in a Conically- Swirl Dominated Helical Motions Engine Chambers Propellants Shaped Cyclonic Chamber J. Majdalani, Auburn University, Auburn, AL B. Kan, S. Heister, Purdue University, West B. Betti, D. Bianchi, F. Nasuti, University J. Willits, J. Dennis, A. Kulkarni, P. T. Barber, J. Majdalani, Auburn University, Lafayette, IN of Rome “La Sapienza”, Rome, Italy; Ramachandran, T. Pourpoint, Purdue Auburn, AL E. Martelli, Second University of Naples, University, West Lafayette, IN Aversa, Italy Tuesday, 29 July 2014 91-LP-10 Combustion Dynamics II Room 5 Chaired by: D. LINEBERRY, UAH Propulsion Research Center and E. JACOB, GTL 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3678 AIAA-2014-3679 AIAA-2014-3680 AIAA-2014-3681 AIAA-2014-3682 Application of Band-Limited White An Analytical Investigation A Computational Study of Combustion Stability Characteristics Transverse Combustion Instabilities: Noise & Single Frequency Acoustic Characterizing the Application Transverse Combustion Instability of the Project Morpheus Liquid Modern Experimental Techniques Modulation as a Control Mechanism of Single Frequency Acoustic Mechanisms Oxygen / Liquid Methane Main and Analysis for Liquid Rocket Engine Modulation for High Frequency K. Shipley, W. Anderson, Purdue University, Engine J. Quinlan, B. Zinn, Georgia Institute of Combustion Instabilities Combustion Instability Suppression West Lafayette, IN; M. Harvazinski, V. J. Melcher, R. Morehead, NASA Johnson Technology, Atlanta, GA J. Bennewitz, J. Cranford, D. Lineberry, J. Cranford, J. Bennewitz, S. Rani, Sankaran, Air Force Research Laboratory, Space Center, Houston, TX R. Frederick, University of Alabama, R. Frederick, University of Alabama, Edwards AFB, CA Huntsville, Huntsville, AL Huntsville, Huntsville, AL Tuesday, 29 July 2014 92-ABPSI-3/GTE-13 Integrated Performance I Room 6 Chaired by: J. TAI, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3683 AIAA-2014-3684 AIAA-2014-3685 AIAA-2014-3686 AIAA-2014-3687 Optimization of an Advanced Open Propulsion System Dynamic Modeling An Assessment of Ultra High A Thrust Drag Bookkeeping Computational Fluid Dynamics Rotor Engine for Civil Transport of the NASA Supersonic Concept Bypass Engine Architecture and Method based on Computational Modeling of a Supersonic Nozzle L. Casalino, D. Pastrone, Technical Vehicle for AeroPropulsoServoElasticity Installation Considerations Fluid Dynamics and Integration into a Variable University of Turin, Turin, Italy G. Kopasakis, J. Connolly, J. Seidel, NASA K. Aloyo, C. Perullo, D. Mavris, Georgia Y. Zhang, H. Chen, Tsinghua University, Cycle Engine Model Glenn Research Center, Cleveland, OH; D. Institute of Technology, Atlanta, GA Beijing, China; M. Zhang, M. Zhang, J. Connolly, D. Friedlander, G. Kopasakis, Christhilf, Lockheed Martin Corporation, Shanghai Aircraft Design and Research NASA Glenn Research Center, Cleveland, Hampton, VA Institute, Shanghai, China; S. Fu, OH Tsinghua University, Beijing, China Tuesday, 29 July 2014 93-SR-3 Solid Rocket Motor Nozzles, Ignition Systems and Propellants Room 7 Chaired by: M. BERDOYES, Herakles and K. NAUMANN, Bayern-Chemie GmbH 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3688 AIAA-2014-3689 AIAA-2014-3690 AIAA-2014-3691 Analysis and Design Optimization Static Aeroelastic Analysis Steam-Plasma Igniter for Temperature Sensitivity of of Three Dimensional Nozzles of Supersonic Nozzles and Aluminum Powder Combustion Composite Propellant Containing S. Eyi, Middle East Technical University, Performance Response S. Lee, J. Lim, K. Noh, W. Yoon, Yonsei Novel Nano-Additive Catalysts Ankara, Turkey U. Duzel, S. Eyi, Middle East Technical University, Seoul, South Korea; D. A. Demko, J. Thomas, T. Sammet, E. University, Ankara, Turkey Lee, Agency for Defense Development, Petersen, Texas A&M University, College Daejeon, South Korea Station, TX; D. Reid, S. Seal, University of

66 Central Florida, Orlando, FL Tuesday, 29 July 2014 94-EP-12 Micro-Propulsion Room 8 Chaired by: L. KING, Michigan Technological University and J. ZIEMER, Jet Propulsion Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3692 AIAA-2014-3693 AIAA-2014-3694 AIAA-2014-3695 Characteristics of a Laser- Wavelength measurements Beam composition of an ionic liquid Direct Thrust Measurements electrostatic Hybrid Propulsion of Rosensweig instabilities in ferrofluid electrospray source for a Multiplexed Borosilicate Thruster a ferrofluid in a non-uniform K. Terhune, L. King, Michigan Technological Electrospray Source A. Osamura, H. Horisawa, T. Sakai, Tokai magnetic field University, Houghton, MI; M. Hause, B. C. Coffman, P. Lozano, Massachusetts University, Kanagawa, Japan E. Meyer, L. King, Michigan Technological Prince, Air Force Research Laboratory, Institute of Technology, Cambridge, MA University, Houghton, MI Kirtland AFB, NM; N. Jain, B. Hawkett, The University of Sydney, Sydney, Australia Tuesday, 29 July 2014 95-EP-13 MPD and Helicon Room 9 Chaired by: O. DUCHEMIN, Snecma S.A. and J. FOSTER, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3696 AIAA-2014-3697 AIAA-2014-3698 AIAA-2014-3699 Numerical Simulation of Plasma Research and Development of Downstream Flow Analysis of High- Design of Helicon Plasma Thruster Flow in a Self-field MPD Thruster Steady-State MPD Thrusters with Power Helicon Double Gun Thruster subsystems Coupled with Electrode Sheath Permanent Magnets and Multi with Application to Spacecraft J. Navarro, Technical University of Madrid, A. Kawasaki, Tokyo Institute of Hollow Cathodes for In-Space Propulsion Systems Madrid, Spain; M. Merino-Martinez, E. Technology, Yokohama, Japan; K. Kubota, Propulsion N. Murakami, B. Roberson, R. Winglee, Ahedo, Charles III University of Madrid, Japan Aerospace Exploration Agency T. Suzuki, H. Tahara, Osaka Institute of I. Johnson, University of Washington, Madrid, Spain; V. Sánchez Martínez, M. (JAXA), Chofu, Japan; I. Funaki, Japan Technology, Osaka, Japan Seattle, Seattle, WA Ruiz Haro, SENER, Tres Cantos, Spain Aerospace Exploration Agency (JAXA), Sagamihara, Japan; Y. Okuno, Tokyo Institute of Technology, Yokohama, Japan Tuesday, 29 July 2014 96-LNCH-2 Luncheon Reception in Exposition Hall Exhibit Hall C 1200 - 1300 hrs Tuesday, 29 July 2014 97-PLENARY-4 High Energy & Power Technologies - The View from Users Grand Ballroom A 1300 - 1430 hrs Government and industry experts will explore the synergies between emerging energy technologies in the aerospace and transportation sectors. The current state of these technologies and evolving trends across different sectors will also be discussed. Moderator: Richard Stulen, Vice President (ret), Sandia National Laboratories

67 Panelists: Gary Smyth, Executive Director, North American Science Labs Global Research and Development, General Motors Company Pierre-Guy Amand, Director Engineering and Economics, SAFRAN Sunita Satyapal, Director, Fuel Cell Technologies Office, Energy Efficiency and Renewable Energy, U.S. Department of Energy Rickey Shyne, Director, Research and Engineering Directorate, NASA Glenn Research Center Tuesday, 29 July 2014 98-NW-5 Networking Break in Exposition Hall Exhibit Hall C 1430 - 1500 hrs Tuesday, 29 July 2014 184-LP-11 LP History: Start and Evolution of Spacecraft Propulsion Room 1 1430 - 1800 hrs Chaired by: T. PUGMIRE, Spincraft; P. WILHELM, US Naval Research Lab and B. AUSTIN, IN Space LLC List of speakers: W. Andrew Hoskins, Aerojet Rocketdyne, In Space Propulsion Evolution, World View Roger M. Myers, Aerojet Rocketdyne, In Space Propulsion Evolution, United States View Peter Wilhelm, Director NRL, Experiment to Flight Lou Ignaziak, NASA Lewis-Glenn, SERT II, As we Lived It Hartwig Ellerbrock, Astrium, In Space Propulsion Developments in Germany T. Kent Pugmire, Spincraft, The Electrothermal Adventure, My View Round Table: Options for Tomorrow, Speakers and Invited Guests Moderator: Peter Wilhelm Tuesday, 29 July 2014 99-ITAR-2 Topics in Liquid Propulsion Room 16 Chaired by: B. WINTERS, Orbital Sciences Corporation and S. FORDE, Aerojet Rocketdyne Corporation 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3700 AIAA-2014-3702 AIAA-2014-3703 AIAA-2014-3704 AIAA-2014-3705 AIAA-2014-3706 Effect of Cooling Channel Shape The Development and Testing of a Design and Development of a Slosh Baffle Design, Test, Characterizing Orbital Maneuvering Development and Testing on the Thermal Characteristics LOX/LCH4 Reaction Control System Hydrogen Peroxide Monopropellant Dampening Analysis, and CFD Subsystem Engine Propellant Vapor Combustion Chamber and of Regeneratively Cooled Rocket Thruster - Please Consider for ITAR Micro Thruster System (consider for Modeling for Spherical Liquid Leakage at Ball Valve Shaft Monolithic Catalyst for 1N AF- Engines Session ITAR Session) Oxygen and Liquid Methane N. Buntain, V. Natewa, NASA White Sands M315E Monopropellant Thruster M. Naraghi, Manhattan College, Riverdale, J. Mena, M. Ingle, J. Chaparro, A. J. Barragan, A. Vazquez, A. Choudhuri, Propellant Tanks for a Lander Test Facility, Las Cruces, NM T. McKechnie, A. Shchetkovskiy, NY; S. Dunn, Sea, Inc., Carson City, NV Choudhuri, University of Texas, El Paso, University of Texas, El Paso, El Paso, TX H. Hernandez, NASA Johnson Space Plasma Processes, LLC, Huntsville, AL; El Paso, TX Center, Houston, TX C. Carpenter, D. Schmuland, J. Overly, Aerojet Rocketdyne, Redmond, WA Tuesday, 29 July 2014 100-EP-14 Vacuum Facility Effects Room 10 Chaired by: A. GALLIMORE, University of Michigan and D. KING, Aerojet 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-3707 AIAA-2014-3708 AIAA-2014-3709 AIAA-2014-3710 AIAA-2014-3711 AIAA-2014-3712 AIAA-2014-3713 Investigation of the Effects of Effect of Background Pressure Backpressure effects on the The Effect of Background Impact of Cathode Position and Preliminary Assessment of the Role Facility Effects on Helicon Plasma Facility Background Pressure on on the Plasma Oscillation operation of Hall thrusters Pressure on SPT-100 Hall Thruster Electrical Facility Effects on Hall of a Conducting Vacuum Chamber Source Operation the Performance and Operation of Characteristics of the HiVHAc Hall R. Hofer, J. Anderson, Jet Propulsion Performance Effect Thruster Performance and in the Hall Effect Thruster Electrical N. Schloeder, J. Frieman, M. Walker, the High Voltage Hall Accelerator Thruster Laboratory, California Institute of K. Diamant, The Aerospace Corporation, Discharge Current Behavior Circuit Georgia Institute of Technology, Atlanta, H. Kamhawi, W. Huang, T. Haag, NASA W. Huang, H. Kamhawi, NASA Glenn Technology, Pasadena, CA El Segundo, CA; R. Liang, R. Corey, Space J. Walker, J. Frieman, M. Walker, Georgia J. Frieman, S. King, M. Walker, Georgia GA Glenn Research Center, Cleveland, OH Research Center, Cleveland, OH; R. Lobbia, Systems/Loral, Palo Alto, CA Institute of Technology, Atlanta, GA; V. Institute of Technology, Atlanta, GA; V.

68 D. Brown, Air Force Research Laboratory, Khayms, Lockheed Martin Corporation, Khayms, Lockheed Martin Corporation, Edwards AFB, CA Sunnyvale, CA Sunnyvale, CA Tuesday, 29 July 2014 101-EP-15 SEP Technology Demonstration Missions Room 11 Chaired by: D. JACOBSON, NASA Glenn Research Center and J. DANKANICH, Aero Dank, Inc. 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-3714 AIAA-2014-3715 AIAA-2014-3716 AIAA-2014-3717 AIAA-2014-3718 AIAA-2014-3719 AIAA-2014-3720 Comparison of Low-Thrust An Integrated Approach to Solar Electric Propulsion Concept designs for NASA’s Solar Solar Electric Propulsion’s A High Power Solar Electric Evaluation of Electric Propulsion Control Laws for Applications in Modeling Solar Electric Propulsion Demonstration Mission Using a Electric Propulsion Technology Applicability to Future NASA Propulsion - Chemical Mission for Systems for Asteroid and Comet Planetocentric Space Vehicles During Long Duration, Minotaur IV Launch Vehicle Demonstration Mission Missions Human Exploration of Mars Sample-Return Missions R. Falck, W. Sjauw, NASA Glenn Research Near-Earth Orbit Transfers W. Deininger, S. Enger, J. Hackel, J. Soto, M. McGuire, K. Hack, D. Manzella, D. D. Manzella, K. Hack, NASA Glenn L. Burke, NASA Glenn Research K. Sankaran, A. French, S. Gady, A. Center, Cleveland, OH; D. Smith, Vantage D. Smith, Vantage Partners, LLC, B. Unruh, Ball Aerospace & Technologies Herman, NASA Glenn Research Center, Research Center, Cleveland, OH Center, Cleveland, OH; M. Martini, ZIN Sehgal, Whitworth University, Spokane, Partners, LLC, Brook Park, OH Cleveland, OH; W. Sjauw, J. Hojnicki, Corporation, Boulder, CO; D. Murphy, ATK, Cleveland, OH Technologies, Inc., Cleveland, OH; S. WA NASA Glenn Research Center, Cleveland, Goleta, CA; et al. Oleson, NASA Glenn Research Center, OH Cleveland, OH Tuesday, 29 July 2014 102-NFF-4 Nuclear Thermal Propulsion III - Fuels Development and Engine Testing Room 12 Chaired by: J. WARREN, NASA Headquarters and A. BELVIN 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation AIAA-2014-3723 AIAA-2014-3724 AIAA-2014-3725 Fuel Development Efforts for Graphite-Based Composite Fuel Process Development & Fabrication Hot Hydrogen Testing of Tungsten- Initial Operation and Shakedown The Nuclear Cryogenic Propulsion Numerical Simulation of Thermal- Nuclear Thermal Propulsion Within Development for Nuclear Thermal of Tungsten-Uranium Dioxide Uranium Dioxide (W-UO2) CERMET of the Nuclear Thermal Rocket Stage Hydrodynamic Transients in the the Department of Energy Propulsion (W-UO2) CERMET Fuel Elements for Fuel Materials for Nuclear Thermal Element Environmental Simulator M. Houts, T. Kim, W. Emrich, R. Hickman, Cooling Channels of a Nuclear A. Qualls, B. Schnitzler, Oak Ridge B. Jolly, M. Trammell, J. Miller, A. Qualls, Nuclear Thermal Propulsion Propulsion (NTREES) J. Broadway, H. Gerrish, NASA Marshall Thermal Propulsion Engine National Laboratory, Oak Ridge, TN; J. Oak Ridge National Laboratory, Oak J. Broadway, R. Hickman, O. Mireles, D. R. Hickman, J. Broadway, NASA Marshall W. Emrich, NASA Marshall Space Flight Space Flight Center, Huntsville, AL; et al. K. Akyuzlu, University of New Orleans, Werner, Idaho National Laboratory, Idaho Ridge, TN Tucker, NASA Marshall Space Flight Center, Space Flight Center, Huntsville, AL Center, Huntsville, AL New Orleans, LA; D. Coote, NASA Stennis Falls, ID; D. Poston, Los Alamos National Huntsville, AL Space Center, Stennis Space Center, MS Laboratory, Los Alamos, NM; A. Weitzberg, Self, Woodland Hills, CA; A. Belvin, Department of Energy, Washington, DC Tuesday, 29 July 2014 103-GTE-14/PC-7 Wave Rotors and Pulse Combustors for Gas Turbine Engines Room 13 Chaired by: M. NALIM, CNRS & Université Paris-Sud and D. FERGUSON, National Energy Technology Laboratory 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3726 AIAA-2014-3727 AIAA-2014-3728 AIAA-2014-3729 AIAA-2014-3730 Thermodynamic Behavior of a Simulation of Hot-Jet Ignition Effect of Fuel Injection and Mixing Numerical analysis of unsteady Experimentally modified unsteady Gas Turbine Engine With Variable- in a Heated Constant-Volume Characteristics on Pulse-Combustor effects in partial admittance shock wave model for wave rotor Pressure Combustion Combustor Using Adadptive Performance at High-Pressure turbine cooperating with pulse design R. Andriani, Technical University of Milan, Mesh Refinement and Multi-Zone S. Yungster, Ohio Aerospace Institute, combustion chambers S. Chan, H. Liu, Beihang University, 69 Milan, Italy; A. Ingenito, F. Gamma, Reaction Cleveland, OH; D. Paxson, H. Perkins, R. Cerpa, University of San Buenaventura, Beijing, China A. Agresta, University of Rome “La M. Rajagopal, M. Nalim, M. Khan, Indiana NASA Glenn Research Center, Cleveland, Bogota, Colombia; J. Piechna, Warsaw Sapienza’’, Rome, Italy University-Purdue University Indianapolis, OH University of Technology, Warsaw, Poland; Indianapolis, IN N. Mueller, Michigan State University, East Lansing, MI Tuesday, 29 July 2014 104-GTE-15/ABPSI-4 Inlet Engine Compatibility and Aeroelasticity Room 14 Chaired by: G. WELCH, NASA Glenn Research Center and G. HERRICK, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3731 AIAA-2014-3732 AIAA-2014-3733 AIAA-2014-3734 AIAA-2014-3735 Numerical Simulation of Boundary Effects of Complicated Rotating Assessing Fan Flutter Stability in Forced Response Analysis of a Experimental Investigation of a Layer Ingesting (BLI) Inlet/Fan Inlet distortion on Compressor Presence of Inlet Distortion Using Fan with Boundary Layer Inlet Forced Response Condition in a Interaction Aerodynamic Stability One-way and Two-way Coupled Distortion Multistage Compressor J. Giuliani, J. Chen, Ohio State University, W. Yan, J. Hu, H. Zhang, Z. Mao, C. Methods M. Bakhle, NASA Glenn Research Center, W. Murray, N. Key, Purdue University, Columbus, OH; T. Beach, Coyote Hollow Yin, Z. Chenkai, Nanjing University of G. Herrick, NASA Glenn Research Center, Cleveland, OH West Lafayette, IN Consulting LLC, Walton Hills, OH; M. Aeronautics and Astronautics, Nanjing, Cleveland, OH Bakhle, NASA Glenn Research Center, China Cleveland, OH Tuesday, 29 July 2014 105-GTE-16/ABPSI-5 Jet Noise Room 15 Chaired by: B. HENDERSON, NASA Glenn Research Center and B. KIEL, Air Force Reseach Laboratory 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-3736 AIAA-2014-3737 AIAA-2014-3738 AIAA-2014-3739 AIAA-2014-3740 AIAA-2014-3741 AIAA-2014-3742 Subsonic Round and Rectangular Prediction, Experiments and Characterization of Supersonic Jet A Design of Experiments Efficient Supersonic Jet Noise Flow Field and Acoustic Predictions Fourth-order Spectral Statistics in Twin Jet Flow Effects Optimization of High-Speed Jet Noise Production and Methods for Investigation of Offset Streams for Simulations Using JENRE for Three-Stream Jets the Developing Shear Layers of Hot R. Bozak, M. Wernet, NASA Glenn Noise Reduction Using Fluidic its Suppression Supersonic Jet Noise Reduction K. Kailasanath, A. Corrigan, J. Liu, R. S. Simmons, Vantage Partners, LLC, Supersonic Jets Research Center, Cleveland, OH Inserts E. Gutmark, D. Cuppoletti, P. Mora B. Henderson, NASA Glenn Research Ramamurti, Naval Research Laboratory, Brook Park, OH; B. Henderson, NASA T. Ecker, K. Lowe, W. Ng, Virginia P. Morris, D. McLaughlin, R. Powers, M. Sanchez, N. Heeb, University of Cincinnati, Center, Cleveland, OH; D. Papamoschou, Washington, DC Glenn Research Center, Brook Park, OH; Polytechnic Institute and State University, Kapusta, Pennsylvania State University, Cincinnati, OH University of California, Irvine, Irvine, CA A. Khavaran, ASRC Aerospace Corporation, Blacksburg, VA University Park, PA Brook Park, OH Tuesday, 29 July 2014 106-HSABP-5 Numerical Investigations in High-Speed Propulsion Room 2 Chaired by: E. AXDAHL, NASA Langley Research Center and R. STARKEY, University of Colorado Boulder 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-3743 AIAA-2014-3744 AIAA-2014-3745 AIAA-2014-3746 AIAA-2014-3747 AIAA-2014-3748 AIAA-2014-3749 A Priori Analysis of Flamelet-based High Resolution Numerical Study High Resolution Numerical Study Effects of Fuel-lean Primary Rocket Effect of fuel injection with mixer Supersonic combustion of liquid Numerical Simulation of a Dual- Modeling for a Dual-Mode Scramjet on the Supersonic Turbulent Flame on the Coaxial Supersonic Turbulent on Bypass Ratio in RBCC Ejector in TBCC Hyperburner n-decane in a dual-cavity based Mode Scramjet Combustor Using Combustor Structures and Dynamics in Dual Flame Structures Mode Y. Fan, C. Xiaojun, C. Di, Nanjing scramjet Flamelet Scheme J. Quinlan, J. McDaniel, University of Combustion Ramjet J. Choi, Pusan National University, Busan, B. Lin, H. Pan, F. Qin, Northwestern University of Aeronautics and Astronautics, Z. Yan, L. Yuzhen, L. Wei, W. Jianchen, Z. Z. Yan, L. Yuzhen, L. Wei, W. Jianchen, Z. Virginia, Charlottesville, Charlottesville, J. Choi, Pusan National University, Busan, South Korea; K. Kim, Seoul National Polytechnical University, Xi’an, China Nanjing, China Yongsheng, Beihang University, Beijing, Yongsheng, Beihang University, Beijing, VA; T. Drozda, NASA Langley Research South Korea; V. Yang, Georgia Institute of University, Seoul, South Korea; S. Han, China China Center, Hampton, VA; G. Lacaze, J. Technology, Atlanta, GA Korea Aerospace Research Institute,

70 Oefelein, Sandia National Laboratories, Daejeon, South Korea Livermore, CA Tuesday, 29 July 2014 107-HR-4 Regression Rate Studies in Hybrid Rockets Room 20 Chaired by: J. DAVITIAN, The Aerospace Corporation and B. EVANS, Stanford University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3750 AIAA-2014-3751 AIAA-2014-3752 AIAA-2014-3753 AIAA-2014-3754 Regression Rate Estimation for High Regression Rate Hybrid Pyrolysis of Acrylonitrile- Hybrid rocket fuel residuals - an Testing of Hybrid Rocket Fuel Swirling-Flow Hybrid Rocket Rocket Fuel Grains with Helical Port Butadiene-Styrene (ABS) Under overlooked topic Grains at Elevated Temperatures Engines Structures High Heat Flux Conditions F. Barato, University of Padua, Padua, with Swirl Patterns Fabricated Using P. Wongyai, D. Greatrix, Ryerson S. Whitmore, M. Sobbi, S. Walker, Utah J. Wilson, S. Whitmore, Utah State Italy; M. Grosse, Energetix, Bonn, Rapid Prototyping Technology University, Toronto, Canada State University, Logan, UT University, Logan, UT Germany; A. Bettella, University of Padua, D. Armold, J. Boyer, B. McKnight, K. Padua, Italy Kuo, Pennsylvania State University, University Park, PA; J. Desain, B. Brady, The Aerospace Corporation, El Segundo, CA; et al. Tuesday, 29 July 2014 108-APC-2 Advanced Vehicle Propulsion Concepts Room 21 Chaired by: J. ROBINSON, Retired f/Boeing 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3755 AIAA-2014-3756 AIAA-2014-3757 AIAA-2014-3758 AIAA-2014-3759 A Cubesat Asteroid Mission: Conceptual Design and Testing Plasmonic Force Propulsion for Assessment of Multi-Mode Cold Gas Propulsion System Propulsion Trade-offs of a Dual-thrust Dual-head Small Spacecraft Spacecraft Micropropulsion Systems Conceptual Design for the SAMSON G. Landis, S. Oleson, M. McGuire, L. Electromagnetic Space Exploration J. Rovey, X. Yang, P. Friz, C. Hu, M. S. Berg, J. Rovey, Missouri University of NanoSatellite Burke, M. Martini, J. Fittje, NASA Glenn Probe Glascock, Missouri University of Science Science and Technology, Rolla, MO J. Herscovitz, D. Lev, Z. Zuckerman, Research Center, Cleveland, OH; et al. J. John, V. Vk, V. Sanal Kumar, and Technology, Rolla, MO Rafael, Haifa, Israel Kumaraguru College of Technology, Coimbatore, India Tuesday, 29 July 2014 109-EPOL-1/ESYS-1 EPOL and ESYS Room 22 Chaired by: M. PISZCZOR, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3760 AIAA-2014-3761 AIAA-2014-3762 AIAA-2014-3763 AIAA-2014-3764 AIAA-2014-3765 On the Modeling of Flow regimes in In-Situ Resource Utilization for Milestone Challenges in Developing Numerical Simulation of Carbon Dioxide Emission Free Goal Based Testing: A Risk Heavy Truck Passengers Cabins Space Exploration: Resource Innovation and Commercialization Biologically Propelling Beetle Wings Power Generation System Informed Process A. Omran, E. Khalil, Cairo University, Processing, Mission-Enabling of Rocket Propulsion Technologies at Various Flying Conditions H. Sameshima, K. Takahashi, T. Sasaki, C. Everline, Jet Propulsion Laboratory, Cairo, Egypt Technologies, and Lessons for R. Freeman, Northcentral University, V. Sanal Kumar, Kumaraguru College of T. Kikuchi, N. Harada, Nagaoka University California Institute of Technology, Sustainability on Earth and Beyond Prescott Valley, AZ Technology, Coimbatore, India of Technology, Nagaoka, Japan; S. Pasadena, CA; N. Goldin, NASA Glenn A. Hepp, B. Palaszewski, A. Colozza, G. Takeshita, Wakayama National College of Research Center, Cleveland, OH; S. Landis, D. Jaworske, M. Kulis, NASA Glenn Technology, Gobo, Japan Di Stefano, Jet Propulsion Laboratory, 71 Research Center, Cleveland, OH California Institute of Technology, Pasadena, CA; C. Smith, Johns Hopkins University Applied Physics Laboratory, Laurel, MD Tuesday, 29 July 2014 110-TM-3 Spacecraft and Lunar/Mars/Venus Surface Thermal Management Room 23 Chaired by: M. CHOI, NASA-Goddard Space Flight Center and C. TARAU, Advanced Cooling Technologies 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3766 AIAA-2014-3767 AIAA-2014-4030 AIAA-2014-3769 AIAA-2014-3770 AIAA-2014-3768 Low Cost Radiator for Fission Power Method of Minimizing Size of On The Modeling Of Film Cooling In Development of Heat Pipes Thermal Model Predictions of On the Computations of Thermal Thermal Control Heat Rejection Systems for Turbine Blades Under Elevated Gas Operating at Mid-Level Advanced Stirling Radioisotope Behaviour of Shell and Tube Heat T. Maxwell, J. Hartenstine, C. Tarau, W. Thermoelectric Coolers to Cool Temperatures Temperature Range Applied for Generator Performance Exchanger Anderson, Advanced Cooling Technologies, Detectors in Space I. Hassan, G. ElHarriry, E. Khalil, Cairo Industry, Defense and Aerospace X. Wang, W. Fabanich, NASA Glenn E. Khalil, Cairo University, Cairo, Egypt; Inc., Lancaster, PA; N. Walmsley, T. Stern, M. Choi, NASA Glenn Research Center, University, Cairo, Egypt R. Riehl, D. Silva, National Institute for Research Center, Cleveland, OH; P. O. AbdelLatif, A. Attia, M. Yehia, Benha Vanguard Space Technologies, Inc., San Cleveland, OH Space Research (INPE), São José dos Schmitz, Power Computing Solutions, Inc., University, Cairo, Egypt Diego, CA; et al. Campos, Brazil Cleveland, OH Tuesday, 29 July 2014 111-ABPSI-7 Integrated Performance II Room 25 A Chaired by: C. CHUCK, Boeing Commercial Airplanes and R. SCHARNHORST, Boeing Defense, Space & Security 1430 hrs 1500 hrs AIAA-2014-3771 AIAA-2014-3772 Performance Estimation for Fluidic Phenomenological Introduction of Thrust Vectoring Nozzle Coupled Propulsion Aspect of External Flow With Aero-engine Choking at Wing in Ground Effect J. Shi, Northwestern Polytechnical V. Sanal Kumar, Kumaraguru College of University, Xi’an, China Technology, Coimbatore, India Tuesday, 29 July 2014 112-PC-8 Combustion Dynamics and Detonations Room 25 B Chaired by: E. LYNCH, Aerojet Rocketdyne 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3773 AIAA-2014-3774 AIAA-2014-3775 AIAA-2014-3776 AIAA-2014-3778 AIAA-2014-3779 High Frequency Signal Analysis Stability Characterization of a High Development of Validation Thermoacoustic Feedback Analysis Effect of the Acoustic Excitation An Acoustically Consistent Methods for Acoustic Modal Pressure Transverse Combustor Approaches for Numerical of a Cylindrical Combustion on Lean Blowoff in Turbulent Investigation of Combustion Onset in a Continuously Varying with Discretely Variable Oxidizer Simulation of Combustion Chamber under Supercritical Premixed Bluff Body Flames Instabilities in a Dump Combustor Resonance Combustor Post Lengths Instability using Flame Imaging Conditions C. Jeong, J. Shin, Y. Yoon, Seoul National V. Rani, S. Rani, University of Alabama, S. Hester, W. Anderson, M. Zoltowski, M. Wierman, W. Hallum, W. Anderson, J. Hardi, German Aerospace Center (DLR), M. Schulze, Technical University of University, Seoul, South Korea Huntsville, Huntsville, AL T. Feldman, Purdue University, West Purdue University, West Lafayette, IN Hardthausen, Germany; W. Hallum, C. Munich, Garching, Germany; A. Urbano, Lafayette, IN Huang, W. Anderson, Purdue University, University of Rome “La Sapienza”, Rome, West Lafayette, IN Italy; M. Zahn, M. Schmid, T. Sattelmayer, Technical University of Munich, Garching, Germany; M. Oschwald, German Aerospace Center (DLR), Lampoldshausen, Germany Tuesday, 29 July 2014 113-HSABP-4 High-Speed Airbreathing Propulsion II Room 26 C Chaired by: P. BARTOLOTTA, NASA Glenn Research Center 1430 hrs 1500 hrs AIAA-2014-3780 AIAA-2014-3781 Effect of Second-stage The possibilities of integrated Conﬁguration on Combustion propulsion system

72 in a Dual-struts Based Staged A. Olah, Self, Budapest, Hungary Supersonic Combustor L. Tian, Z. Shaohua, Beihang University, Beijing, China; Z. Qin, China Aerospace Science and Industry Corporation (CASIC), Beijing, China; L. Xuan, X. Xu, Beihang University, Beijing, China Tuesday, 29 July 2014 114-LP-12 Propellant Feed Systems & Fluid Management Technology Room 3 Chaired by: D. RANSOM, Southwest Research Institute and B. MARCU, SpaceX 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3782 AIAA-2014-3783 AIAA-2014-3784 AIAA-2014-3785 AIAA-2014-3786 Low Cost Turbopump Concept for LAPLACE - Inducer Cryogenic Development of a Pistonless Rocket Surge Pressure Mitigation in the Experiments on fluid hammer Wide Throttle Range Applications Cavitation Test Rig : a Key-Stone in Engine Pump Suborbital Flight Test Global Precipitation Measurement involving cavitation and pressurant S. Sargent, J. Preuss, R. Pulling, Barber- the Long-Term Cavitation Research Demonstrator Mission Core Propulsion System gas desorption for aerospace Nichols, Inc., Arvada, CO Program R. Starkey, M. Cannella, J. Brendel, A. Scroggins, M. Fiebig, NASA Goddard applications T. Watiotienne, J. NGuyen Duc, P. University of Colorado, Boulder, Boulder, Space Flight Center, Greenbelt, MD M. Lema, von Kármán Institute for Manfredi, P. Nivet, Safran Group, Snecma, CO; S. Harrington, Flometrics, Inc., Fluid Dynamics, Rhode-Saint-Genése, Vernon, France; J. Dehouve, J. Herpe, Carlsbad, CA Belgium; J. Steelant, ESA, Noordwijk, The French Space Agency (CNES), Paris, Netherlands; F. López Peña, University of France A Coruña, A Coruña, Spain; P. Rambaud, von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genése, Belgium Tuesday, 29 July 2014 115-LP-13 Injectors II Room 4 Chaired by: O. HAIDN, Technische Universität München and S. MILLER, Aerojet Rocketdyne Corporation 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3787 AIAA-2014-3788 AIAA-2014-3789 AIAA-2014-3790 AIAA-2014-3791 Effect of Injector Exit Geometry An Experimental Study of the Numerical and Experimental Interpretation of Core Length in Application of a Real-Gas-Library on Atomization of a Liquid-Liquid Effects of Plate Geometry on the Investigation of Confined Turbulent Shear Coaxial Rocket Injectors from Multi-Fluid-Mixing Model to Double Swirl Coaxial Injector using Spray Atomization of LOX/CH4 in Multiple Transverse Jets X-ray Radiography Measurements Supercritical Single Injector Flow Non-Invasive Laser, Optical and Uni-Element Shear Coaxial Injectors F. Davoudzadeh, Air Force Research S. Schumaker, S. Danczyk, M. Lightfoot, D. Banuti, K. Hannemann, German X-ray Techniques L. Sanchez, V. Dorado, R. Ellis, R. Laboratory, Edwards AFB, CA; D. Forliti, Air Force Research Laboratory, Edwards Aerospace Center (DLR), Göttingen, C. Radke, NASA Johnson Space Center, Woodward, A. Choudhuri, University of Sierra Lobo, Inc., Edwards AFB, CA AFB, CA; A. Kastengren, Argonne National Germany Houston, TX; T. Meyer, T. Heindel, Iowa Texas, El Paso, El Paso, TX Laboratory, Argonne, IL State University, Ames, IA Tuesday, 29 July 2014 116-LP-14 Spacecraft Propulsion Systems II Room 5 Chaired by: P. ALLIOT, Snecma S.A. and K. KREINER, Boeing Defense, Space & Security 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3792 AIAA-2014-3793 AIAA-2014-3794 AIAA-2014-3795 AIAA-2014-3796 AIAA-2014-3797 Ignition Overpressure in Laser Development of Dual Propulsion Overview of the German Gel Life Test Results of a MONARC 5 1 Gelled Green Propellant Rocket Control Characteristics of a Gel Ignited Reaction and Control System with Mono-/Bi-propellants Propulsion Technology Program lbf Monopropellant Thruster with Motor and Gas Generator Propellant Throtteable Rocket Thrusters Specialized for Microsatellites H. Ciezki, German Aerospace Center Heraeus Catalyst Technology at Bayern-Chemie - Motor with a Pintle Nozzle C. Manfletti, German Aerospace Center T. Oohira, T. Sakuma, S. Nishikizawa, H. (DLR), Hardthausen, Germany; J. Hürttlen, C. Gatto, B. Nakazono, Jet Propulsion Status and Applications for Space P. Pinto, J. Ramsel, H. Niedermaier, A. (DLR), Hardthausen, Germany Sahara, Tokyo Metropolitan University, Fraunhofer, Pfinztal-Berghausen, Germany; Laboratory, California Institute of Systems Thumann, K. Naumann, Bayern-Chemie, Tokyo, Japan K. Naumann, Bayern-Chemie, Aschau Technology, Pasadena, CA K. Naumann, J. Ramsel, P. Pinto, H. Aschau am Inn, Germany

73 am Inn, Germany; M. Negri, German Niedermaier, A. Thumann, Bayern-Chemie, Aerospace Center (DLR), Hardthausen, Aschau am Inn, Germany Germany; J. Ramsel, Bayern-Chemie, Aschau am Inn, Germany; V. Weiser, Fraunhofer, Pfinztal-Berghausen, Germany Tuesday, 29 July 2014 117-ABPSI-6 Inlets II Room 6 Chaired by: L. LEAVITT, NASA and K. BLODGETT, GE Aviation 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3798 AIAA-2014-3799 AIAA-2014-3801 AIAA-2014-3802 Low Drag Design and Aerodynamic The Origin of Inlet Buzz in a Mach Grid Resolution Study over Performance of a Supersonic Over- Performance Evaluation of 1.7 Low Boom Inlet Design Operability Space for a Mach 1.7 Wing Inlet with Application to a Supersonic Air Inlet B. Anderson, NASA Glenn Research Center, Low Boom External Compression Low-Sonic-Boom Aircraft H. Miki, M. Kameda, Tokyo University Cleveland, OH Inlet C. Trefny, S. Hirt, B. Anderson, NASA of Agriculture and Technology, Koganei, B. Anderson, NASA Glenn Research Center, Glenn Research Center, Cleveland, OH; L. Japan; Y. Watanabe, Japan Aerospace Cleveland, OH Fink, The Boeing Company, Seattle, WA; T. Exploration Agency (JAXA), Mitaka, Japan Magee, The Boeing Company, Huntington Beach, CA Tuesday, 29 July 2014 118-SR-4 Solid Rocket Motor Modeling, Simulation and Analysis I Room 7 Chaired by: J. SPURLING, Naval Air Warfare Center Weapons Division and J. MAJDALANI, Auburn University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3803 AIAA-2014-3804 AIAA-2014-3805 AIAA-2014-3806 AIAA-2014-3807 Modeling Cracks in Nonlinear Improvements to the Solid Analysis and Performance A Monte Carlo Analysis of the 3D Flow Simulation of Dual Thrust Viscoelastic Media Subjected to Performance Program (SPP’12) Reconstruction of VEGA Solid Thrust Imbalance for the Space Solid Rocket Motors during Starting Thermal Loading and a Review of Nozzle Rocket Motors Qualification Flights Launch System Booster During Both Transient S. Özüpek, C. Iyidiker, Bogazici University, Performance Predictions E. Cavallini, B. Favini, University of Rome the Ignition Transient and Steady V. Sanal Kumar, J. John, Kumaraguru Istanbul, Turkey D. Coats, A. Dang, Software and “La Sapienza”, Rome, Italy; A. Neri, ESA, State Operation College of Technology, Coimbatore, India Engineering Associates, Inc., Carson Frascati, Italy T. Steadman, NASA Marshall Space Flight City, NV Center, Huntsville, AL; W. Foster, W. Crowder, Auburn University, Auburn, AL Tuesday, 29 July 2014 119-ECS-1 Energetic Component Modeling, Porous Explosives and Composites, Technical Roadmaps and Margin Assessments in Testing Room 8 Chaired by: B. SMITH, Pacific Scientific Energetic Materials Company 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3808 AIAA-2014-3809 AIAA-2014-3810 AIAA-2014-3811 AIAA-2014-3812 AIAA-2014-3813 Underwater Performance Sizing of an Explosive Bolt using an Microstructure Dependent Reactive 2014 CAD/PAD Technology Margin Requirements and Input Rapid Design and Optimization of a Characterization of a Ballistic Elastic Plastic-Strength Model Burn Modeling of Porous Solid Roadmap Update Report Level Formulation in Dynamic Composite Retainer to Support the Guillotine Cutter at Operating J. Kozmic, H. Lee, Chemring Energetic Explosives T. Blachowski, J. Burchett, Naval Surface Testing of ECS Energetic Loading of an Expanding Temperature Extremes Devices, Downers Grove, IL P. Rao, K. Gonthier, Louisiana State Warfare Center, Indian Head, MD; J. L. Yang, Self, La Canada Flintridge, CA Tube Assembly H. Lee, Chemring Energetic Devices, University, Baton Rouge, LA Baglini, Exodynamics Technology, Inc., R. Davis, Pacific Scientific Energetic Downers Grove, IL Phoenix, AZ; C. Wheeler, A. Woods, Naval Materials Company, Hollister, CA

74 Surface Warfare Center, Indian Head, MD Tuesday, 29 July 2014 120-EP-16 Hall Thruster Room 9 Chaired by: R. HOFER, Jet Propulsion Laboratory and P. PETERSON, ElectroDynamic Applications, Inc. (EDA) 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-4031 AIAA-2014-3814 AIAA-2014-3815 AIAA-2014-4032 AIAA-2014-3816 AIAA-2014-3817 AIAA-2014-3818 Effects of Wall Temperature and Performance Characteristics of The X3 100-kW Class Nested- Establishing an In Situ Technique Throttled Performance of the SPT- Investigation of the Effects Performance Comparison between Surface Roughness on the Plasma High-Power, High-Speciﬁc-Impulse Channel Hall Thruster: Motivation, for Measuring Boron Nitride 140 Hall Thruster of Cathode Position on the a Magnesium- and Xenon-fueled 2 Sheath Hall Thrusters for In-Space Implementation, and Initial Testing Erosion J. Snyder, R. Hofer, Jet Propulsion Performance and Operation of the kW Hall Thruster S. Langendorf, M. Walker, Georgia Propulsion S. Hall, R. Florenz, A. Gallimore, University K. Lemmer, A. Hine, G. Neff, Western Laboratory, California Institute of High Voltage Hall Accelerator M. Hopkins, L. King, Michigan Institute of Technology, Atlanta, GA T. Kagota, H. Tahara, Osaka Institute of of Michigan, Ann Arbor, Ann Arbor, MI; H. Michigan University, Kalamazoo, MI Technology, Pasadena, CA H. Kamhawi, W. Huang, T. Haag, NASA Technological University, Houghton, MI Technology, Osaka, Japan Kamhawi, NASA Glenn Research Center, Glenn Research Center, Cleveland, OH Cleveland, OH; D. Brown, Air Force Research Laboratory, Edwards AFB, CA; J. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; et al. Tuesday, 29 July 2014 121-ET-4 Energy Life Cycle Vulnerability and Life Cycle Management Room 24 1500 - 1800 hrs Panel 1: Managing the Life-Cycle of Complex Systems: Using Advanced Models for Energy Decision Support Of the many challenges confronting system developers in the modern era, perhaps none is more challenging than Life-Cycle management of the “System of Systems” contained within the Energy Sector. At the same time, the reliable delivery of energy continues to be a vital function on which all modern economies depend. This session will examine the availability of sophisticated industry offerings in simulation tools and methods that provide effective life-cycle management / decision support for complex systems designers, such as the energy systems of today.. Panelists will provide a general overview and focus on the signiﬁcant advances made in the areas of Applied Model-based SE methods in dealing with the complex systems challenges. Examples of energy system models will be discussed. Moderator: David Long, Vitech Corp/ INCOSE Panelists: Matthew Hause, Atego / PTC Phil LePlante, Penn State University Benjie Loop, PC Krause & Associates, Inc *Sean McGervey, Johns Hopkins University/ APL Panel 2: Examining Energy System Risks and Power Grid Vulnerability The Energy Infrastructure in many countries is aging and vulnerable to a variety of threats, both man-made and natural phenomena. The risks of wide-spread, sustained outage of electricity on modern society could be more devastating than anything that has been experienced in human civilization. This panel will examine the risks and discuss an assessment of various threat scenarios and the current state of power grid challenges for maintaining security and availability. It will also explore possible recovery strategies in the event of grid failure and an action plan for national leadership. Moderator: Frank Gaffney, Center for Security Policy Panelists: Larry Bugh, Reliabiity First Corp. James Stevens, Software Engr Insitute/CMU *Thom Pearce, PUCO *Tom Popik, Foundation for Resilient Societies

75 Tuesday, 29 July 2014 122-PANEL-4 Implementation, Utilization, and Coordination of Advanced Energy Concepts within the Government and Department of Defense Room 26 A 1500 - 1800 hrs Given the reliance of the modern warfighter on advanced technology, the need for lightweight, highly efficient power sources is greater than ever for the military. Advanced battery technology, photovoltaics, advanced fuels, etc. have taken on ever increasing roles within the Department of Defense. This reliance on efficient, low-cost power systems has increased the need for coordination and collaboration on advanced technology between the DoD and other Government agencies. Topics discussed will be include research in advanced power generation technology, system requirements, planned implementation, and coordination activities for these advanced technologies. Moderator: Michael F. Piszczor, Jr., Chief, Photovoltaic and Electrochemical Systems Branch, NASA Glenn Research Center Panelists: Dr. Phillip Jenkins, Senior Technologist, Naval Research Laboratory John Nairus, Chief Engineer Power and Controls Division, Air Force Research Lab, Randall Furnas, Chief, Power Division, NASA Glenn Research Center Evan O. Jones, Manager Energy and Environment for Naitonal Security, Pacific Northwest National Laboratory Tuesday, 29 July 2014 123-PANEL-9 70 Years of Aero Propulsion Research at NASA Glenn Research Center Room 26 B 1500 - 1800 hrs A historical perspective on aero propulsion research conducted at NASA Glenn Research Center over the past 70 years will be presented, with emphasis on research related to engine noise, combustion, CFD, controls, materials and structures, and sensors and instrumentation. Moderator: Dhanireddy Reddy, NASA Glenn Research Center Presenters: Dennis Huff, NASA Glenn Research Center Clarence Chang, NASA Glenn Research Center Louis Povinelli, NASA Glenn Research Center Sanjay Garg, NASA Glenn Research Center Ajay Misra, NASA Glenn Research Center Larry Matus, NASA Glenn Research Center Tuesday, 29 July 2014 124-PLENARY-5 History of the Skunk Works© Grand Ballroom A 1800 - 1900 hrs Alton Romig, Vice President, Engineering and Advanced Systems, Lockheed Martin Aeronautics Known for their ability to rapidly solve even the most daunting challenges, employees of the Skunk Works have supported the missions of their customers for more than 70 years. That singular focus has led to some of the most significant achievements in aerospace to include the first Mach 2 fighter, the highest-flying single engine aircraft, the first (and only) operational Mach 3 aircraft, the first stealth aircraft, and the first operational Mach 3 stealthy unmanned aircraft. The contribution of these Lockheed Martin Skunk Works’ projects to peace, stability and prosperity for the United States and its allies is one reason why it is the only aerospace company in history to receive the National Medal of Technology and Innovation. Join Alton Romig for a discussion of the Skunk Works approach and how it enables the men and women who work there to continue to redefine what is possible. Join us learn and about the exciting history of Lockheed Martin Skunk Works! Tuesday, 29 July 2014 125-PANEL-14 Rising Leaders in Aerospace: “Brand Yourself” Room 5 1900 - 2100 hrs Engineers need to think of themselves not just as an individual, but as a brand. Today, an engineer’s brand is both virtual and in person. Come to the Rising Leaders event “Brand Yourself “ where branding specialist Brad Owen of Creavos will talk about how to manage your brand. Tuesday, 29 July 2014 126-NFF-5 Future Flight Propulsion Systems Room 6 Chaired by: G. MEHOLIC, The Aerospace Corporation and B. PALASZEWSKI, NASA Glenn Research Center 1900 hrs 1930 hrs 2000 hrs AIAA-2014-3819 AIAA-2014-3820 AIAA-2014-3821 Atmospheric Mining in the Outer Mars Aerial Nuclear Global Landing Theory of a Mach Effect Thruster Solar System: Aerial Vehicle Explorer: A Global Mobility and H. Fearn, J. Woodward, K. Wanser, California State University, Fullerton, CA

76 Reconnaissance and Exploration Multi-Mission Platform Options G. Zha, K. Haefner, B. Hayton, University B. Palaszewski, NASA Glenn Research of Miami, Coral Galbes, FL; M. Ding, Center, Cleveland, OH Harbin Engineering Institute, Harbin, China Wednesday Wednesday, 30 July 2014 127-PLENARY-6 Advanced Manufacturing Solutions for P&E Systems - The Art of the Possible Grand Ballroom A 0800 - 0900 hrs Greg Morris, Additive Strategy and Business Development Manager, GE Aviation A leading expert from the additive manufacturing community will share his thoughts on how new manufacturing techniques and technologies are revolutionizing the design and production of propulsion and energy systems. Wednesday, 30 July 2014 185-NW-6 Networking Coffee and Pastries in Exposition Hall Exhibit Hall C 0900 - 0930 hrs Wednesday, 30 July 2014 186-SB-3 Speaker Brieﬁng Session Rooms 0900 - 0930 hrs Please meet your session chairs at 0900 hrs in your session room to load presentations for both the morning and afternoon sessions Wednesday, 30 July 2014 128-ITAR-3 Topics In Energy and Power Management Room 16 Chaired by: M. PISZCZOR, NASA Glenn Research Center and M. CHOI, NASA-Goddard Space Flight Center 0930 hrs AIAA-2014-3822 Design, Optimization, and Experimental Testing of the SLS Avionics Box Thermal Link T. Laker, M. Mecham, ATK, Promontory, UT Wednesday, 30 July 2014 129-ITAR-4 Topics In Turbine Technology and Air Breathing Propulsion Room 16 Chaired by: A. YATSKO, Teledyne Turbine Engines and B. WINTERS, Orbital Sciences Corporation 0930 hrs 1100 hrs 1130 hrs No Presentation AIAA-2014-3823 AIAA-2014-3824 A Compact Safe Cold Start A Low Cost Modular Approach System for Scramjets using Dilute to Flight Testing of Hypersonic Triethylaluminum Fuel Mixtures Systems S. Gallimore, R. Voland, A. Castrogiovanni, R. Voland, A. Castrogiovanni, ACENT A. Mason, M. Green, ACENT Laboratories, Laboratories, LLC, Bohemia, NY LLC, Manorville, NY Wednesday, 30 July 2014 130-EP-17 Cathodes Room 10

77 Chaired by: R. SHASTRY, NASA Glenn Research Center and M. PATTERSON, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3825 AIAA-2014-3826 AIAA-2014-3827 Experimental Investigation of the Investigation of Energetic Ions in a Reservoir-Type Hollow Cathode for RF-Controlled Hollow Cathode 100-A Hollow Cathode Electric Propulsion Applications M. Plasek, C. Wordingham, S. Rojas Mata, B. Jorns, D. Goebel, I. Mikellides, Jet W. Ohlinger, Self, Babson Park, FL; E. Choueiri, Princeton University, Princeton, Propulsion Laboratory, California Institute B. Vancil, V. Schmidt, eBeam, Inc., NJ; J. Polk, Jet Propulsion Laboratory, of Technology, Pasadena, CA Beaverton, OR; J. Polk, Jet Propulsion California Institute of Technology, Laboratory, California Institute of Pasadena, CA Technology, Pasadena, CA Wednesday, 30 July 2014 131-EP-18 Ion Thrusters - Modeling Room 11 Chaired by: R. WIRZ, UCLA 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3828 AIAA-2014-3829 AIAA-2014-3830 AIAA-2014-3831 Modeling and Simulation of EP A Validation Study of a 3D PIC Investigation of Plasma Leakage Numerical Simulation of Microwave Plasma Plume Expansion into Model for a Miniature Microwave through a Permanent Magnet Cusp Neutralizer Including Ion’s Kinetic Vacuum Discharge Ion Thruster via Particle Simulation Effects F. Cichocki, M. Merino, E. Ahedo, Charles Y. Takao, K. Eriguchi, K. Ono, Kyoto S. Araki, B. Dankongkakul, R. Wirz, K. Kubota, Japan Aerospace Exploration III University of Madrid, Leganés, Spain University, Kyoto, Japan; Y. Sugita, University of California, Los Angeles, Los Agency (JAXA), Chofu, Japan; H. Shizuoka University, Shizuoka, Japan; Angeles, CA Watanabe, Japan Aerospace Exploration H. Koizumi, K. Komurasaki, University of Agency (JAXA), Sagamihara, Japan; Tokyo, Tokyo, Japan N. Yamamoto, H. Nakashima, Kyushu University, Kasuga, Japan; T. Miyasaka, Gifu University, Gifu, Japan; I. Funaki, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Wednesday, 30 July 2014 132-APS-3 Spacecraft Power Concepts Room 12 Chaired by: J. HAINES, Retired - formerly ESA/ESTEC and A. SALIM, Retired - Lockheed Martin Space Systems Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3832 AIAA-2014-3833 AIAA-2014-3834 AIAA-2014-3835 AIAA-2014-3836 Experimental Investigation of Overview of Intelligent Power An Architecture to Enable Simulation and Control Lab Application of Autonomous Latent Heat Thermal Energy Controller Development for Human Autonomous Control of a Spacecraft Development for Power and Energy Spacecraft Power Control Storage for Bi-Modal Solar Thermal Deep Space Exploration R. May, Vantage Partners, LLC, Cleveland, Management for NASA Manned Technology to Terrestrial Microgrids Propulsion J. Soeder, A. Mcnelis, R. Beach, N. OH; J. Soeder, R. Beach, P. George, NASA Deep Space Missions T. Dever, L. Trase, J. Soeder, R. Beach, N. M. Gilpin, University of Southern McNelis, T. Dever, L. Trase, NASA Glenn Glenn Research Center, Cleveland, OH; A. McNelis, R. Beach, J. Soeder, N. McNelis, A. McNelis, NASA Glenn Research California, Los Angeles, CA; D. Scharfe, Research Center, Cleveland, OH; et al. J. Frank, M. Schwabacher, NASA Ames McNelis, NASA Glenn Research Center, Center, Cleveland, OH; et al. ERC, Inc., Edwards AFB, CA; M. Young, Research Center, Moffett Field, CA; et al. Cleveland, OH; R. May, Vantage Partners, Air Force Research Laboratory, Edwards LLC, Cleveland, OH; T. Dever, NASA Glenn AFB, CA; R. Webb, University of Colorado, Research Center, Cleveland, OH; et al. Colorado Springs, Colorado Springs, CO Wednesday, 30 July 2014 133-GTE-17 AIAA/ASME Student Engine Design Competition Room 13 0930 - 1130 hrs Chaired by: I. HALLIWELL, Power Systems Manufacturing LLC Wednesday, 30 July 2014 134-GTE-18 Turbines II Room 14 Chaired by: S. SUBRAMANIAN, QuEST Global, Inc. 0930 hrs 1000 hrs 1030 hrs 78 AIAA-2014-3838 AIAA-2014-3839 AIAA-2014-3840 Comparison of Heat Transfer Time Filtered Navier Stokes (TFNS) Structural Analysis of a Gas Turbine Prediction for Various Turbulence Simulations and Application to Film Disk Containing Heat Pipes Using Models in a Pin Fin Channel Cooling on a Flat Plate Through Finite Element Analysis M. Ricklick, Embry-Riddle Aeronautical Long Cooling Tubes S. Eisenmann, M. Mair, A. Hupfer, University, Daytona Beach, FL; C. A. Ameri, Ohio State University, Columbus, Technical University of Munich, Garching, Carpenter, CD-adapco, Orlando, FL OH Germany Wednesday, 30 July 2014 135-GTE-19 Engine Icing Room 15 Chaired by: J. VERES, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3841 AIAA-2014-3842 AIAA-2014-3843 Analysis of Stall Onset in a Modeling the Deterioration Use of a Turbofan Engine to Multistage Axial Flow Compressor of Engine and Low Pressure Measure Ice Crystal Cloud in Response to Engine Icing Compressor Performance During a Concentration In-Flight R. Kundu, J. Prasad, Georgia Institute of Rollback Event due to Ice Accretion C. Califf, D. Knezevici, General Electric Technology, Atlanta, GA P. Jorgenson, J. Veres, S. Jones, NASA Company, Cincinnati, OH Glenn Research Center, Cleveland, OH Wednesday, 30 July 2014 136-HSABP-7/ABPSI-8 High-Speed Inlets Room 2 Chaired by: R. STARKEY, University of Colorado Boulder and R. NICHOLS, The University of Alabama at Birmingham 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3844 AIAA-2014-3845 AIAA-2014-3846 AIAA-2014-3847 Uncertainty Quantification for a Multifidelity Simulation of a Dual A Fluidic Control Method of Shock Investigation of a Movable Scramjet Inlet Flow Mode Scramjet Compression Train in Hypersonic Inlet/Isolator Slot-Plate Control Method for J. Burt, M. Hagenmaier, D. Eklund, H. System using Coupled NPSS and H. Hexia, T. Huijun, S. Shu, N. Le, College Hypersonic Inlet Unstart Caused by Wilkin, E. Josyula, Air Force Research FLUENT Codes of Energy and Power Engineering, Nanjing, Downstream Mass-Flow Choking Laboratory, Wright-Patterson AFB, OH N. Vijayakumar, D. Wilson, F. Lu, China Z. Qifan, T. Huijun, B. Huanxian, Nanjing University of Texas, Arlington, Arlington, TX University of Aeronautics and Astronautics, Nanjing, China Wednesday, 30 July 2014 137-HR-5 Investigations into Fundamental Physical Processes in Hybrid Rocket Motors Room 20 Chaired by: S. CLAFLIN, Aerojet Rocketdyne and P. LEMIEUX, California State Polytechnic University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3848 AIAA-2014-3849 AIAA-2014-3850 AIAA-2014-3851 Combustion Visualization of Schlieren Imaging of the Visualization of Flames in Effect of “O/F Shift” on Paraffin-Based Hybrid Rocket Fuel Combustion of Classical and High Combustion Chamber of Hybrid Combustion Efficiency at Elevated Pressures Regression Rate Hybrid Rocket Rocket Engine with Multi-Section A. Karabeyoglu, KOC University, Istanbul, E. Jens, Stanford University, Stanford, CA; Fuels Swirl Injection Method Turkey; B. Evans, SPG, Inc., Palo Alto, CA A. Chandler, Jet Propulsion Laboratory, E. Jens, P. Narsai, B. Cantwell, G. H. Tada, S. Aso, Y. Tani, S. Oyama, K. California Institute of Technology, Hubbard, Stanford University, Stanford, CA Araki, Kyushu University, Fukuoka, Japan; Pasadena, CA; B. Cantwell, G. Hubbard, T. Shimada, Japan Aerospace Exploration

79 F. Mechentel, Stanford University, Agency (JAXA), Tokyo, Japan Stanford, CA Wednesday, 30 July 2014 138-APC-3 Unique Propulsion Concepts I Room 21 Chaired by: J. ROBINSON, Retired f/Boeing 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3852 AIAA-2014-3853 AIAA-2014-3854 AIAA-2014-3855 Control of an Active Magnetic Numerical and Experimental PECyT - Plasma Enhanced Cycloidal Film-Evaporation MEMS Tunable Bearing System during Results for a Novel Propulsion Thruster Array: Theory of Operation and Maneuvering Flight Technology Requiring no On-Board C. Xisto, J. Páscoa, M. Abdollahzadeh, J. Proof of Concept K. Zheng, AVIC Shenyang Engine Design Propellant Leger, University of Beira Interior, Covilhã, A. Cofer, W. O’neill, A. Alexeenko, S. and Research Institute, Shenyang, China G. Fetta, Cannae, LLC, Doylestown, PA Portugal; M. Schwaiger, D. Wills, IAT Heister, Purdue University, West Lafayette, 21 Innovative Aeronautics Technologies IN; E. Cardiff, NASA Goddard Space Flight GmbH, Traun, Austria; et al. Center, Greenbelt, MD Wednesday, 30 July 2014 139-EC-4 Stirling Convertor Analysis and Simulation Room 22 Chaired by: L. MASON, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3856 AIAA-2014-3857 AIAA-2014-3858 AIAA-2014-3859 New Analytical Model for Appendix Improving Free-Piston Stirling Development and Validation of an NASA GRC Support of the Flight Gap Losses in Stirling Cycle Engine Speciﬁc Power Advanced Stirling Convertor Model ASRG Project Machines M. Briggs, NASA Glenn Research Center, and Simulation Tool S. Wilson, W. Wong, NASA Glenn Research J. Pfeiffer, H. Kuehl, Technical University of Cleveland, OH J. Metscher, E. Lewandowski, NASA Glenn Center, Cleveland, OH Dortmund, Dortmund, Germany Research Center, Cleveland, OH Wednesday, 30 July 2014 140-TES-2 Numerical Modeling and Simulations Room 23 Chaired by: M. PISZCZOR, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3860 AIAA-2014-3861 AIAA-2014-3862 AIAA-2014-3863 The Use of Software Agents for Modeling Vertical-Axis Wind Residential and Institutional A Benchmark Distribution System Autonomous Control of a DC Space Turbine Performance: Blade Photovoltaic Installations for the Study of Power Quality Power System Element Method vs. Finite Volume M. Sokol, Bold Alternatives, Cleveland, Problems and their Compensation R. May, Vantage Partners, LLC, Cleveland, Approach OH; P. Penko, Baldwin Wallace University, L. Tuladhar, CSU, Cleveland, OH OH; K. Loparo, Case Western Reserve P. Kozak, D. Rempfer, Illinois Institute of Berea, OH University, Cleveland, OH Technology, Chicago, IL Wednesday, 30 July 2014 141-ET-5 Regulation & Reliability in the Energy Sector Room 24 0930 - 1200 hrs Panel 1: Measuring Regulatory Impact of Recent Trends in Power and Energy Resiliency This panel session will examine and summarize power and energy trends and policy outlook at the Federal and State levels for the development of future domestic and global needs. The focuse will be on resiliency in power and energy, including discussions of the impact in Ohio and nationally of hot and cold weather events, plant closures, demand-response advances, and distributed generation in a rapidly changing market. How can a systems approach deﬁne suitable measures of policy success, exposing potential unintended consequences including reduced resiliency? Panelists will also address means of providing ongoing assessment of actual outcomes versus regulatory intent, thereby establishing a framework of accountability for energy sector policies, using tools like value metrics and maturity modeling. Moderator: Carl Dister, Reliabiity First Corp. Panelists: Beth Trumbold, PUCO Theresa Cunniff, Reliabiity First Corp. Paul Centolella, Analysis Group

80 James Stevens, Software Engr Insitute/CMU Panel 2: Using Systems Thinking to Improve the Reliability of Power Delivery Electric power is delivered by a complex system. Occasionally, outages occur unexpectedly and can include whole regions, even in good weather! The North American Power Industry is currently working to improve service reliability by adding focus to strengthening management practices. One approach being used is to formally appraise key management practices by reviewing them through the lens of holistic Systems Thinking. This roundtable discussion will explore the application of Systems Thinking to Improve the Reliability of Power Delivery. Moderator: Michael Ahern, WPI / Power Systems Panelists: Don Gelosh, WPI / Systems Engineering Tim Gallagher, Reliabiity First Corp. Yee Chou, American Electric Power Wednesday, 30 July 2014 142-SCP-2 Integrated Modeling, Design, Simulation and Diagnostics in Systems Room 25 A Chaired by: C. GATTO, Jet Propulsion Laboratory 0930 hrs 1000 hrs AIAA-2014-3864 AIAA-2014-3865 Numerical Study Of a Mach 6 Wind Multi-sensor data fusion using least Tunnel square support vector regression F. Malo-Molina, A. Rougeux, Air Force for missing data online recovery Research Laboratory, Wright-Patterson F. Lu, T. Zhu, J. Huang, Nanjing University AFB, OH of Aeronautics and Astronautics, Nanjing, China Wednesday, 30 July 2014 143-HR-6 Current Programs in Hybrid Rocket Motor Development Room 25 B Chaired by: B. MADHANABHARATAM, Sierra Nevada Corporation and S. COOGAN, Southwest Research Institute 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3866 AIAA-2014-3867 AIAA-2014-3868 AIAA-2014-3869 AIAA-2014-3870 Hybrid Propulsion In-Situ Development and Testing of Effects of Injector Design on Overview of the University of Peregrine Hybrid Rocket Motor Resource Utilization Test Facility Hydrogen Peroxide Hybrid Rocket Combustion Stability in Hybrid Colorado at Boulder Hybrid Development Development Motors at Nammo Raufoss Rockets Using Self-Pressurizing Sounding Rocket Project G. Zilliac, NASA Ames Research Center, A. Chandler, C. Gatto, B. Nakazono, K. C. Verberne, A. Boiron, J. Rønningen, Oxidizers B. Schaefer, C. Brechtel, J. Crowley, B. Moffett Field, CA; B. Waxman, Stanford Grayson, D. Vaughan, Jet Propulsion Nammo Raufoss, Raufoss, Norway B. Waxman, J. Zimmerman, B. Cantwell, Michels, S. Muir, C. Pulido, University of University, Stanford, CA; A. Karabeyoglu, Laboratory, California Institute of Stanford University, Stanford, CA; G. Colorado, Boulder, Boulder, CO; et al. SPG, Inc., Sunnyvale, CA; B. Cantwell, Technology, Pasadena, CA Zilliac, NASA Ames Research Center, Stanford University, Stanford, CA; B. Moffett Field, CA Evans, SPG, Inc., Sunnyvale, CA Wednesday, 30 July 2014 144-PANEL-5 Additive Manufacturing: A Holistic View—From Education, Design, Research, and Production Room 26 A 0930 - 1200 hrs What the can the aerospace industry learn from the new centers for manufacturing innovation launched by the U.S. Department of Commerce? Panelists representing a broad industry cross-section will join representatives of the newly created institutes to discuss the U.S. plans to recapture America’s lead in manufacturing innovation. Moderator: David Salay, Consultant, Ohio Aerospace Institute Panelists: Tim Shinbara, Technical Director, Association for Manufacturing Technology Dan Hartman, DMDI Representative, Rolls-Royce Terri Burgess Sandu, Director, Entrepreneurship Innovation Institute, Executive Director, Workforce, Lorain Community College Lawrence Brown, Executive Director, American Lightweight Materials Manufacturing Innovation Institute (ALMMII)

81 Larry Knauer, President, HSSE, Inc. Wednesday, 30 July 2014 145-PANEL-10 Keeping It Going: Sustainability and Growth in Technology and Workforce Room 26 B 0930 - 1200 hrs This session will discuss the underlying factors that can impact the technology development and transition process, including risk aversion; apathy with regard to the national benefits of aerospace; declining investments that impede our ability to develop, test, and mature key technologies adequately; and our inability to inspire and energize the workforce of tomorrow. The session will also discuss policy changes that can help mitigate these factors. Moderator: Mark Lewis, Director, Science and Technology Policy Institute Panelists: Christopher Singer, Director of Engineering, NASA Marshall Space Flight Center Jarrod (Jay) Littles, Jr., Director of Advanced Launch Propulsion Programs, Aerojet Rocketdyne Neil Garrigan, Executive Manager, Aviation Advanced Technology, GE Aviation Wednesday, 30 July 2014 146-HSABP-6 High-Speed Airbreathing Propulsion III Room 26 C Chaired by: R. HARTFIELD, Auburn University and D. MUSIELAK, University of Texas at Arlington 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3871 AIAA-2014-3872 AIAA-2014-3873 AIAA-2014-3874 Combustion characteristics Diagnostic Investigation of Flow Mixing and Combustion Design of a High Turbulence of single-component liquid field Characteristics of Cavity based Experiments with Hyper-Mixer Intensity Combustion System hydrocarbon in a scramjet Scramjet Combustors Injectors in a Scramjet Combustor A. Acosta-Zamora, A. Choudhuri, A. combustor V. Sanal Kumar, Kumaraguru College of N. Kubo, Tohoku University, Sendai, Japan; Hossain, M. Quiroz, University of Texas, El W. Liu, Beihang University, Beijing, China Technology, Coimbatore, India S. Tomioka, A. Murakami, K. Kudo, Japan Paso, El Paso, TX Aerospace Exploration Agency (JAXA), Kakuda, Japan Wednesday, 30 July 2014 147-LP-15 Modeling and Simulation of Engines and Propulsion Systems Room 3 Chaired by: T. GIEL, Jacobs Technology and D. PRECLIK, Astrium, an EADS Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3875 AIAA-2014-3876 AIAA-2014-3877 AIAA-2014-3878 AIAA-2014-3879 Conceptual Design, Feasibility and Development of Thrust Chamber Throttling of Liquid Rockets using Performance Analysis of Design-For-Reliability Payoff Analysis of a Third Stage Components for a System Analysis Higher Order Sliding Mode Control Low-Complexity Upper-Stage Considerations and Modeling for for EELV Tool C. Tournes, Tournes Associates, Madison, Demonstrator Engines Liquid Propulsion Engines Starting N. Sedano, J. Painter, Air Force Research M. Leonardi, University of Rome “La AL; P. Reimonte, Centro Espacial Teofilio A. Herbertz, C. Manfletti, C. Fromm, from Conceptual Design Laboratory, Edwards AFB, CA Sapienza”, Rome, Italy; F. Di Matteo, Tabanera, Codoba, Argentina; Y. Shtessel, German Aerospace Center (DLR), Z. Huang, Aerojet Rocketdyne, Canoga J. Steelant, ESA, Noordwijk, The University of Alabama, Huntsville, Hardthausen, Germany Park, CA Netherlands; B. Betti, F. Nasuti, M. Onofri, Huntsville, AL University of Rome “La Sapienza”, Rome, Italy Wednesday, 30 July 2014 148-LP-16 MPCV European Service Module Propulsion System Room 4 Chaired by: A. FRANKEL, Moog Inc, ISP Division and D. COOTE, NASA Stennis Space Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3880 AIAA-2014-3881 AIAA-2014-3882 AIAA-2014-3883 Evolution of MPCV Service An Overview of the Concept Implementation of the Orbital Plume Impingement Analysis for Module Propulsion and GN&C of Operations for Assembly, Maneuvering System Engine the European Service Module Interface Requirements between Integration, Testing and Ground and Thrust Vector Control for the Propulsion System Constellation and European Service Servicing Developed for the MPCV- European Service Module J. Yim, NASA Glenn Research Center, Module ESM Propulsion System J. Millard, B. Reed, NASA Glenn Research Cleveland, OH; F. Sibé, Airbus Defense and

82 H. Hickman, NASA Glenn Research Center, M. Bielozer, NASA Glenn Research Center, Center, Cleveland, OH Space, Les Mureaux, France; N. Lerardo, Cleveland, OH Cleveland, OH ESA/ESTEC, Noordwijk, The Netherlands Wednesday, 30 July 2014 150-ABPSI-9 Propellers, Small Engines, & Alternative Fuels Room 6 Chaired by: C. HUGHES, NASA Glenn Research Center and K. BLODGETT, GE Aviation 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3886 AIAA-2014-3887 AIAA-2014-3888 Unsteady Flow Simulations of Open-Rotor Aerodynamics Experimental Validation of an Over-the-wing Propeller Installation Effects By a RANS- Modifications to a TDI Model Configuration Lifting Line Coupling Method 2700 Turbine Powered Simulator L. Müller, Technical University of M. Barry, Safran Group, Snecma, to Simulate a High-Bypass Ratio Braunschweig, Braunschweig, Germany; Villaroche, France Engine D. Kozulovic, Hamburg University of D. Tompkins, The Boeing Company, Applied Sciences, Hamburg, Germany; Huntington Beach, CA; J. Flamm, NASA J. Friedrichs, Technical University of Langley Research Center, Hampton, VA; Braunschweig, Braunschweig, Germany K. Long, K. James, NASA Ames Research Center, Moffett Field, CA Wednesday, 30 July 2014 151-SR-6 Solid Rocket Motor Systems - Historical and Current Developments Room 7 Chaired by: W. RYAN, United Launch Alliance, LLC and B. LEARY, JHU/Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3891 AIAA-2014-3890 AIAA-2014-3889 VEGA new first stage: P105 Zefiro 40 Solid Rocket Motor Surveyor and the Birth of the STAR SRM - Overview of Technological Technological and programmatic Motor Line innovations development status D. McGrath, Alliant Techsystems, Elkton, D. Scoccimarro, Avio S.p.A., Colleferro, C. Di Trapani, A. Mataloni, F. Giliberti, MD Italy A. Di Cosmo, N. Pasquale, Avio S.p.A., Colleferro, Italy; C. Milana, ELV S.p.A., Colleferro, Italy Wednesday, 30 July 2014 152-ECS-2 Metal Composite Powders, Nanosize Fuels, Additives, Oxidizers Effects and Experimental Methods Room 8 Chaired by: J. BAGLINI, Exodynamics Technology Incorporated 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3892 AIAA-2014-3893 AIAA-2014-3894 AIAA-2014-3895 Metal-Composite Powder Energetic Peculiarities in the Formation of Additive Manufacturing for Experiment Study on the Materials Nanosize Fuels during Attrition Energetic Components and Performance of Explosive Cutting A. Sherman, N. Farkas, Terves, Inc., Milling in Organic Solvents Materials H. Guan, Beihang University, Beijing, Euclid, OH M. Puszynski, Innovative Materials and F. Ruz-Nuglo, L. Groven, J. Puszynski, China; Y. Zhu, X. Zhang, W. Song, Aviation Processes, LLC, Rapid City, SD; J. Schley, South Dakota School of Mines and Industry Corporation of China (AVIC), South Dakota School of Mines and Technology, Rapid City, SD Xi’an, China Technology, Rapid City, SD; Z. Doorenbos,

83 Innovative Materials and Processes, LLC, Rapid City, SD; J. Puszynski, South Dakota School of Mines and Technology, Rapid City, SD Wednesday, 30 July 2014 153-EP-19 Hall - Magnetic Shielded Thrusters Room 9 Chaired by: D. HERMAN, NASA Glenn Research Ctr and D. BROWN, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3896 AIAA-2014-3897 AIAA-2014-3898 AIAA-2014-3899 Magnetically Shielded Miniature Assessment of Pole Erosion in a Preliminary Performance Pole-piece Interactions with the Hall Thruster: Performance Magnetically Shielded Hall Thruster Characterization of the SEP TDM Plasma in a Magnetically Shielded Assessment and Status Update I. Mikellides, A. Lopez Ortega, B. Jorns, 12.5-kW Hall Thruster Hall Thruster R. Conversano, University of California, Jet Propulsion Laboratory, California H. Kamhawi, W. Huang, R. Shastry, G. D. Goebel, B. Jorns, R. Hofer, I. Mikellides, Los Angeles, Los Angeles, CA; D. Goebel, Institute of Technology, Pasadena, CA Soulas, D. Herman, NASA Glenn Research I. Katz, Jet Propulsion Laboratory, I. Mikellides, R. Hofer, Jet Propulsion Center, Cleveland, OH; R. Hofer, Jet California Institute of Technology, Laboratory, California Institute of Propulsion Laboratory, California Institute Pasadena, CA Technology, Pasadena, CA; T. Matlock, R. of Technology, Pasadena, CA; et al. Wirz, University of California, Los Angeles, Los Angeles, CA; et al. Wednesday, 30 July 2014 154-LNCH-3 Awards Luncheon Grand Ballroom B 1200 - 1330 hrs Wednesday, 30 July 2014 155-PLENARY-7 Advanced Manufacturing Solutions for P&E Systems - The View from Users Grand Ballroom A 1330 - 1500 hrs Representatives from leading manufacturers of aerospace systems will discuss how their organizations are utilizing advanced manufacturing today and how new advancements will impact their processes in the future. Moderator: Christine Furstoss, Global Technology Director, Manufacturing & Materials Technologies, GE Global Research Panelists: Homer “H.D.” Stevens, Chief Engineer, STAR Labs, Lockheed Martin Space Subsystems, Space Technology Advanced R&D Labs Edward Morris, Director, America Makes - National Additive Manufacturing Innovation Institute, Vice President, National Center for Defense Manufacturing and Machining (NCDMM) Jerrol (Jay) Littles, Jr., Director of Advanced Launch Propulsion Programs, Aerojet Rocketdyne Tom Williams, Manager, Propulsion Engineering Division, NASA Marshall Space Flight Center Wednesday, 30 July 2014 156-NW-7 Networking Break Exhibit Hall C 1500 - 1530 hrs Wednesday, 30 July 2014 157-HSABP-8/PC-9 Rotating Detonation Engines Room 1 Chaired by: V. TANGIRALA, General Electric and A. SIEBENHAAR, Aerojet Rocketdyne 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3900 AIAA-2014-3901 AIAA-2014-3902 AIAA-2014-3903 Oral Presentation Area Effects on Rotating Detonation Effect of Low Pressure Ratio Survey of Rotating Detonation Numerical Study of Detonation Thrust Measurement of Rotating Engine Performance on Exhaust Plumes of Rotating Wave Combustor Technology Wave Propagation in Non- Circular Detonation Engine by Sled Test C. Nordeen, University of Connecticut, Detonation Engines and Potential Rocket Vehicle Channels for Arbitrary Shaped Y. Kato, Nagoya University, Nagoya, Storrs, Storrs, CT; D. Schwer, A. Corrigan, D. Schwer, K. Kailasanath, Naval Research Applications Rotating Detonation Engines Japan; K. Gawahara, University of Naval Research Laboratory, Washington, Laboratory, Washington, DC S. Heister, D. Stechmann, Purdue T. Kim, J. Choi, Pusan National University, Tsukuba, Tsukuba, Japan; K. Matsuoka, DC J. Kasahara, Nagoya University, Nagoya, 84 University, West Lafayette, IN Busan, South Korea Japan; A. Matsuo, Keio University, Yokohama, Japan; I. Funaki, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; et al.

Wednesday, 30 July 2014 158-EP-20 Mission Concepts Room 10 Chaired by: L. BURKE, NASA-Glenn Research Center and D. MANZELLA, NASA Glenn Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-3905 AIAA-2014-3906 AIAA-2014-3907 AIAA-2014-3908 AIAA-2014-3909 AIAA-2014-3910 Mission and System Advantages of Feasibility of All-Electric Three Axis A Direct Drive Experiment as Part Mission Analysis for a Micro RF Quad channel Micro-Cathode Iodine Hall Thruster Demonstration Iodine Hall Thrusters Momentum Management for Deep of a SEP Demonstration Ion Thruster for CubeSat Orbital Arc Thruster Electric Propulsion Mission Concept and Development J. Dankanich, NASA Marshall Space Space Small Body Rendezvous W. Deininger, S. Enger, B. Unruh, Ball Maneuvers subsystem for the Ballistic J. Dankanich, K. Polzin, NASA Marshall Flight Center, Huntsville, AL; J. Szabo, D. Oh, S. Collins, T. Randolph, C. Vanelli, Aerospace & Technologies Corporation, D. Kolosa, Western Michigan University, Reinforced Satellite (BRICSat-P) Space Flight Center, Huntsville, AL; H. B. Pote, Busek Company, Inc., Natick, Jet Propulsion Laboratory, California Boulder, CO; B. Pote, V. Hruby, Busek Kalamazoo, MI; S. Spangelo, Jet S. Haque, George Washington University, Kamhawi, NASA Glenn Research Center, MA; S. Oleson, H. Kamhawi, NASA Glenn Institute of Technology, Pasadena, CA; S. Company, Inc., Natick, MA; D. Murphy, Propulsion Laboratory, California Institute Washington, DC; C. Dinelli, U.S. Cleveland, OH Research Center, Cleveland, OH Tilley, Space Systems/Loral, Palo Alto, CA ATK, Goleta, CA of Technology, Pasadena, CA; K. Lemmer, Naval Academy, Annapolis, MD; M. J. Hudson, Western Michigan University, Keidar, George Washington University, Kalamazoo, MI Washington, DC Wednesday, 30 July 2014 159-EP-21 Micro-Thrusters Room 11 Chaired by: J. POLK, Jet Propulsion Laboratory 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3911 AIAA-2014-3912 AIAA-2014-3913 AIAA-2014-3914 AIAA-2014-3915 Miniaturized Radio Frequency Ion Experimental characterization of Experimental Study for New Low-Power Plasma Thruster Iodine Hall Thruster Propellant Thrusters and Systems - Technology an open-ended spiral-type antenna Enhancement Thrust Force of the for Nanosatellites Feed System for a CubeSat Development and Applications RF plasma source ECR Ion Thruster μ10 J. Sheehan, B. Longmier, I. Reese, T. K. Polzin, NASA Marshall Space Flight H. Leiter, C. Altmann, D. Lauer, R. Kukies, J. Little, E. Choueiri, Princeton University, I. Nishiyama, University of Tokyo, Bunkyo, Collard, University of Michigan, Ann Arbor, Center, Huntsville, AL Airbus, Heilbronn, Germany Princeton, NJ Japan; R. Tsukizaki, K. Nishiyama, Japan Ann Arbor, MI Aerospace Exploration Agency (JAXA), Sagamihara, Japan; H. Kuninaka, University of Tokyo, Bunkyo, Japan Wednesday, 30 July 2014 160-PC-11 Combustion Modeling and Simulation III Room 12 Chaired by: J. MURPHY, The Aerospace Corporation 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3916 AIAA-2014-3917 AIAA-2014-3918 AIAA-2014-3919 AIAA-2014-3920 Numerical Investigations of a Low Unsteady Thermo-Gasdynamic Prediction of Spatial Distributions Preliminary Study of Reacting Flow Fast and robust time integration Emission Gas Turbine Combustor Processes in Scramjet Combustion of Equilibrium Product Species from Field in A Burner with Cap-induced method for sti chemical kinetic using Detailed Chemistry Chamber with Periodical Input of High Explosive Blasts in Air Premixing Combustion ODEs A. Filosa, B. Noll, M. Di Domenico, M. Cold Air A. Brundage, S. Attaway, M. Hobbs, M. K. Pan, E. Fang, S. Zhang, National Y. Morii, Japan Aerospace Exploration Aigner, German Aerospace Center (DLR), S. Surzhikov, Russian Academy of Kaneshige, L. Boye, Sandia National Taiwan University, Taipei, Taiwan Agency (JAXA), Sagamihara, Japan; H. Stuttgart, Germany Sciences, Moscow, Russia; R. Seleznev, Laboratories, Albuquerque, NM Terashima, University of Tokyo, Tokyo,

85 All-Russian Scientific Research Institute of Japan; M. Koshi, Yokohama National Automatics, Moscow, Russia; P. Tretjakov, University, Yokohama, Japan; T. Shimizu, V. Zabaykin, Russian Academy of Sciences, Japan Aerospace Exploration Agency Novosibirsk, Russia (JAXA), Sagamihara, Japan Wednesday, 30 July 2014 161-GTE-20 Vehicle Integrated Propulsion Research (VIPR) Room 13 Chaired by: J. LEKKI, NASA Glenn Research Center and J. LITT, NASA Glenn Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2014-3922 AIAA-2014-3923 AIAA-2014-3924 AIAA-2014-3925 Vehicle Integrated Propulsion Development and performance Design and operation of a fast, An Integrated Architecture for Aircraft Ground Demonstration Research Overview verification of fiber optic thin-film thermocouple probe on a Aircraft Engine Performance of Engine Emissions Monitoring J. Lekki, NASA Glenn Research Center, temperature sensors in high turbine engine Monitoring and Fault Diagnostics: System Based on a Gas Microsensor Cleveland, OH temperature engine environments R. Meredith, J. Wrbanek, G. Fralick, L. Engine Test Results Array G. Adamovsky, NASA Glenn Research Greer, G. Hunter, NASA Glenn Research A. Rinehart, Vantage Partners, LLC, Brook G. Hunter, D. Simon, J. Xu, A. Biaggi- Center, Cleveland, OH; J. Mackey, Vantage Center, Cleveland, OH; L. Chen, Ohio Park, OH; D. Simon, NASA Glenn Research Labiosa, NASA Glenn Research Center, Partners, LLC, Cleveland, OH; B. Floyd, Aerospace Institute, Brook Park, OH Center, Cleveland, OH Cleveland, OH; S. Carranza, D. Makel, Sierra Lobo, Inc., Cleveland, OH; K. Elam, Makel Engineering, Inc., Chico, CA Jacobs, Cleveland, OH; M. Martinez, NASA Dryden Flight Research Center, Edwards, CA Wednesday, 30 July 2014 162-GTE-21 Engine Cycle Simulation & Modeling Room 14 Chaired by: R. BRUCKNER, NASA Glenn Research Center and J. LITT, NASA Glenn Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2014-3926 AIAA-2014-3927 AIAA-2014-3928 AIAA-2014-3929 AIAA-2014-3930 AIAA-2014-3931 AIAA-2014-3932 Turbofan Engine Transient Compressor Modeling and Using Density Estimation in Propulsion System Simulation Development of a twin-spool A Process for the Creation of Cantera Integration with the Response Predictions Using Real- Simulation Using Object-Oriented Comparing Input Signals for Gas Using the Toolbox for the Modeling turbofan engine simulation T-MATS Propulsion System Models Modeling and Analysis of Time Analytical Linear Models Turbomachinery Analysis Code Turbine Engine Transient Models and Analysis of Thermodynamic using the Toolbox for Modeling from NPSS data Thermodynamic Systems (T MATS) G. Chung, J. Prasad, Georgia Institute of (OTAC) M. Ozcan, B. Kestner, J. Tai, D. Mavris, Systems (T MATS) and Analysis of Thermodynamic J. Chapman, Vantage Partners, LLC, Brook T. Guo, T. Lavelle, NASA Glenn Research Technology, Atlanta, GA R. Denney, B. Kestner, D. Mavris, Georgia Georgia Institute of Technology, Atlanta, J. Chapman, Vantage Partners, LLC, Systems (T-MATS) Park, OH; T. Lavelle, J. Litt, T. Guo, NASA Center, Cleveland, OH Institute of Technology, Atlanta, GA GA Brook Park, OH; T. Lavelle, NASA Glenn A. Zinnecker, N&R Engineering, Inc., Glenn Research Center, Cleveland, OH Research Center, Cleveland, OH; R. May, Parma Heights, OH; J. Chapman, Vantage Vantage Partners, LLC, Brook Park, OH; J. Partners, LLC, Brook Park, OH; T. Lavelle, Litt, T. Guo, NASA Glenn Research Center, J. Litt, NASA Glenn Research Center, Cleveland, OH Cleveland, OH Wednesday, 30 July 2014 163-GTE-22 Variable Speed Power Turbine (VSPT) Room 15 Chaired by: P. GIEL, VPL and A. FLEGEL, NASA Glenn Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3933 AIAA-2014-3934 AIAA-2014-3935 AIAA-2014-3936 AIAA-2014-3938 Aerodynamic Effects of High Inlet Turbulence and Length Scale Simulation of VSPT Experimental Midline Heat Transfer and Pressure Heat Transfer Measurements in a Turbulence Intensity on a Variable- Measurements in a Large Scale Cascade under High and Low Free- Measurements on an Incident Compressible Flow Vane Cascade Speed Power-Turbine Blade with Transonic Turbine Cascade Stream Turbulence Conditions Tolerant Blade Section for a Showing the Influence of Reynolds Large Incidence and Reynolds D. Thurman, Army Research Laboratory, A. Ameri, Ohio State University, Columbus, Variable Speed Power Turbine Number, Mach Number, and

86 Number Variations Cleveland, OH; A. Flegel, NASA Glenn OH; P. Giel, Vantage Partners, LLC, Brook at Low to Moderate Reynolds Turbulence Level on Transition and A. Flegel, NASA Glenn Research Center, Research Center, Cleveland, OH; P. Giel, Park, OH; A. Flegel, NASA Glenn Research Numbers in a Transonic Turbine Augmentation of Laminar Heat Cleveland, OH; P. Giel, Vantage Partners, Vantage Partners, LLC, Cleveland, OH Center, Cleveland, OH Cascade Transfer by Free-Stream Turbulence LLC, Cleveland, OH; G. Welch, NASA Glenn L. Moualeu, F. Ames, University of North K. Stahl, L. Moualeu, J. Long, F. Ames, Research Center, Cleveland, OH Dakota, Grand Forks, Grand Forks, ND; University of North Dakota, Grand Forks, Y. Suzen, North Dakota State University, Grand Forks, ND; Y. Suzen, North Dakota Fargo, ND State University, Fargo, ND Wednesday, 30 July 2014 164-EP-24 Effects of Ground Test Facilities on Electric Propulsion Thruster Characteristics - ITAR Panel Session Room 16 1500 - 1830 hrs Chaired by: D. HERMAN, NASA Glenn Research Ctr and D. BROWN, Air Force Reseach Laboratory Invited panel consisting of participants from NASA (Dr. Wensheng Huang - Glenn Research Center and Dr. Richard Hofer - Jet Propulsion Laboratory), the Air Force Research Laboratory (Dr. Dan Brown), the Aerospace Corporation (Dr. Mark Crofton), and Aerojet Rocketdyne (Dr. David King) will present findings from investigations of the effect of the ground test facility on electric propulsion thrusters. Topics will cover ion and Hall thruster technologies, the effect of background pressure, the impact of grounded facility structures, and comparison of flight to ground test data. Wednesday, 30 July 2014 165-HSABP-9 Special Session on Supersonic Combustion Simulation (Invited) Room 19 Chaired by: F. LADEINDE, TTC Technologies Inc and F. MALO-MOLINA, Air Force Reseach Laboratory 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation AIAA-2014-3940 Oral Presentation AIAA-2014-3941 Model ‘Steering” for LES of High Mach Number Implications for Analysis of Successful Pulsed Turbulence/Chemistry Interaction Fundamental Physics and Supersonic Turbulent Combustion Flamelet Modeling of Supersonic Detonation vs. a Deflagration in a in High-Speed Combustion: LES of Model Assumptions in Turbulent J. Edwards, T. Echekki, C. Patton, T. Combustion Supersonic Combustor UV Dual-Mode Scramjet Combustor Combustion Models for Aerospace Wignall, North Carolina State University, F. Ladeinde, Z. Lou, Stony Brook F. Malo-Molina, Air Force Research M. Ihme, Stanford University, Stanford, Propulsion Raleigh, NC University, Stony Brook, NY; W. Li, TTC Laboratory, Wright-Patterson AFB, OH CA; W. Chan, University of Michigan, Ann V. Sankaran, Air Force Research Technologies, Inc., Centereach, NY Arbor, Ann Arbor, MI Laboratory, Edwards AFB, CA; C. Merkle, Purdue University, West Lafayette, IN Wednesday, 30 July 2014 166-HSABP-10 Experimental Investigations in High-Speed Propulsion Room 2 Chaired by: J. LEE, NASA-Glenn Research Center and J. CASTRO, Pratt & Whitney-Rocketdyne 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2014-3942 AIAA-2014-3943 AIAA-2014-3944 AIAA-2014-3945 AIAA-2014-3946 AIAA-2014-3947 AIAA-2014-3948 Skin Friction Sensor for High- Investigation of Ethylene Fuel Combustion Experiments for a Effect of Fin-Guided Fuel Injection Compression Wave Structure Experimental investigation on the Design Analysis of the Sampling Speed, High-Enthalpy Scramjet Combustion in a Dual-Mode Liquid Hydrocarbon Fueled Mach 5 on Dual Mode Scramjet Operation on Droplets under Supersonic multi-staged injection in a strut- Probe for Supersonic Combustion Flow Applications Combustor Scramjet Engine Model C. Aguilera Munoz, K. Yu, University of Conditions cavity based scramjet combustor W. Jianchen, L. Yuzhen, Beihang R. Meritt, J. Schetz, Virginia Polytechnic K. Nojima, Y. Suzuki, Tohoku University, I. Yang, Y. Lee, K. Lee, Korea Aerospace Maryland, College Park, College Park, MD E. Lin, J. Hermanson, University of W. Jianchen, L. Yuzhen, Z. Yongsheng, L. University, Beijing, China Institute and State University, Blacksburg, Sendai, Japan; S. Tomioka, N. Research Institute, Daejeon, South Korea Washington, Seattle, Seattle, WA Wei, Beihang University, Beijing, China; VA; J. Donbar, Air Force Research Sakuranaka, Japan Aerospace Exploration Z. Yan, Nanyang Institute of Technology, Laboratory, Wright-Patterson AFB, OH; J. Agency (JAXA), Kakuda, Japan Nanyang, China 87 Tam, Taitech, Inc., Beavercreek, OH Wednesday, 30 July 2014 167-HR-7 New Hybrid Motor Concepts Room 20 Chaired by: B. EVANS, Stanford University and M. KOBALD, DLR-German Aerospace Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2014-3949 AIAA-2014-3950 AIAA-2014-3951 AIAA-2014-3952 AIAA-2014-3953 AIAA-2014-3954 AIAA-2014-3955 Development of a Power Efficient, Low Frequency Instability in Experimental Demonstration of Study on the key technologies of a Optimization of Hybrid Propellant Study on Hybrid Rocket with Multi- Hybrid Rocket Burning Rate Restart-Capable Arc Ignitor for Labscale Hybrid Rocket Motors the Vacuum Specific Impulse of a Hybrid Rocket & Ramjet Combined Mars Ascent Vehicle Section Swirl Injection Method Enhancement by Nano-Scale Hybrid Rockets K. Park, C. Lee, Konkuk University, Seoul, Hybrid Rocket Engine Cycle Engine L. Casalino, D. Pastrone, Technical toward Flight Experiments of Additives in HTPB Fuel Grains S. Whitmore, D. Merkley, N. Inkley, Utah South Korea J. Anthoine, J. Lestrade, ONERA, Mauzac, I. Nakagawa, Y. Ezawa, Tokai University, University of Turin, Turin, Italy Subscale Space Plane J. Thomas, E. Petersen, Texas A&M State University, Logan, UT France; C. Verberne, A. Boiron, Nammo Hiratsuka, Japan K. Ohe, S. Oyama, K. Araki, S. Aso, Y. University, College Station, TX; B. Brady, Raufoss, Raufoss, Norway; C. Figus, G. Tani, Kyushu University, Fukuoka, Japan; J. Desain, The Aerospace Corporation, El Khimeche, Airbus, Toulouse, France T. Shimada, Japan Aerospace Exploration Segundo, CA Agency (JAXA), Tokyo, Japan Wednesday, 30 July 2014 168-APC-4 Unique Propulsion Concepts II Room 21 Chaired by: J. ROBINSON, Retired f/Boeing 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3956 AIAA-2014-3957 AIAA-2014-3958 AIAA-2014-3959 AIAA-2014-3960 Conceptual Design for a Dual-Bell Generating Higher and Controllable Application of Aerogravity Assist Experimental Investigation of Fugine: the supermultijet- Rocket Nozzle System Using a Thrust and Specific Impulse with with Active Cooling and Thermal Magnetoplasma Sail with High Beta convergence engine working from NASA F-15 Airplane as the Flight Electronic Cyclotron Resonance EP Propulsion to the Solar Probe Plasma Jet startup to hypersonic scram mode Testbed J. Brainerd, A. Reisz, Reisz Engineers, Mission Y. Oshio, I. Funaki, K. Ueno, Japan and attaining simultaneously D. Jones, T. Bui, C. St. John, M. Martinez, Huntsville, AL D. Murakami, NASA Ames Research Aerospace Exploration Agency (JAXA), light-weight, high-efficiency, and NASA Dryden Flight Research Center, Center, Moffett Field, CA Sagamihara, Japan; H. Yamakawa, Kyoto low noise Edwards, CA; J. Ruf, NASA Marshall Space University, Uji, Japan K. Naitoh, Y. Sagara, T. Tamura, T. Flight Center, Huntsville, AL Hashimoto, Y. Nojima, M. Tanaka, Waseda University, Tokyo, Japan Wednesday, 30 July 2014 169-EC-5 Stirling Power System Analysis and Testing Room 22 Chaired by: S. ORITI, NASA Glenn Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-3961 AIAA-2014-3962 AIAA-2014-3963 AIAA-2014-3964 AIAA-2014-3965 AIAA-2014-3966 Thermoacoustic Duplex Technology Advanced Stirling Convertor (ASC) The Use of Redundancy to Improve Test Program for Stirling Telemetry Analysis of the Advanced System-level Testing of the for Cooling and Powering a Venus Development for NASA RPS Reliability of Deep Space Missions Radioisotope Generator Hardware Stirling Radioisotope Generator Advanced Stirling Radioisotope Lander W. Wong, S. Wilson, NASA Glenn Using an ASRG (Advance Stirling at NASA Glenn Research Center Using a Steady State Modeling Generator Engineering Hardware M. Haberbusch, C. Nguyen, A. Walker, J. Research Center, Cleveland, OH; J. Collins, Radioisotope Generator) Power E. Lewandowski, NASA Glenn Research Approach T. Chan, Lockheed Martin Space Systems Sasson, Sierra Lobo, Inc., Milan, OH Sunpower, Inc., Athens, OH Center, Cleveland, OH; G. Bolotin, Jet A. Mahpour, G. Bolotin, Jet Propulsion Company, King of Prussia, PA

88 Source S. Di Stefano, C. Everline, G. Bolotin, Jet Propulsion Laboratory, California Institute Laboratory, California Institute of Propulsion Laboratory, California Institute of Technology, Pasadena, CA; S. Oriti, Technology, Pasadena, CA of Technology, Pasadena, CA NASA Glenn Research Center, Cleveland, OH Wednesday, 30 July 2014 170-TM-4 Aerospace and Terrestrial Energy Systems Thermal Management Room 23 Chaired by: M. CHOI, NASA-Goddard Space Flight Center and C. TARAU, Advanced Cooling Technologies 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2014-3967 AIAA-2014-3968 AIAA-2014-3969 AIAA-2014-3970 AIAA-2014-3971 AIAA-2014-3972 AIAA-2014-3973 The Energy Balance of Circulation- CFD Modelling of An Open Air Development of high melting Numerical modeling and simulation Scope, Objectives and International Numerical and experimental Thermoacoustic Oscillations in type Superheated Steam Stadium Air Conditioning temperature microencapsulated of an integrated TEG/PCM system Dimension of a Dynamic Aircraft analysis into the thermal Supercritical Fuel Flows degreasing Systems for Oily Metal A. Abu-Kabsha, E. Khalil, A. Jouda, M. phase change material for for the enhancement of PV power Robust Power Management performance of a novel phase S. Heister, S. Hunt, Purdue University, Recycling Muhammad, M. Afify, Cairo University, compacted thermal energy storage output Programme change material gypsum board West Lafayette, IN N. Maruyama, Y. Watanabe, H. Ito, Y. Giza, Egypt bed D. Du, J. Darkwa, G. Kokogiannakis, J. Van Muijden, B. Eussen, National T. Zhou, J. Darkwa, G. Kokogiannakis, Achawangkul, M. Hirota, Mie University, W. Su, J. Darkwa, G. Kokogiannakis, University of Nottingham, Ningbo, China Aerospace Laboratory (NLR), Amsterdam, University of Nottingham, Ningbo, China Tsu, Japan University of Nottingham, Ningbo, China The Netherlands Wednesday, 30 July 2014 171-ET-6 Systems Engineering Electric Utilities for Resiliency Room 24 1500 - 1800 hrs Systems Engineering Resilient Electric Utilities in a Rapidly Changing Environment This panel continues the discussions from the Regulatory Panel, looking more deeply into the systems engineering models required to facilitate public policy success, and help measure the regulatory impact of measures aimed at making Electric Utilities more resilient. The panelists will discuss future interoperability of classic power systems tools with emerging risk communication models, reliability models, ecosystem impact models, maturity models, and social complexity models. The ability for these tools to offset the loss of design capabilities in the power industry, coupled with the new complex resiliency skills required to restore the aging infrastructure will also be examined. Moderator: Carl Dister, Reliabiity First Corp. Panelists: Dr. Rajeev Rajaram, Kent State University Dr. Dan Kovacs, Decision Partners Thom Pearce, PUCO Brian Keaveny, Nescaum Matthew Butkovic, Carnegie Mellon Wednesday, 30 July 2014 172-SCP-3 Engineering, Sensing, Measuring and Distributed Technologies for Propulsion Systems Room 25 A Chaired by: T. GIEL, Jacobs Technology and T. CHEN, NASA 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3974 AIAA-2014-3975 AIAA-2014-3976 AIAA-2014-3977 AIAA-2014-3978 Design and Selection Criteria of Application of the Tool for Turbine Development of Self-Reliant A Review of Exhaust Gas Limit Protection in Gas Turbine High Temperature Accelerometers Engine Closed-loop Transient Satellite-Level Propulsion System Temperature Sensing Techniques Engines Based on Reference and B. Metz, PCB Piezotronics, Inc., Depew, Analysis (TTECTrA) for Dynamic by Using Hydrogen Peroxide for Modern Turbine Engine Controls Extended Command Governors NY Systems Analysis Propellant A. Von Moll, A. Behbahani, Air Force I. Kolmanovsky, University of Michigan, J. Csank, NASA Glenn Research Center, H. Liu, Y. Chan, C. Pai, K. Tseng, Y. Chen, Research Laboratory, Wright-Patterson Ann Arbor, Ann Arbor, MI; W. Merill, 89 Cleveland, OH; A. Zinnecker, N&R Y. Chan, National Space Organization, AFB, OH; G. Fralick, J. Wrbanek, G. Bluberry, LLC, Columbia Station, OH Engineering, Inc., Parma Heights, OH Hsinchu, Taiwan; et al. Hunter, NASA Glenn Research Center, Cleveland, OH Wednesday, 30 July 2014 173-PC-10 Combustion Diagnostics II Room 25 B Chaired by: L. SMITH, United Technologies Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-3979 AIAA-2014-3980 AIAA-2014-3981 AIAA-2014-3982 AIAA-2014-3983 AIAA-2014-3984 Characterization and Analysis Measurements of Laminar Flame Ion Measurements in Premixed Measurement of Plasma Activity in Shock Tube Measurements of the Blast Wave Propagation in Cross- of Plain Jet Injection of Liquid Speeds of Alternative Gaseous Fuel Methane-Oxygen Flames a 1D Premixed Methane-Air Flame Branching Ratios of Propene + OH Flow of Detonable Mixture Alternative Fuels Into a Crossflow Mixtures A. Alquaity, N. Hourani, M. Chahine, S. Jacobs, B. Roy, K. Xu, University of -> Products J. Burr, K. Yu, University of Maryland, C. Brown, U. Mondragon, V. McDonell, A. Ibrahim, M. Abdalwahab, O. Abulaban, H. Selim, M. Sarathy, A. Farooq, King Alabama, Huntsville, Huntsville, AL F. Khaled, J. Barda, A. Faooq, King College Park, College Park, MD Energy Research Consultants, Laguna S. Ahmed, Qatar University, Doha, Qatar Abdullah University of Science and Abdullah University of Science and Hills, CA Technology, Thuwal, Saudi Arabia Technology, Thuwal, Saudi Arabia Wednesday, 30 July 2014 174-PANEL-11 Energy Trends and Its Implications on Advanced Technology Room 26 A 1500 - 1800 hrs Today’s energy landscape is complicated by increasing energy demands, the push for increased energy efficiency, and the introduction of advanced energy technology. These challenges have varying implications from industry, Government, and regional perspectives. Panelists will address the current energy situation, future trends, and potential plans from their organization’s perspective. Moderator: Matt Moran, Sector Manager for Energy & Materials, NASA Glenn Research Center Panelists: Hasso Weiland, Technical Fellow, Alcoa Advanced Technical Center Lorry Wagner, President, LEEDCo Larry Viterna, President, Nautica Wind Power LLC Rao Tatavarti, Technical Director, MicroLink Devices, Inc. Michael Sweet, Director-MES, First Solar (invited) Byron Clayton, Vice President, NorTech (invited) Paul Savage, CEO, Nextek Power Systems (invited) Wednesday, 30 July 2014 175-PANEL-12 70 Years of Power and Space Propulsion at NASA Glenn Research Center Room 26 B 1500 - 1800 hrs A historical perspective on power and space propulsion research conducted at NASA Glenn Research Center over the past 70 years will be presented, with emphasis on research related to electrical, chemical and nuclear propulsion, cryogenic propellants, direct energy conversion, and electrochemical and energy storage. Moderator: George Schmidt, NASA Glenn Research Center Presenters: Valerie Lyons, NASA Glenn Research Center Michael Patterson, NASA Glenn Research Center Dianne Linne, NASA Glenn Research Center

90 Stanley Borowski, NASA Glenn Research Center Michael Meyer, NASA Glenn Research Center Lee Mason, NASA Glenn Research Center Concha Reid, NASA Glenn Research Center Wednesday, 30 July 2014 176-LP-18 Combustion Devices II Room 26 C Chaired by: D. KIRK, Florida Institute of Technology and J. RICCIUS, DLR - German Aerospace Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2014-3985 AIAA-2014-3986 AIAA-2014-3987 AIAA-2014-3988 AIAA-2014-3989 AIAA-2014-3990 AIAA-2014-3991 Comparison of Performance and An Experimental Investigation of a Near-wall Velocity Field Inner liner temperature variation Experimental Investigations of Investigation of Blanching behavior Thrust Performance of 70 N-class Stability Analyses for LOX/CH4 LOX/CH4 Torch Ignition System for Measurements of a Very Low caused deformation localisation a GO2/Kerosene Ejector Rocket of Cu-Ag-Zr alloy using oxidation- Hydrazine Thruster with Various Rocket Engines Propulsion Research Momentum Flux Transverse Jet effects in a multichannel model of Chamber for the RBCC Propulsion reduction cycles Characteristic Lengths A. French, F. Battista, V. Salvatore, M. L. Sanchez, R. Ellis, V. Dorado, A. D. Salazar, D. Forliti, Sierra Lobo, Inc., a generic LRE wall structure System K. Bubenheim, C. Wilhelmi, M. Holzapfel, J. Kim, H. Jung, J. Kim, Pukyong National Marini, Italian Aerospace Research Center Choudhuri, University of Texas, El Paso, Edwards AFB, CA; K. Kuzmich, N. Sedano, J. Riccius, German Aerospace Center S. Zhu, L. Tian, L. Xuan, X. Xu, Beihang Airbus, Munich, Germany; S. Fasoulas, University, Busan, South Korea (CIRA), Capua, Italy El Paso, TX E. Coy, Air Force Research Laboratory, (DLR), Lampoldshausen, Germany; Q. University, Beijing, China Institute of Space Systems, University of Edwards AFB, CA Wargnier, Supméca, Paris, France; W. Stuttgart, Stuttgart, Germany Bouajila, E. Zametaev, German Aerospace Center (DLR), Lampoldshausen, Germany Wednesday, 30 July 2014 177-LP-19 Propellant Storage and Management Room 3 Chaired by: V. AHUJA, CRAFT Tech and M. DEANS, NASA Glenn Research Ctr 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-3992 AIAA-2014-3993 AIAA-2014-3994 AIAA-2014-3995 AIAA-2014-3996 AIAA-2014-3997 Warm Pressurant Gas Effects on Inverted Outflow Ground Testing Phase Change in Cryogenic Upper Development of New Composite Effects of Curvature on Spacecraft Numerical & Experimental the Static Bubble Point Pressure for of Cryogenic Propellant Liquid Stage Tanks Propellant Tank for Satellites Propellant Management Surface Investigation of Cavitating Venturi Cryogenic LADs Acquisition Devices M. Konopka, P. Behruzi, Airbus, Bremen, I. Masuda, T. Masuoka, K. Mouri, H. Tension Screen Capillary Capability Geometry on LOX Flows J. Hartwig, D. Chato, J. McQuillen, NASA D. Chato, J. Hartwig, E. Rame, J. Germany; S. Schmitt, M. Dreyer, Kagawa, H. Ikeda, Japan Aerospace P. MacEachron, E. Alexander, N. Khan, M. M. Solmaz, B. Yazici, Scientific and Glenn Research Center, Cleveland, OH McQuillen, NASA Glenn Research Center, University of Bremen, Bremen, Germany Exploration Agency (JAXA), Tsukuba, Randeria, Yale University, New Haven, Technological Research Council of Turkey Cleveland, OH Japan; K. Yamada, IHI Corporation, CT; J. Braun, C. Stewart, Lockheed Martin (TÜBITAK), Ankara, Turkey Tomioka, Japan; et al. Corporation, Littleton, CO Wednesday, 30 July 2014 178-LP-20 Rocket Nozzles Room 4 Chaired by: S. BARSI, NASA 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-3998 AIAA-2014-3999 AIAA-2014-4000 AIAA-2014-4001 AIAA-2014-4002 AIAA-2014-4003 Flow Separation Response to Design of High Area Nozzle Influence of downstream Geometric Analysis of the Linear Flow Characteristics of Micro-Scale Comparison of Eigenmode Unsteady External Disturbances in Contours Using Circular Arcs unsteadiness on shock pattern in Expansion-Deflection Nozzle Planar Nozzles Extraction Techniques for Separated Dual Bell Nozzles K. Schomberg, G. Doig, J. Olsen, separated nozzle flows at Highly Overexpanded Flow D. Banuti, M. Grabe, K. Hannemann, Nozzle Flows E. Martelli, Second University of Naples, University of New South Wales, Sydney, A. Georges-Picot, A. Hadjadj, National Conditions German Aerospace Center (DLR), R. Larusson, N. Andersson, L. Eriksson, Aversa, Italy; B. Betti, F. Nasuti, University Australia Institute of Applied Sciences (INSA) of K. Schomberg, G. Doig, J. Olsen, Göttingen, Germany Chalmers University of Technology, of Rome “La Sapienza’’, Rome, Italy Rouen, Saint Etienne du Rouvray, France; University of New South Wales, Sydney, Göteborg, Sweden; J. Östlund, GKN J. Herpe, French Space Agency (CNES), Australia; A. Neely, University of New Aerospace Engine Systems, Trollhattan, 91 Paris, France South Wales, Canberra, Australia Sweden Wednesday, 30 July 2014 179-LP-21 Combustion Chamber Heat Transfer Room 5 Chaired by: M. NARAGHI, Manhattan College and M. PIZZARELLI, University of Rome 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs AIAA-2014-4004 AIAA-2014-4005 AIAA-2014-4006 AIAA-2014-4007 AIAA-2014-4008 AIAA-2014-4009 AIAA-2014-4010 Cooling Channel Analysis of a LOX/ Experimental Investigation on Ceramic Composites as Liners in Experimental Investigation of Experimental and Numerical Film Modeling of Fuel Film Cooling on Flowfield and Heat Transfer LCH4 Rocket Engine Demonstrator Methane in Transcritical Conditions LOX/Methane Ablative Thrust Liquid Methane Convection and Cooling Investigations in a GOX/ Chamber Hot Wall Characteristics in the LE-X Expander M. Pizzarelli, B. Betti, F. Nasuti, University R. Votta, F. Battista, A. Gianvito, A. Chambers Boiling in Rocket Engine Cooling Kerosene Rocket Combustion A. Himansu, E. Coy, V. Sankaran, S. Bleed Cycle Combustion Chamber of Rome “La Sapienza’’, Rome, Italy; Smoraldi, Italian Aerospace Research E. Besnard, A. Schmitz, D. Lee, California Channels Chamber Danczyk, Air Force Research Laboratory, H. Negishi, Y. Daimon, H. Kawashima, D. Ricci, P. Roncioni, F. Battista, Italian Center (CIRA), Capua, Italy; M. Pizzarelli, State University, Long Beach, CA A. Trejo, M. Galvan, A. Trujillo, A. G. Schlieben, C. Kirchberger, O. Haidn, Edwards AFB, CA Japan Aerospace Exploration Agency Aerospace Research Center (CIRA), Capua, G. Leccese, University of Rome “La Choudhuri, University of Texas, El Paso, Technical University of Munich, Munich, (JAXA), Tsukuba, Japan Italy; et al. Sapienza’’, Rome, Italy; et al. El Paso, TX Germany; C. Höglauer, B. Kniesner, O. Knab, Airbus, Munich, Germany Wednesday, 30 July 2014 180-ABPSI-10 Nozzles Room 6 Chaired by: L. LEAVITT, N A S A and J. FLAMM, NASA Langley Research Center 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-4011 AIAA-2014-4012 AIAA-2014-4013 AIAA-2014-4014 An Interactive Method of Sensitivity to inflow conditions of a Numerical Study of Three-Stream Steady and Unsteady Nozzle Characteristics Java Applet to dual-stream nozzle Nozzle Exhaust Flow From a Simulations Using the Conservation Design and Analyze Supersonic J. Verrière, Airbus, Toulouse, France; Simplified Model of a Turbofan Element and Solution Element Aircraft Nozzles V. Brunet, ONERA, Meudon, France; Nacelle Method T. Benson, NASA Glenn Research Center, C. Bourdeau, Airbus, Toulouse, France; J. Mern, R. Agarwal, Washington D. Friedlander, X. Wang, J. Connolly, G. Cleveland, OH S. Deck, ONERA, Meudon, France; C. University in St. Louis, St. Louis, MO Kopasakis, NASA Glenn Research Center, Gacherieu, Airbus, Toulouse, France Cleveland, OH Wednesday, 30 July 2014 181-SR-7 Solid Rocket Motor Modeling, Simulation and Analysis II Room 7 Chaired by: B. LEARY, JHU/Applied Physics Laboratory and W. RYAN, United Launch Alliance, LLC 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2014-4015 AIAA-2014-4016 AIAA-2014-4017 AIAA-2014-4018 AIAA-2014-4019 AIAA-2014-4020 Numerical Simulation of 3D Improved Mean Flow Solution Energy Steepened States of the Rotational Approximation of the Analytical model and numerical Analysis of Pressure Oscillations Unsteady Flowfield in Aft-Finocyl for Solid Rocket Motors with a Swirling Mean Flow in a Solid Taylor-Culick Profile for Rockets simulations for solid propellant during Ignition Transient and Solid Rocket Motor Naturally Developing Swirling Rocket Motor with Noncircular Grains using a Random Loose Packing Steady-State of an Overloaded A. Di Mascio, Centro Nazionale delle Motion A. Fist, J. Majdalani, Auburn University, J. Majdalani, E. Van Horn, Auburn approach VEGA First Stage Ricerche, Rome, Italy; E. Cavallini, B. J. Majdalani, A. Fist, Auburn University, Auburn, AL University, Auburn, AL D. Fedele, F. Ponti, R. Bertacin, University E. Cavallini, B. Favini, University of Rome Favini, Sapienza University of Rome, Auburn, AL of Bologna, Forlì, Italy “La Sapienza’’, Rome, Italy; A. Neri, ESA, Rome, Italy; A. Neri, ESA, Frascati Frascati, Italy 92 (Rome), Italy Wednesday, 30 July 2014 182-ST-1 Space Transportation Room 8 Chaired by: L. DANIEL, University of New Orleans and D. SAUVAGEAU, ATK Mission Systems 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-4021 AIAA-2014-4022 AIAA-2014-4023 AIAA-2014-4024 The Space Launch System Analysis and Adjoint Design Cutting More Than Metal: Breaking Research on the long-term Capabilities for Beyond Earth of Hypersonic Blunt Bodies The Development Cycle eccentricity drift of critical Missions T. Piskin, S. Eyi, Middle East Technical C. Singer, NASA Marshall Space Flight inclination orbits B. Donahue, The Boeing Company, University, Ankara, Turkey Center, Huntsville, AL J. Chen, W. Tan, State Key Laboratory of Huntsville, AL; K. Klaus, The Boeing Astronautic Dynamics, Xi’an, China; C. Li, Company, Houston, TX Xi’an Satellite Control Center, Xi’an, China Wednesday, 30 July 2014 183-EP-22 Advanced Concepts Room 9 Chaired by: J. GILLAND, Ohio Aerospace Institute and R. THOMAS 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-4025 AIAA-2014-4026 AIAA-2014-4027 AIAA-2014-4028 AIAA-2014-4029 Self-Consistent Cross-Field Plasma Experimental investigation of Quasi-one-dimensional code Collisionless electron cooling in a Anomalous Thrust Production from Motion in a Magnetic Null Thruster plasma plume characteristics for particle-in-cell simulation of magnetic nozzle an RF Test Device Measured on a M. Feldman, E. Choueiri, Princeton in applied radial electric field magnetic nozzle expansion J. Navarro, Technical University of Madrid, Low-Thrust Torsion Pendulum University, Princeton, NJ magnetic nozzle F. Ebersohn, J. Sheehan, B. Longmier, Madrid, Spain; M. Martinez-Sanchez, D. Brady, H. White, P. March, J. Lawrence, L. Ferrario, Technical University of Milan, University of Michigan, Ann Arbor, Ann Massachusetts Institute of Technology, F. Davies, NASA Johnson Space Center, Milan, Italy; J. Little, E. Choueiri, Princeton Arbor, MI; J. Shebalin, NASA Johnson Cambridge, MA; E. Ahedo, Charles III Houston, TX University, Princeton, NJ Space Center, Houston, TX University of Madrid, Leganés, Spain Author/Session Chair Index A. Shaaban, A., 82-TM-2 Araki, K., 137-HR-5, 167-HR-7 Berg, S., 53-PC-3, 108-APC-2 Brown, C., 173-PC-10 Chandler, A., 20-HR-1, 137-HR-5, 143-HR-6 Aanesland, A., 12-EP-2 Araki, S., 131-EP-18 Berger, M., 12-EP-2 Brown, D., 41-EP-6, 100-EP-14, 120-EP-16, 153-EP- Chandrashekhar, M., 22-EC-1 Abdalwahab, M., 173-PC-10 Aretskin-Hariton, E., 46-GTE-8 Bertacin, R., 181-SR-7 19, 164-EP-24 Chang, C., 15-GTE-1 AbdelLatif, O., 110-TM-3 Arkun, U., 79-HR-3 Besnard, E., 179-LP-21 Brown, G., 78-APS-2 Chap, A., 43-NFF-2, 51-EC-2 AbdelMaksoud, W., 82-TM-2 Armold, D., 107-HR-4 Bettella, A., 107-HR-4 Bruckner, R., 162-GTE-21 Chaparro, J., 99-ITAR-2 Abdollahzadeh, M., 138-APC-3 Armstrong, M., 33-ABPSI-1/GTE-4 Betti, B., 49-HR-2, 90-LP-9, 147-LP-15, 178-LP-20, Brundage, A., 160-PC-11 Chapek, R., 85-PC-6 Abdulrahman, A., 85-PC-6 Arrington, L., 31-LP-3 179-LP-21 Brunet, V., 180-ABPSI-10 Chapman, J., 162-GTE-21 Abu-Kabsha, A., 170-TM-4 Arrowood, R., 61-EDU-2 Bettrich, V., 16-GTE-2 Bubenheim, K., 176-LP-18 Charles, P., 21-APS-1 Abulaban, O., 173-PC-10 Asipauskas, M., 56-LP-5 Biaggi-Labiosa, A., 161-GTE-20 Bui, T., 168-APC-4 Chase, R., 80-APC-1 Achawangkul, Y., 170-TM-4 Aso, S., 137-HR-5, 167-HR-7 Bialy, E., 4-PSTR-1, 52-TES-1, 82-TM-2 Buntain, N., 99-ITAR-2 Chato, D., 177-LP-19 Acosta, W., 45-GTE-7 Atalayer, C., 59-ABPSI-2 Bianchi, D., 49-HR-2, 90-LP-9 Burchett, J., 119-ECS-1 Chatterjee, S., 15-GTE-1 Acosta-Zamora, A., 146-HSABP-6 Attaway, S., 160-PC-11 Biao, L., 19-HSABP-1 Burke, L., 74-NFF-3, 101-EP-15, 108-APC-2, 158- Chehroudi, B., 54-PC-4 Adamovsky, G., 161-GTE-20 Attia, A., 110-TM-3 Bielozer, M., 148-LP-16 EP-20 Chen, H., 92-ABPSI-3/GTE-13 Afify, M., 170-TM-4 Auslender, A., 19-HSABP-1 Bindl, S., 59-ABPSI-2 Burr, J., 173-PC-10 Chen, J., 104-GTE-15/ABPSI-4, 182-ST-1 Agarwal, R., 180-ABPSI-10 Austin, B., 99-LP-11 Blachowski, T., 119-ECS-1 Burrus, D., 75-GTE-10 Chen, L., 161-GTE-20 Agresta, A., 103-GTE-14/PC-7 Axdahl, E., 106-HSABP-5 Black, D., 187-ITAR-1 Burt, J., 136-HSABP-7/ABPSI-8 Chen, T., 172-SCP-3 Agui, J., 56-LP-5 Bade Shrestha, S., 88-HSABP-3 Black, R., 46-GTE-8 Bushman, S., 89-LP-8 Chen, Y., 49-HR-2, 172-SCP-3 Aguilera Munoz, C., 166-HSABP-10 Baglini, J., 119-ECS-1, 152-ECS-2 Blackwelder, M., 33-ABPSI-1/GTE-4 Butler, B., 16-GTE-2 Chenkai, Z., 104-GTE-15/ABPSI-4 Ahedo, E., 29-EP-1, 41-EP-6, 95-EP-13, 131-EP-18, Bailey, S., 22-EC-1 Blakely, J., 41-EP-6 Cabrera, L., 4-PSTR-1 Chi, H., 19-HSABP-1 183-EP-22 Baisden, A., 22-EC-1 Blanchard, C., 49-HR-2 Cadou, C., 84-PC-5 Chianese, S., 57-LP-6 Ahmed, S., 173-PC-10 Bakhle, M., 104-GTE-15/ABPSI-4 Blodgett, K., 117-ABPSI-6, 150-ABPSI-9 Cagan, L., 45-GTE-7 Chicatelli, A., 77-GTE-12 Ahuja, V., 177-LP-19 Ballato, J., 187-ITAR-1 Bobula, G., 17-GTE-3 Caillat, T., 81-EC-3 Cho, D., 48-HSABP-2/GTE-9

93 Aigner, M., 26-PC-2, 160-PC-11 Bane, S., 33-ABPSI-1/GTE-4 Bodruzzaman, M., 46-GTE-8 Cain, G., 58-LP-7 Cho, S., 13-EP-3 Ajmani, K., 45-GTE-7, 85-PC-6 Banuti, D., 54-PC-4, 115-LP-13, 178-LP-20 Boiron, A., 143-HR-6, 167-HR-7 Califf, C., 135-GTE-19 Choi, B., 78-APS-2 Akashi, N., 47-EP-5 Baran, A., 49-HR-2 Bolotin, G., 169-EC-5 Cameron, J., 16-GTE-2, 44-GTE-6, 76-GTE-11 Choi, G., 20-HR-1 Akyuzlu, K., 102-NFF-4 Barato, F., 107-HR-4 Borowski, S., 14-NFF-1, 74-NFF-3 Cannella, M., 114-LP-12 Choi, J., 48-HSABP-2/GTE-9, 106-HSABP-5, Albright, J., 58-LP-7 Barber, T., 90-LP-9 Bosi, F., 4-PSTR-1 Cantwell, B., 137-HR-5, 143-HR-6 157-HSABP-8/PC-9 Alexander, E., 177-LP-19 Barda, J., 173-PC-10 Bossaert, A., 30-LP-2 Cao, M., 17-GTE-3, 55-GTE-5 Choi, M., 13-EP-3, 110-TM-3, 128-ITAR-3, 170-TM-4 Alexeenko, A., 138-APC-3 Barragan, J., 99-ITAR-2 Bouajila, W., 176-LP-18 Capece, V., 16-GTE-2 Choi, S., 53-PC-3 Ali, H., 51-EC-2 Barry, M., 150-ABPSI-9 Bourdeau, C., 180-ABPSI-10 Cardiff, E., 138-APC-3 Chou, T., 49-HR-2 Alkali, M., 4-PSTR-1 Barsi, S., 178-LP-20 Bowman, C., 21-APS-1 Carmicino, C., 49-HR-2 Choudhuri, A., 4-PSTR-1, 99-ITAR-2, 115-LP-13, Allen, D., 21-APS-1, 78-APS-2 Bartkowiak, B., 58-LP-7 Boyd, I., 13-EP-3 Carpenter, C., 99-ITAR-2, 134-GTE-18 146-HSABP-6, 176-LP-18, 179-LP-21 Alliot, P., 30-LP-2, 116-LP-14 Bartolotta, P., 113-HSABP-4 Boye, L., 160-PC-11 Carranza, S., 161-GTE-20 Choueiri, E., 41-EP-6, 130-EP-17, 159-EP-21, 183- Aloyo, K., 92-ABPSI-3/GTE-13 Batterson, J., 32-LP-4, 34-SR-1 Boyer, J., 107-HR-4 Casalino, L., 92-ABPSI-3/GTE-13, 167-HR-7 EP-22 Alquaity, A., 173-PC-10 Battista, F., 176-LP-18, 179-LP-21 Bozak, R., 105-GTE-16/ABPSI-5 Cassenti, B., 74-NFF-3 Christhilf, D., 92-ABPSI-3/GTE-13 Altmann, C., 159-EP-21 Baumeister, J., 89-LP-8 Brady, B., 107-HR-4, 167-HR-7 Castro, J., 166-HSABP-10 Christie, R., 56-LP-5 Ameri, A., 44-GTE-6, 134-GTE-18, 163-GTE-22 Beach, R., 132-APS-3 Brady, D., 183-EP-22 Castrogiovanni, A., 129-ITAR-4 Chu, M., 4-PSTR-1 Anand, M., 85-PC-6 Beach, T., 104-GTE-15/ABPSI-4 Brainerd, J., 168-APC-4 Catori, C., 45-GTE-7 Chuck, C., 111-ABPSI-7 Anderson, B., 117-ABPSI-6 Bedard, M., 84-PC-5 Braun, J., 177-LP-19 Cavallini, E., 34-SR-1, 71-SR-5, 118-SR-4, 181-SR-7 Chung, G., 162-GTE-21 Anderson, D., 62-EP-8 Behbahani, A., 46-GTE-8, 77-GTE-12, 172-SCP-3 Braun, R., 19-HSABP-1, 51-EC-2 Celik, M., 4-PSTR-1 Chupp, R., 60-SCP-1 Anderson, J., 100-EP-14 Behruzi, P., 177-LP-19 Braunscheidel, E., 76-GTE-11 Cerpa, R., 103-GTE-14/PC-7 Cichocki, F., 131-EP-18 Anderson, R., 15-GTE-1, 75-GTE-10 Belair, M., 14-NFF-1 Brechtel, C., 143-HR-6 Chabert, P., 12-EP-2 Ciezki, H., 34-SR-1, 116-LP-14 Anderson, W., 15-GTE-1, 32-LP-4, 84-PC-5, 91-LP-10, Belvin, A., 102-NFF-4 Brehm, S., 59-ABPSI-2 Chahine, M., 173-PC-10 Claﬂin, S., 137-HR-5 110-TM-3, 112-PC-8 Bennett, W., 50-EST-1 Breisacher, K., 45-GTE-7 Chaineray, G., 71-SR-5 Clark, R., 88-HSABP-3 Andersson, N., 178-LP-20 Bennewitz, J., 91-LP-10 Brendel, J., 114-LP-12 Chan, S., 103-GTE-14/PC-7 Coats, D., 118-SR-4 Andriani, R., 103-GTE-14/PC-7 Bennington, M., 16-GTE-2 Briggs, M., 139-EC-4 Chan, T., 169-EC-5 Cofer, A., 138-APC-3 Anthoine, J., 167-HR-7 Benson, T., 180-ABPSI-10 Broadway, J., 102-NFF-4 Chan, W., 165-HSABP-9 Coffman, C., 94-EP-12 Aoyagi, J., 58-LP-7 Berdoyes, M., 93-SR-3 Brouillette, M., 19-HSABP-1 Chan, Y., 172-SCP-3 Coil, M., 25-PC-1 Author/Session Chair Index Cole, A., 55-GTE-5 Deans, M., 31-LP-3, 149-LP-17, 177-LP-19 Duquerrois, A., 22-EC-1 Feldman, T., 112-PC-8 Gabriel, S., 18-EP-9, 36-EP-4 Coleman, B., 53-PC-3 Deck, S., 180-ABPSI-10 Duzel, U., 93-SR-3 Feller, J., 56-LP-5 Gacherieu, C., 180-ABPSI-10 Coletti, M., 18-EP-9, 36-EP-4 Dehouve, J., 114-LP-12 Dynys, F., 81-EC-3 Ferguson, D., 103-GTE-14/PC-7 Gad, A., 20-HR-1 Collard, T., 159-EP-21 Deininger, W., 101-EP-15, 158-EP-20 Eaton, A., 187-ITAR-1 Ferrario, L., 183-EP-22 Gady, S., 101-EP-15 Collins, J., 169-EC-5 DeKorver, V., 30-LP-2 Eberle, C., 26-PC-2 Fetta, G., 138-APC-3 Gaio, T., 30-LP-2 Collins, S., 158-EP-20 Delalu, H., 4-PSTR-1 Ebersohn, F., 183-EP-22 Fiebig, M., 114-LP-12 Gallimore, A., 41-EP-6, 100-EP-14, 120-EP-16 Colozza, A., 21-APS-1, 109-EPOL-1/ESYS-1 Delange, J., 30-LP-2 Echekki, T., 165-HSABP-9 Figus, C., 167-HR-7 Gallimore, S., 129-ITAR-4 Connell, T., 25-PC-1 Delgado, J., 62-EP-8 Ecker, T., 105-GTE-16/ABPSI-5 Filosa, A., 160-PC-11 Galvan, M., 179-LP-21 Connolly, J., 92-ABPSI-3/GTE-13, 180-ABPSI-10 Delot, A., 59-ABPSI-2 Edeline, E., 30-LP-2 Fink, L., 117-ABPSI-6 Gamma, F., 103-GTE-14/PC-7 Conversano, R., 153-EP-19 Delventhal, R., 58-LP-7 Edwards, J., 165-HSABP-9 Finkbeiner, J., 60-SCP-1 Gang, L., 88-HSABP-3 Coogan, S., 143-HR-6 Demange, J., 60-SCP-1 Eichele, P., 44-GTE-6 Firdosy, S., 81-EC-3 Gang, Z., 57-LP-6 Coote, D., 102-NFF-4, 148-LP-16 Demko, A., 93-SR-3 Eisenmann, S., 134-GTE-18 Fist, A., 181-SR-7 Garg, S., 77-GTE-12 Corey, R., 100-EP-14 Denney, R., 22-EC-1, 162-GTE-21 Ekkad, S., 15-GTE-1 Fittje, J., 14-NFF-1, 108-APC-2 Garner, C., 62-EP-8 Corrigan, A., 105-GTE-16/ABPSI-5, 157-HSABP-8/ Dennis, J., 90-LP-9 Eklund, D., 136-HSABP-7/ABPSI-8 Flamm, J., 150-ABPSI-9, 180-ABPSI-10 Garverick, S., 78-APS-2 PC-9 Desai, R., 47-EP-5 Elam, K., 161-GTE-20 Fleeman, E., 35-EDU-1 Gatto, C., 58-LP-7, 116-LP-14, 142-SCP-2, 143-HR-6 Costa, J., 46-GTE-8 Desain, J., 107-HR-4, 167-HR-7 ElHarriry, G., 110-TM-3 Flegel, A., 163-GTE-22 Gawahara, K., 157-HSABP-8/PC-9 Coy, E., 176-LP-18, 179-LP-21 Dever, T., 78-APS-2, 132-APS-3 Elliott, T., 71-SR-5 Fleurial, J., 81-EC-3 Gejji, R., 15-GTE-1 Cranford, J., 91-LP-10 Di, C., 106-HSABP-5 Ellis, R., 115-LP-13, 176-LP-18 Florea, R., 76-GTE-11 George, P., 132-APS-3 Creasy, J., 21-APS-1 Di Cosmo, A., 151-SR-6 Emrich, W., 102-NFF-4 Florenz, R., 120-EP-16 Georges-Picot, A., 178-LP-20 Crocker, A., 30-LP-2 Di Domenico, M., 160-PC-11 Enger, S., 101-EP-15, 158-EP-20 Floyd, B., 161-GTE-20 Gerlinger, P., 26-PC-2 Crofton, M., 12-EP-2, 13-EP-3, 18-EP-9, 72-EP-10 Di Mascio, A., 181-SR-7 Erdmann, T., 75-GTE-10 Forde, S., 99-ITAR-2 Gerrish, H., 102-NFF-4 Crowder, W., 118-SR-4 Di Matteo, F., 147-LP-15 Eriguchi, K., 131-EP-18 Forliti, D., 32-LP-4, 115-LP-13, 176-LP-18 Ghiasi, Z., 26-PC-2

94 Crowley, J., 143-HR-6 Di Stefano, S., 109-EPOL-1/ESYS-1, 169-EC-5 Eriksson, L., 178-LP-20 Foster, J., 12-EP-2, 95-EP-13, 141-EP-23 Gianvito, A., 179-LP-21 Csank, J., 172-SCP-3 Di Trapani, C., 151-SR-6 Ertmer, K., 30-LP-2 Foster, W., 118-SR-4 Gibson, M., 21-APS-1 Culley, D., 46-GTE-8 Diallo, A., 41-EP-6 Escobar Anton, D., 41-EP-6 Fouad, M., 82-TM-2 Giel, P., 163-GTE-22 Cuppoletti, D., 105-GTE-16/ABPSI-5 Diamant, K., 100-EP-14 Esmaeili, S., 4-PSTR-1 Foutch, D., 16-GTE-2 Giel, T., 147-LP-15, 172-SCP-3 Curriston, D., 44-GTE-6 Dinelli, C., 158-EP-20 Eussen, B., 170-TM-4 Fralick, G., 161-GTE-20, 172-SCP-3 Gieras, J., 52-TES-1 Dai, Z., 75-GTE-10 Ding, M., 126-NFF-5 Evans, B., 107-HR-4, 137-HR-5, 143-HR-6, 167-HR-7 Frank, J., 132-APS-3 Giliberti, F., 151-SR-6 Daimon, Y., 179-LP-21 Doering, K., 30-LP-2 Evans, J., 43-NFF-2 Frankel, A., 148-LP-16 Gilland, J., 183-EP-22 Dam, B., 15-GTE-1 Doig, G., 178-LP-20 Everline, C., 109-EPOL-1/ESYS-1, 169-EC-5 Frederick, R., 35-EDU-1, 61-EDU-2, 91-LP-10 Gilloux, T., 4-PSTR-1 Danczyk, S., 115-LP-13, 179-LP-21 Donahue, B., 182-ST-1 Eyi, S., 4-PSTR-1, 93-SR-3, 182-ST-1 Freeman, R., 58-LP-7, 109-EPOL-1/ESYS-1 Gilpin, M., 132-APS-3 Dang, A., 118-SR-4 Donbar, J., 166-HSABP-10 Ezawa, Y., 167-HR-7 French, A., 101-EP-15, 176-LP-18 Ginty, C., 56-LP-5 Daniel, L., 182-ST-1 Donnan, R., 61-EDU-2 Fabanich, W., 110-TM-3 Frezzotti, M., 32-LP-4 Giuliani, J., 104-GTE-15/ABPSI-4 Daniels, C., 60-SCP-1 Dooley, S., 25-PC-1, 85-PC-6 Faber, J., 161-GTE-20 Friedlander, D., 92-ABPSI-3/GTE-13, 180-ABPSI-10 Glascock, M., 108-APC-2 Dankanich, J., 12-EP-2, 62-EP-8, 101-EP-15, 158- Doorenbos, Z., 152-ECS-2 Fabignon, Y., 71-SR-5 Friedrichs, J., 59-ABPSI-2, 150-ABPSI-9 Gloyer, P., 91-LP-10 EP-20 Dorado, V., 115-LP-13, 176-LP-18 Falck, R., 101-EP-15 Frieman, J., 100-EP-14 Godar, T., 72-EP-10 Dankongkakul, B., 131-EP-18 Drennan, S., 75-GTE-10 Fan, Y., 106-HSABP-5 Friz, P., 108-APC-2 Goebel, D., 41-EP-6, 62-EP-8, 130-EP-17, 153-EP-19 Dantonio, J., 76-GTE-11 Dreyer, M., 177-LP-19 Fang, E., 160-PC-11 Frollani, D., 18-EP-9, 36-EP-4 Goeke, J., 75-GTE-10 Darkwa, J., 82-TM-2, 170-TM-4 Driscoll, R., 88-HSABP-3 Faooq, A., 173-PC-10 Fromm, C., 147-LP-15 Goff, D., 78-APS-2 Darwich, C., 4-PSTR-1 Drozda, T., 106-HSABP-5 Farkas, N., 152-ECS-2 Fu, S., 92-ABPSI-3/GTE-13 Gogineni, S., 44-GTE-6 Das, M., 15-GTE-1 Dryer, F., 25-PC-1 Farooq, A., 173-PC-10 Fuchigami, K., 13-EP-3 Gokulakrishnan, P., 85-PC-6 David, N., 30-LP-2 Du, D., 170-TM-4 Farouk, T., 85-PC-6 Fujita, R., 62-EP-8 Goldin, N., 109-EPOL-1/ESYS-1 Davidson, A., 62-EP-8 Du, M., 22-EC-1 Fasoulas, S., 176-LP-18 Fuller, C., 85-PC-6 Gollahalli, S., 52-TES-1 Davies, F., 183-EP-22 Du, X., 77-GTE-12 Favini, B., 118-SR-4, 181-SR-7 Fuller, T., 84-PC-5 Gomez Ramirez, D., 15-GTE-1 Davis, R., 119-ECS-1 Duchemin, O., 95-EP-13 Fearn, H., 126-NFF-5 Funaki, I., 4-PSTR-1, 29-EP-1, 48-HSABP-2/GTE-9, Gonthier, K., 119-ECS-1 Davitian, J., 107-HR-4 Dudzinski, L., 21-APS-1 Fedele, D., 181-SR-7 95-EP-13, 131-EP-18, 157-HSABP-8/ Gontmacher, P., 62-EP-8 Davoudzadeh, F., 115-LP-13 Dunlap, P., 60-SCP-1 Feiz, H., 45-GTE-7 PC-9, 168-APC-4 Gonyea, K., 19-HSABP-1 Daykin-Iliopoulos, A., 47-EP-5 Dunn, S., 99-ITAR-2 Feldman, M., 183-EP-22 Funami, Y., 20-HR-1 Goodman, J., 61-EDU-2 Author/Session Chair Index Gordon, S., 61-EDU-2 Hartwig, J., 177-LP-19 Hollander, S., 49-HR-2 Ishikawa, Y., 30-LP-2 Kameda, M., 117-ABPSI-6 Goyer, S., 84-PC-5 Harvazinski, M., 32-LP-4, 91-LP-10 Holzapfel, M., 176-LP-18 Ishizaki, S., 30-LP-2 Kamhawi, H., 13-EP-3, 41-EP-6, 62-EP-8, 100-EP-14, Grabe, M., 178-LP-20 Hashimoto, T., 168-APC-4 Homan-Cruz, G., 53-PC-3 Ito, H., 170-TM-4 120-EP-16, 153-EP-19, 158-EP-20 Graham, S., 89-LP-8 Hassan, H., 19-HSABP-1 Honda, K., 13-EP-3 Ito, S., 29-EP-1 Kamimura, T., 62-EP-8 Grayson, G., 177-LP-19 Hassan, I., 110-TM-3 Hopkins, M., 120-EP-16 Iwasaki, Y., 51-EC-2 Kan, B., 90-LP-9 Grayson, K., 143-HR-6 Hassan, M., 4-PSTR-1, 52-TES-1 Horisawa, H., 4-PSTR-1, 36-EP-4, 47-EP-5, 94-EP-12 Iyidiker, C., 118-SR-4 Kaneshige, M., 160-PC-11 Greatrix, D., 34-SR-1, 107-HR-4 Hathaway, M., 76-GTE-11 Hosokawa, H., 47-EP-5 Jaberi, F., 26-PC-2 Kapusta, M., 105-GTE-16/ABPSI-5 Green, M., 129-ITAR-4 Hause, M., 94-EP-12 Hossain, A., 146-HSABP-6 Jackson, B., 47-EP-5 Karabeyoglu, A., 79-HR-3, 137-HR-5, 143-HR-6 Greer, L., 161-GTE-20 Hawkett, B., 94-EP-12 Hourani, N., 173-PC-10 Jacob, E., 32-LP-4, 91-LP-10 Kartuzova, O., 56-LP-5 Grillenbeck, A., 30-LP-2 Hawkins, T., 187-ITAR-1 Houts, M., 102-NFF-4 Jacob, G., 4-PSTR-1 Kasahara, J., 48-HSABP-2/GTE-9, 157-HSABP-8/ Grondein, P., 12-EP-2 Hayton, B., 126-NFF-5 Howard, R., 16-GTE-2 Jacobs, S., 173-PC-10 PC-9 Gross, J., 75-GTE-10 He, Z., 15-GTE-1 Hruby, V., 158-EP-20 Jacobson, D., 4-PSTR-1, 101-EP-15 Kassemi, M., 56-LP-5 Grosse, M., 107-HR-4 Heeb, N., 105-GTE-16/ABPSI-5 Hu, C., 108-APC-2 Jaffa, N., 16-GTE-2 Kastengren, A., 115-LP-13 Groven, L., 152-ECS-2 Heil, M., 11-LP-1 Hu, J., 104-GTE-15/ABPSI-4 Jagannath, R., 33-ABPSI-1/GTE-4 Kato, Y., 157-HSABP-8/PC-9 Guan, H., 152-ECS-2 Heindel, T., 115-LP-13 Hu, L., 51-EC-2 Jahanbakhsh, S., 4-PSTR-1 Katz, I., 153-EP-19 Gueyfﬁer, D., 71-SR-5 Heister, S., 49-HR-2, 53-PC-3, 57-LP-6, 90-LP-9, Huang, C., 15-GTE-1, 81-EC-3, 112-PC-8 Jain, N., 94-EP-12 Kawabata, S., 58-LP-7 Guinet, C., 16-GTE-2 138-APC-3, 157-HSABP-8/PC-9, 170-TM-4 Huang, J., 142-SCP-2 James, K., 150-ABPSI-9 Kawasaki, A., 4-PSTR-1, 95-EP-13 Gümmer, V., 16-GTE-2 Henderson, B., 105-GTE-16/ABPSI-5 Huang, W., 47-EP-5, 41-EP-6, 100-EP-14, 120-EP-16, Jaworske, D., 109-EPOL-1/ESYS-1 Kawashima, H., 179-LP-21 Guo, T., 77-GTE-12, 162-GTE-21 Henderson, E., 80-APC-1 153-EP-19 Jemcov, A., 44-GTE-6 Kawashima, R., 73-EP-11 Gupta, A., 55-GTE-5 Hendricks, E., 17-GTE-3 Huang, Z., 147-LP-15 Jenista, C., 61-EDU-2 Keidar, M., 158-EP-20 Gutmark, E., 88-HSABP-3, 105-GTE-16/ABPSI-5 Hepp, A., 22-EC-1, 109-EPOL-1/ESYS-1 Huanxian, B., 136-HSABP-7/ABPSI-8 Jens, E., 137-HR-5 Keller, S., 41-EP-6 Haag, T., 100-EP-14, 120-EP-16 Herbertz, A., 147-LP-15 Hubbard, G., 137-HR-5 Jensen, D., 17-GTE-3 Kestner, B., 162-GTE-21

95 Haas, F., 25-PC-1, 85-PC-6 Herman, D., 72-EP-10, 101-EP-15, 153-EP-19, Hudgins, J., 36-EP-4 Jeong, C., 112-PC-8 Key, N., 104-GTE-15/ABPSI-4 Haberbusch, M., 169-EC-5 164-EP-24 Hudson, J., 158-EP-20 Jianchen, W., 106-HSABP-5, 166-HSABP-10 Khaled, F., 173-PC-10 Hack, K., 101-EP-15 Hermanson, J., 166-HSABP-10 Huffman, M., 45-GTE-7 Jin, L., 76-GTE-11 Khalil, E., 4-PSTR-1, 52-TES-1, 82-TM-2, 109-EPOL- Hackel, J., 101-EP-15 Hernandez, F., 58-LP-7 Hughes, C., 150-ABPSI-9 Jinli, H., 57-LP-6 1/ESYS-1, 110-TM-3, 170-TM-4 Hadjadj, A., 178-LP-20 Hernandez, H., 99-ITAR-2 Hughes, M., 17-GTE-3 John, J., 108-APC-2, 118-SR-4 Khan, J., 33-ABPSI-1/GTE-4 Haefner, K., 126-NFF-5 Herpe, J., 114-LP-12, 178-LP-20 Huijun, T., 136-HSABP-7/ABPSI-8 Johnson, I., 4-PSTR-1, 95-EP-13 Khan, M., 103-GTE-14/PC-7 Hagenmaier, M., 136-HSABP-7/ABPSI-8 Herrick, G., 104-GTE-15/ABPSI-4 Hunt, S., 35-EDU-1, 170-TM-4 Johnson, W., 56-LP-5 Khan, N., 177-LP-19 Haidn, O., 53-PC-3, 115-LP-13, 179-LP-21 Herring, N., 33-ABPSI-1/GTE-4 Hunter, G., 161-GTE-20, 172-SCP-3 Jolly, B., 102-NFF-4 Khandelwal, B., 4-PSTR-1 Haines, J., 132-APS-3 Herscovitz, J., 62-EP-8, 108-APC-2 Huo, H., 15-GTE-1 Jones, D., 168-APC-4 Khavaran, A., 105-GTE-16/ABPSI-5 Hall, S., 120-EP-16 Hester, S., 32-LP-4, 112-PC-8 Hupfer, A., 134-GTE-18 Jones, S., 17-GTE-3, 135-GTE-19 Khayms, V., 73-EP-11, 100-EP-14 Halliwell, I., 133-GTE-17 Hexia, H., 136-HSABP-7/ABPSI-8 Hurlbert, E., 58-LP-7 Jorgenson, P., 135-GTE-19 Khimeche, G., 167-HR-7 Hallum, W., 112-PC-8 Hickman, H., 148-LP-16 Hürttlen, J., 116-LP-14 Jorns, B., 73-EP-11, 130-EP-17, 153-EP-19 Kibbey, T., 187-ITAR-1 Hamley, J., 21-APS-1 Hickman, R., 102-NFF-4 Hwang, W., 48-HSABP-2/GTE-9 Joshi, D., 48-HSABP-2/GTE-9 Kiel, B., 85-PC-6, 105-GTE-16/ABPSI-5 Han, S., 106-HSABP-5 Hicks, Y., 15-GTE-1, 75-GTE-10 Iannetti, A., 75-GTE-10 Joshi, N., 15-GTE-1 Kikuchi, T., 18-EP-9, 109-EPOL-1/ESYS-1 Hannemann, K., 54-PC-4, 115-LP-13, 178-LP-20 Himansu, A., 179-LP-21 Ibrahim, A., 4-PSTR-1, 52-TES-1, 173-PC-10 Josyula, E., 136-HSABP-7/ABPSI-8 Kim, D., 57-LP-6, 187-ITAR-1 Hansen, J., 72-ITAR-1 Himeno, T., 78-APS-2 Ibrahim, M., 55-GTE-5 Joucla, L., 4-PSTR-1 Kim, J., 48-HSABP-2/GTE-9, 176-LP-18 Haque, S., 158-EP-20 Hine, A., 120-EP-16 Ihme, M., 165-HSABP-9 Jouda, A., 170-TM-4 Kim, K., 106-HSABP-5 Harada, N., 18-EP-9, 109-EPOL-1/ESYS-1 Hinerman, T., 32-LP-4 Iihara, S., 13-EP-3 Joyner, C., 14-NFF-1 Kim, S., 187-ITAR-1 Hardi, J., 112-PC-8 Hirota, M., 170-TM-4 Iizuka, T., 58-LP-7 Ju, Y., 25-PC-1, 85-PC-6 Kim, T., 48-HSABP-2/GTE-9, 102-NFF-4, Hari, P., 22-EC-1 Hirt, S., 117-ABPSI-6 Ikeda, H., 177-LP-19 Jung, H., 176-LP-18 157-HSABP-8/PC-9 Harrington, S., 114-LP-12 Hitt, M., 35-EDU-1, 61-EDU-2 Ingenito, A., 103-GTE-14/PC-7 Kächele, T., 59-ABPSI-2 Kim, Y., 15-GTE-1 Harris, J., 22-EC-1 Hobbs, M., 160-PC-11 Ingle, M., 99-ITAR-2 Kagawa, H., 56-LP-5, 177-LP-19 Kimoto, K., 30-LP-2 Harris, M., 45-GTE-7 Hofer, R., 41-EP-6, 73-EP-11, 100-EP-14, 120-EP-16, Inkley, N., 167-HR-7 Kagota, T., 120-EP-16 Kinefuchi, K., 36-EP-4 Harsh, K., 46-GTE-8 153-EP-19 Inoue, F., 36-EP-4 Kailasanath, K., 105-GTE-16/ABPSI-5, King, D., 100-EP-14 Hartenstine, J., 110-TM-3 Höglauer, C., 179-LP-21 Irannejad, A., 26-PC-2 157-HSABP-8/PC-9 King, L., 47-EP-5, 94-EP-12, 120-EP-16 Hartfield, R., 44-GTE-6, 146-HSABP-6 Hojnicki, J., 101-EP-15 Ishida, S., 51-EC-2 Kamath, U., 58-LP-7 King, S., 100-EP-14 Author/Session Chair Index Kirchberger, C., 58-LP-7, 179-LP-21 Kuwahara, T., 54-PC-4 Li, B., 81-EC-3 Mackey, J., 81-EC-3, 161-GTE-20 McClure, P., 21-APS-1 Kirk, D., 176-LP-18 Kuzmich, K., 176-LP-18 Li, C., 182-ST-1 Madhanabharatam, B., 143-HR-6 McCown, K., 53-PC-3 Kirtley, D., 43-NFF-2 Labarthe, E., 4-PSTR-1 Li, J., 4-PSTR-1 Magee, T., 117-ABPSI-6 McCurdy, D., 74-NFF-3 Kitaide, Y., 51-EC-2 Lacaze, G., 106-HSABP-5 Li, W., 165-HSABP-9 Mahalingam, S., 72-EP-10 McDaniel, J., 106-HSABP-5 Klassen, M., 85-PC-6 Ladeinde, F., 165-HSABP-9 Lianbo, Z., 54-PC-4 Mahpour, A., 169-EC-5 McDonell, V., 173-PC-10 Klaus, K., 182-ST-1 Lafleur, T., 12-EP-2 Liang, R., 100-EP-14 Mair, M., 134-GTE-18 McGrath, D., 40-SR-2, 151-SR-6 Klein, A., 21-APS-1, 22-EC-1 Lai, A., 49-HR-2 Lightfoot, M., 115-LP-13 Majdalani, J., 20-HR-1, 34-SR-1, 71-SR-5, 90-LP-9, McGuire, M., 101-EP-15, 108-APC-2 Kmiec, T., 30-LP-2 Laker, T., 128-ITAR-3 Lim, D., 35-EDU-1 118-SR-4, 181-SR-7 McKay, H., 58-LP-7 Knab, O., 179-LP-21 Lancellotti, V., 4-PSTR-1 Lim, J., 93-SR-3 Majerus, S., 78-APS-2 McKechnie, T., 99-ITAR-2 Knezevici, D., 135-GTE-19 Landis, G., 21-APS-1, 108-APC-2, 109-EPOL-1/ Lin, B., 106-HSABP-5 Makel, D., 161-GTE-20 McKnight, B., 107-HR-4 Kniesner, B., 179-LP-21 ESYS-1 Lin, E., 166-HSABP-10 Malo-Molina, F., 48-HSABP-2/GTE-9, 142-SCP-2, McLaughlin, D., 105-GTE-16/ABPSI-5 Kobald, M., 79-HR-3, 167-HR-7 Langendorf, S., 120-EP-16 Lin, J., 49-HR-2 165-HSABP-9 McLean, C., 31-LP-3 Kobayashi, H., 51-EC-2 Lariviere, B., 30-LP-2 Linassier, G., 84-PC-5 Manente, M., 4-PSTR-1 McManamen, J., 58-LP-7 Koizumi, H., 73-EP-11, 131-EP-18 Larusson, R., 178-LP-20 Lineberry, D., 91-LP-10 Manfletti, C., 116-LP-14, 147-LP-15 McNatt, J., 22-EC-1 Kojima, J., 31-LP-3 Laskhmanan, V., 15-GTE-1 Litt, J., 77-GTE-12, 161-GTE-20, 162-GTE-21 Manfredi, P., 30-LP-2, 114-LP-12 Mcnelis, A., 132-APS-3 Kokogiannakis, G., 170-TM-4 Lauer, D., 159-EP-21 Little, J., 159-EP-21, 183-EP-22 Manickavelu, T., 34-SR-1 McNelis, A., 132-APS-3 Kolmanovsky, I., 172-SCP-3 Lavelle, T., 14-NFF-1, 162-GTE-21 Liu, C., 19-HSABP-1 Manzella, D., 101-EP-15, 158-EP-20 McNelis, N., 132-APS-3 Kolosa, D., 158-EP-20 Lawrence, J., 183-EP-22 Liu, H., 103-GTE-14/PC-7, 172-SCP-3 Mao, Z., 104-GTE-15/ABPSI-4 McQuillen, J., 177-LP-19 Komperda, J., 26-PC-2 Le, N., 136-HSABP-7/ABPSI-8 Liu, J., 105-GTE-16/ABPSI-5 March, P., 183-EP-22 Meadows, R., 30-LP-2 Komurasaki, K., 36-EP-4, 73-EP-11, 131-EP-18 Leary, B., 151-SR-6, 181-SR-7 Liu, N., 54-PC-4 Marcu, B., 114-LP-12 Meamarzadeh, G., 4-PSTR-1 Konopka, M., 177-LP-19 Leavitt, L., 117-ABPSI-6, 180-ABPSI-10 Liu, S., 50-EST-1 Marini, M., 176-LP-18 Mecham, M., 128-ITAR-3 Koo, J., 57-LP-6 Leccese, G., 179-LP-21 Liu, T., 12-EP-2 Marlar, C., 43-NFF-2 Mechentel, F., 137-HR-5

96 Kopasakis, G., 92-ABPSI-3/GTE-13, 180-ABPSI-10 Lecourt, R., 84-PC-5 Liu, W., 146-HSABP-6 Marshall, W., 90-LP-9 Medic, G., 76-GTE-11 Korkut, B., 18-EP-9 Lee, C., 20-HR-1, 53-PC-3, 167-HR-7 Liu, Y., 46-GTE-8, 77-GTE-12 Martelli, E., 90-LP-9, 178-LP-20 Meholic, G., 43-NFF-2, 126-NFF-5 Koshi, M., 160-PC-11 Lee, D., 93-SR-3, 179-LP-21 Lobbia, R., 41-EP-6, 100-EP-14 Martin, M., 58-LP-7 Meier, E., 57-LP-6 Kozak, P., 140-TES-2 Lee, H., 119-ECS-1 Long, J., 163-GTE-22 Martinez, M., 161-GTE-20, 168-APC-4 Melazzi, D., 4-PSTR-1 Kozmic, J., 119-ECS-1 Lee, I., 4-PSTR-1 Long, K., 150-ABPSI-9 Martinez-Sanchez, M., 183-EP-22 Melcher, J., 91-LP-10 Kozulovic, D., 150-ABPSI-9 Lee, J., 4-PSTR-1, 57-LP-6, 166-HSABP-10 Longmier, B., 41-EP-6, 159-EP-21, 183-EP-22 Martini, M., 101-EP-15, 108-APC-2 Melis, M., 56-LP-5 Kratz, J., 77-GTE-12 Lee, K., 166-HSABP-10 Loparo, K., 140-TES-2 Maruyama, N., 51-EC-2, 170-TM-4 Mena, J., 99-ITAR-2 Kreiner, K., 116-LP-14 Lee, P., 15-GTE-1, 45-GTE-7 Lopez, A., 32-LP-4 Mashayek, F., 26-PC-2 Menart, J., 13-EP-3, 72-EP-10 Kroeger, D., 58-LP-7 Lee, S., 93-SR-3 Lopez Ortega, A., 73-EP-11, 153-EP-19 Mason, A., 129-ITAR-4 Menon, S., 35-EDU-1 Kublik, D., 58-LP-7 Lee, W., 53-PC-3 López Peña, F., 114-LP-12 Mason, L., 21-APS-1, 139-EC-4 Meredith, R., 161-GTE-20 Kubo, N., 146-HSABP-6 Lee, Y., 166-HSABP-10 Lord, C., 4-PSTR-1 Masuda, I., 177-LP-19 Merill, W., 172-SCP-3 Kubota, K., 4-PSTR-1, 13-EP-3, 95-EP-13, 131-EP-18 Leger, J., 138-APC-3 Lou, Z., 165-HSABP-9 Masuoka, T., 177-LP-19 Merino, M., 131-EP-18 Kudo, K., 146-HSABP-6 Leiter, H., 12-EP-2, 47-EP-5, 159-EP-21 Loureda, O., 4-PSTR-1 Mataloni, A., 151-SR-6 Merino-Martinez, M., 95-EP-13 Kuehl, H., 139-EC-4 Lekeux, A., 30-LP-2 Love, N., 4-PSTR-1 Matlock, T., 41-EP-6, 153-EP-19 Meritt, R., 166-HSABP-10 Kuhmann, J., 12-EP-2 Lekki, J., 161-GTE-20 Lowe, K., 105-GTE-16/ABPSI-5 Matsuo, A., 48-HSABP-2/GTE-9, 157-HSABP-8/PC-9 Merkle, C., 165-HSABP-9 Kukies, R., 12-EP-2, 159-EP-21 Lema, M., 114-LP-12 Lozano, P., 94-EP-12 Merkley, D., 167-HR-7 Kulis, M., 109-EPOL-1/ESYS-1 Lemieux, P., 137-HR-5 Lu, F., 48-HSABP-2/GTE-9, 136-HSABP-7/ABPSI-8, Matsuoka, K., 48-HSABP-2/GTE-9, 157-HSABP-8/ Mern, J., 180-ABPSI-10 Kulkarni, A., 90-LP-9 Lemmer, K., 29-EP-1, 120-EP-16, 158-EP-20 142-SCP-2 PC-9 Merrill, W., 78-APS-2 Kumar, S., 45-GTE-7 Leonardi, M., 147-LP-15 Lucca Fabris, A., 4-PSTR-1 Mavris, D., 17-GTE-3, 22-EC-1, 33-ABPSI-1/GTE-4, Metscher, J., 139-EC-4 Kumar, V., 15-GTE-1, 45-GTE-7 Lerardo, N., 148-LP-16 Lupoglazoff, N., 71-SR-5 92-ABPSI-3/GTE-13, 162-GTE-21 Metz, B., 172-SCP-3 Kundu, K., 85-PC-6 Lestrade, J., 167-HR-7 Lynch, A., 75-GTE-10 Maxwell, T., 110-TM-3 Metzger, S., 56-LP-5 Kundu, R., 135-GTE-19 Lev, D., 108-APC-2 Lynch, E., 112-PC-8 May, R., 132-APS-3, 140-TES-2, 162-GTE-21 Meyer, E., 94-EP-12 Kuninaka, H., 36-EP-4, 159-EP-21 Levin, D., 18-EP-9 Lynch, S., 44-GTE-6, 76-GTE-11 Mazouffre, S., 12-EP-2, 41-EP-6 Meyer, M., 56-LP-5 Kuo, K., 107-HR-4 Lewandowski, E., 51-EC-2, 139-EC-4, 169-EC-5 MacEachron, P., 177-LP-19 McBride, S., 49-HR-2 Meyer, T., 115-LP-13 Kurbatskii, K., 45-GTE-7 Leylegian, J., 85-PC-6 MacInnis, D., 88-HSABP-3 McCallum, P., 21-APS-1 Michels, B., 143-HR-6 Kurishita, Y., 53-PC-3 Leyva, I., 32-LP-4, 57-LP-6 Mack, M., 60-SCP-1 McCleskey, C., 80-APC-1 Author/Session Chair Index Mikellides, I., 13-EP-3, 73-EP-11, 130-EP-17, 153- Nakagaki, M., 54-PC-4 Oefelein, J., 26-PC-2, 106-HSABP-5 Parthasarathy, R., 52-TES-1 Pulido, C., 143-HR-6 EP-19 Nakagawa, I., 167-HR-7 Oh, D., 158-EP-20 Páscoa, J., 138-APC-3 Pulling, R., 114-LP-12 Miki, H., 117-ABPSI-6 Nakamura, T., 29-EP-1 Ohe, K., 167-HR-7 Pasquale, N., 151-SR-6 Puszynski, J., 152-ECS-2 Milana, C., 151-SR-6 Nakashima, H., 131-EP-18 Ohlinger, W., 130-EP-17 Pastrone, D., 92-ABPSI-3/GTE-13, 167-HR-7 Puszynski, M., 152-ECS-2 Milanovic, I., 76-GTE-11 Nakata, D., 36-EP-4 Oigawa, Y., 47-EP-5 Patterson, M., 12-EP-2, 62-EP-8, 72-EP-10, 130- Puterbaugh, S., 16-GTE-2 Millard, J., 148-LP-16 Nakazono, B., 58-LP-7, 116-LP-14, 143-HR-6 Okai, K., 78-APS-2 EP-17 Qifan, Z., 136-HSABP-7/ABPSI-8 Miller, J., 61-EDU-2, 102-NFF-4 Nakles, M., 18-EP-9 Okaya, S., 78-APS-2 Patton, C., 165-HSABP-9 Qin, A., 25-PC-1 Miller, S., 115-LP-13 Nalim, M., 33-ABPSI-1/GTE-4, 103-GTE-14/PC-7 Okita, K., 36-EP-4 Pavarin, D., 4-PSTR-1 Qin, F., 106-HSABP-5 Mireles, O., 102-NFF-4 Naraghi, M., 99-ITAR-2, 179-LP-21 Okninski, A., 58-LP-7 Paxson, D., 48-HSABP-2/GTE-9, 103-GTE-14/PC-7 Qin, Z., 113-HSABP-4 Miyamoto, C., 35-EDU-1 Nardi, R., 61-EDU-2 Okuno, Y., 4-PSTR-1, 51-EC-2, 95-EP-13 Pencil, E., 62-EP-8 Qualls, A., 14-NFF-1, 102-NFF-4 Miyasaka, T., 131-EP-18 Narsai, P., 137-HR-5 Olah, A., 43-NFF-2, 50-EST-1, 113-HSABP-4 Penko, P., 20-HR-1, 140-TES-2 Quinlan, J., 91-LP-10, 106-HSABP-5 Miyazaki, K., 4-PSTR-1, 18-EP-9 Nasuti, F., 32-LP-4, 49-HR-2, 90-LP-9, 147-LP-15, Oleson, S., 101-EP-15, 108-APC-2, 158-EP-20 Perez, V., 61-EDU-2 Quiroz, M., 146-HSABP-6 Mizukami, M., 58-LP-7 178-LP-20, 179-LP-21 Olsen, J., 178-LP-20 Perigo, D., 178-LP-20 Rademakers, R., 59-ABPSI-2 Moder, J., 56-LP-5 Natan, B., 25-PC-1 Omran, A., 109-EPOL-1/ESYS-1 Perkins, H., 103-GTE-14/PC-7 Radke, C., 115-LP-13 Mohamed, D., 4-PSTR-1 Natewa, V., 99-ITAR-2 Ono, K., 131-EP-18 Perullo, C., 17-GTE-3, 33-ABPSI-1/GTE-4, Rafalskyi, D., 12-EP-2 Mohammadi-Abdar, H., 4-PSTR-1 Naumann, K., 93-SR-3, 116-LP-14 Onofri, M., 147-LP-15 92-ABPSI-3/GTE-13 Raitses, Y., 41-EP-6 Mon, K., 20-HR-1 Navarro, J., 29-EP-1, 95-EP-13, 183-EP-22 Oohira, T., 116-LP-14 Petersen, E., 53-PC-3, 61-EDU-2, 93-SR-3, 167-HR-7 Rajagopal, M., 103-GTE-14/PC-7 Mondragon, U., 173-PC-10 Neal, J., 35-EDU-1 Oravec, H., 60-SCP-1 Peterson, P., 120-EP-16 Ramachandran, P., 90-LP-9 Mongia, H., 15-GTE-1, 45-GTE-7 Neely, A., 178-LP-20 Oriti, S., 169-EC-5 Pfeiffer, J., 139-EC-4 Ramamurti, R., 105-GTE-16/ABPSI-5 Moon, H., 15-GTE-1 Neff, G., 120-EP-16 Osamura, A., 94-EP-12 Picard, M., 19-HSABP-1 Ramasubramanian, C., 57-LP-6 Mora Sanchez, P., 105-GTE-16/ABPSI-5 Negishi, H., 179-LP-21 Oschwald, M., 112-PC-8 Piechna, J., 103-GTE-14/PC-7 Rambaud, P., 114-LP-12 Morcos, S., 82-TM-2 Negri, M., 116-LP-14 Oshio, Y., 168-APC-4 Pimenta, A., 4-PSTR-1, 61-EDU-2 Rame, E., 177-LP-19

97 Morehead, R., 91-LP-10 Neri, A., 118-SR-4, 181-SR-7 Östlund, J., 178-LP-20 Pinero, L., 62-EP-8 Ramsel, J., 116-LP-14 Morgan, V., 60-SCP-1 Neto, S., 61-EDU-2 Overly, J., 99-ITAR-2 Pinto, P., 116-LP-14 Rancourt, D., 19-HSABP-1 Morii, Y., 160-PC-11 Neuroth, C., 75-GTE-10 Owen, A., 77-GTE-12 Piskin, T., 182-ST-1 Randeria, M., 177-LP-19 Morozumi, T., 48-HSABP-2/GTE-9 Ng, W., 105-GTE-16/ABPSI-5 Oyama, S., 137-HR-5, 167-HR-7 Piszczor, M., 52-TES-1, 109-EPOL-1/ESYS-1, 128- Randolph, T., 158-EP-20 Morris, P., 105-GTE-16/ABPSI-5 Nguyen, C., 169-EC-5 Oyama, T., 4-PSTR-1 ITAR-3, 140-TES-2 Rani, S., 91-LP-10, 112-PC-8 Morris, S., 16-GTE-2, 44-GTE-6, 76-GTE-11 Nguyen, H., 22-EC-1 Ozawa, K., 20-HR-1 Pizzarelli, M., 179-LP-21 Rani, V., 112-PC-8 Morrison, C., 78-APS-2 NGuyen Duc, J., 114-LP-12 Ozcan, M., 162-GTE-21 Plachta, D., 56-LP-5 Ranjan, D., 61-EDU-2 Moslehi, B., 46-GTE-8 Nichols, R., 136-HSABP-7/ABPSI-8 Ozgun, M., 4-PSTR-1 Plante, J., 19-HSABP-1 Ransom, D., 114-LP-12 Motil, S., 56-LP-5 Nieberding, J., 89-LP-8 Ozkan, S., 45-GTE-7 Plasek, M., 130-EP-17 Rao, P., 119-ECS-1 Mouri, K., 177-LP-19 Niedermaier, H., 116-LP-14 Özüpek, S., 118-SR-4 Poinsatte, P., 44-GTE-6 Rarata, G., 58-LP-7 Mueller, N., 103-GTE-14/PC-7 Niehuis, R., 59-ABPSI-2 Pack, S., 75-GTE-10 Polk, J., 120-EP-16, 130-EP-17, 159-EP-21 Rath, M., 12-EP-2 Muhammad, M., 170-TM-4 Nirudhoddi, B., 35-EDU-1 Packard, T., 74-NFF-3 Polzin, K., 12-EP-2, 36-EP-4, 158-EP-20, 159-EP-21 Rayman, M., 62-EP-8 Muir, S., 143-HR-6 Nishida, H., 29-EP-1 Pai, C., 172-SCP-3 Pons Lorente, A., 49-HR-2 Reed, B., 31-LP-3, 148-LP-16 Mukhopadhyay, A., 15-GTE-1 Nishikizawa, S., 116-LP-14 Painter, J., 147-LP-15 Ponti, F., 181-SR-7 Reese, I., 159-EP-21 Müller, L., 150-ABPSI-9 Nishiyama, I., 159-EP-21 Paisley, J., 40-SR-2 Porst, J., 12-EP-2 Reid, C., 50-EST-1 Murakami, A., 146-HSABP-6 Nishiyama, K., 159-EP-21 Pakmehr, M., 46-GTE-8 Poston, D., 21-APS-1, 102-NFF-4 Reid, D., 93-SR-3 Murakami, D., 168-APC-4 Nivet, P., 114-LP-12 Palaszewski, B., 109-EPOL-1/ESYS-1, 126-NFF-5 Pote, B., 158-EP-20 Reimonte, P., 147-LP-15 Murakami, N., 95-EP-13 Noh, K., 93-SR-3 Pan, H., 106-HSABP-5 Pourpoint, T., 31-LP-3, 90-LP-9 Reisz, A., 168-APC-4 Murakami, T., 51-EC-2 Nojima, K., 166-HSABP-10 Pan, K., 160-PC-11 Powers, R., 105-GTE-16/ABPSI-5 Rempfer, D., 140-TES-2 Murphy, D., 101-EP-15, 158-EP-20 Nojima, Y., 168-APC-4 Pancotti, A., 43-NFF-2 Prasad, J., 135-GTE-19, 162-GTE-21 Ren, J., 72-EP-10 Murphy, J., 160-PC-11 Noll, B., 160-PC-11 Panzardi, S., 55-GTE-5 Preclik, D., 147-LP-15 Renganathan, A., 22-EC-1 Murray, C., 21-APS-1, 22-EC-1 Nomura, H., 78-APS-2 Papamoschou, D., 105-GTE-16/ABPSI-5 Preuss, J., 114-LP-12 Rezaei, F., 4-PSTR-1 Murray, W., 35-EDU-1, 104-GTE-15/ABPSI-4 Nordeen, C., 157-HSABP-8/PC-9 Park, C., 20-HR-1, 187-ITAR-1 Prince, B., 94-EP-12 Rhodes, R., 80-APC-1 Musielak, D., 146-HSABP-6 Notaro, V., 57-LP-6 Park, G., 4-PSTR-1 Proctor, M., 60-SCP-1 Ribarov, L., 52-TES-1 Myers, S., 50-EST-1 O’Brien, W., 88-HSABP-3 Park, K., 167-HR-7 Pugachev, A., 60-SCP-1 Ricci, D., 179-LP-21 Naitoh, K., 168-APC-4 O’neill, W., 138-APC-3 Parker, T., 22-EC-1 Pugmire, T., 99-LP-11 Riccius, J., 176-LP-18 Author/Session Chair Index Ricklick, M., 134-GTE-18 Sankaran, V., 32-LP-4, 91-LP-10, 165-HSABP-9, Sehgal, A., 101-EP-15 Snyder, C., 17-GTE-3 Swanson, T., 72-ITAR-1 Riehl, R., 110-TM-3 179-LP-21 Sehirlioglu, A., 81-EC-3 Snyder, J., 72-EP-10, 120-EP-16 Sweeney, B., 35-EDU-1 Rinehart, A., 161-GTE-20 Santner, J., 25-PC-1, 85-PC-6 Seidel, J., 92-ABPSI-3/GTE-13 Sobbi, M., 107-HR-4 Szabo, J., 158-EP-20 Risha, G., 25-PC-1 Sarathy, M., 173-PC-10 Sekerak, M., 41-EP-6 Sobczak, K., 58-LP-7 Tacina, K., 15-GTE-1, 75-GTE-10 Roberson, B., 4-PSTR-1, 95-EP-13 Sarawate, N., 60-SCP-1 Seleznev, R., 160-PC-11 Soeder, J., 132-APS-3 Tada, H., 137-HR-5 Robinson, J., 80-APC-1, 108-APC-2, 138-APC-3, Sardeshmukh, S., 53-PC-3 Selim, H., 173-PC-10 Sokol, M., 140-TES-2 Tafti, D., 15-GTE-1 168-APC-4 Sargent, D., 31-LP-3 Selmo, A., 4-PSTR-1 Solmaz, M., 26-PC-2, 177-LP-19 Tagashira, T., 78-APS-2 Rodriguez, M., 43-NFF-2 Sargent, S., 114-LP-12 Semrau, G., 78-APS-2 Song, W., 152-ECS-2 Tahara, H., 36-EP-4, 62-EP-8, 95-EP-13, 120-EP-16 Rojas Mata, S., 130-EP-17 Sasaki, T., 18-EP-9, 54-PC-4, 109-EPOL-1/ESYS-1 Sen, S., 15-GTE-1 Soto, J., 101-EP-15 Tai, J., 92-ABPSI-3/GTE-13, 162-GTE-21 Romero, D., 52-TES-1 Sasson, J., 169-EC-5 Shaohua, Z., 57-LP-6, 113-HSABP-4 Soulas, G., 12-EP-2, 72-EP-10, 153-EP-19 Tak, H., 53-PC-3 Roncioni, P., 179-LP-21 Sato, Y., 58-LP-7 Sharma, O., 76-GTE-11 Sowers, T., 77-GTE-12 Takagi, S., 48-HSABP-2/GTE-9 Ross, C., 33-ABPSI-1/GTE-4 Sattelmayer, T., 112-PC-8 Shastry, R., 72-EP-10, 130-EP-17, 153-EP-19 Spangelo, S., 158-EP-20 Takahashi, K., 18-EP-9, 54-PC-4, 109-EPOL-1/ESYS-1 Ross, M., 16-GTE-2 Satyanarayana, C., 34-SR-1 Shchetkovskiy, A., 99-ITAR-2 Spencer, V., 58-LP-7 Takao, Y., 131-EP-18 Rossoni, L., 84-PC-5 Sauer, J., 90-LP-9 Shebalin, J., 183-EP-22 Spores, R., 31-LP-3 Takegahara, H., 58-LP-7 Rotella, S., 35-EDU-1 Sauvageau, D., 182-ST-1 Sheehan, J., 159-EP-21, 183-EP-22 Spurling, J., 34-SR-1, 118-SR-4 Takenaka, S., 4-PSTR-1 Rougeux, A., 142-SCP-2 Sawka, W., 187-ITAR-1 Sherman, A., 152-ECS-2 Spurlock, F., 89-LP-8 Takeshita, S., 18-EP-9, 109-EPOL-1/ESYS-1 Roux, F., 71-SR-5 Schaefer, B., 143-HR-6 Shi, J., 111-ABPSI-7 Spyridon, P., 49-HR-2 Takiguchi, K., 51-EC-2 Rovey, J., 53-PC-3, 108-APC-2 Schaible, B., 46-GTE-8 Shi, K., 44-GTE-6 St. George, A., 88-HSABP-3 Talley, D., 32-LP-4 Roy, B., 173-PC-10 Scharfe, D., 132-APS-3 Shimada, T., 20-HR-1, 49-HR-2, 54-PC-4, 137-HR-5, St. John, C., 168-APC-4 Tam, J., 166-HSABP-10 Roy, S., 4-PSTR-1 Scharnhorst, R., 59-ABPSI-2, 111-ABPSI-7 167-HR-7 Stahl, K., 163-GTE-22 Tamura, T., 168-APC-4 Rønningen, J., 143-HR-6 Schetz, J., 166-HSABP-10 Shimizu, T., 160-PC-11 Starkey, R., 106-HSABP-5, 114-LP-12, Tan, W., 182-ST-1 Ruf, J., 168-APC-4 Schierman, J., 77-GTE-12 Shin, J., 112-PC-8 136-HSABP-7/ABPSI-8 Tanabe, M., 26-PC-2, 84-PC-5

98 Ruiz Haro, M., 95-EP-13 Schlapkohl, T., 77-GTE-12 Shin, K., 53-PC-3 Steadman, T., 118-SR-4 Tanaka, M., 34-SR-1, 51-EC-2, 168-APC-4 Russo Sorge, A., 49-HR-2 Schley, J., 152-ECS-2 Shindo, T., 58-LP-7 Stechmann, D., 35-EDU-1, 157-HSABP-8/PC-9 Tang, Y., 4-PSTR-1 Ruz-Nuglo, F., 152-ECS-2 Schlieben, G., 179-LP-21 Shinohara, S., 29-EP-1 Steelant, J., 114-LP-12, 147-LP-15 Tangirala, V., 157-HSABP-8/PC-9 Ryan, S., 74-NFF-3 Schloeder, N., 12-EP-2, 100-EP-14 Shipley, K., 91-LP-10 Steen, D., 49-HR-2 Tani, Y., 137-HR-5, 167-HR-7 Ryan, W., 151-SR-6, 181-SR-7, 71-SR-5 Schmid, M., 112-PC-8 Shouse, D., 75-GTE-10 Steffan, S., 78-APS-2 Tanikawa, T., 29-EP-1 Ryon, J., 75-GTE-10 Schmidt, V., 130-EP-17 Shtessel, Y., 147-LP-15 Steiner, M., 35-EDU-1 Tao, H., 19-HSABP-1 Sagara, Y., 168-APC-4 Schmitt, S., 177-LP-19 Shu, S., 136-HSABP-7/ABPSI-8 Steinetz, B., 60-SCP-1 Tarau, C., 110-TM-3, 170-TM-4 Sahara, H., 116-LP-14 Schmitz, A., 179-LP-21 Shyam, V., 44-GTE-6, 55-GTE-5 Stern, T., 110-TM-3 Tarditi, A., 51-EC-2 Saito, M., 26-PC-2, 51-EC-2 Schmitz, P., 21-APS-1, 110-TM-3 Sibé, F., 148-LP-16 Sternchuss, A., 30-LP-2 Taya, K., 30-LP-2 Sakai, S., 54-PC-4 Schmuland, D., 99-ITAR-2 Siebenhaar, A., 157-HSABP-8/PC-9 Stewart, C., 177-LP-19 Taylor, T., 35-EDU-1 Sakai, T., 94-EP-12 Schnackel, J., 30-LP-2 Sik, F., 4-PSTR-1 Stewart, J., 49-HR-2 Tedder, S., 15-GTE-1, 75-GTE-10 Sakuma, T., 116-LP-14 Schnitzler, B., 14-NFF-1, 74-NFF-3, 102-NFF-4 Silva, D., 110-TM-3 Stewart, M., 14-NFF-1 Terashima, H., 160-PC-11 Sakuranaka, N., 166-HSABP-10 Schoenberg, R., 58-LP-7 Simmons, S., 105-GTE-16/ABPSI-5 Stoddard, W., 88-HSABP-3 Terhune, K., 94-EP-12 Salazar, D., 21-APS-1, 176-LP-18 Schomberg, K., 178-LP-20 Simon, D., 161-GTE-20 Stoltz, P., 72-EP-10 Terracciano, A., 32-LP-4 Salim, A., 132-APS-3 Schulze, M., 112-PC-8 Singer, C., 182-ST-1 Strauch, PE, J., 21-APS-1, 22-EC-1 Thomas, J., 93-SR-3, 167-HR-7 Salvatore, V., 176-LP-18 Schumaker, S., 115-LP-13 Sjauw, W., 101-EP-15 Stucky, M., 76-GTE-11 Thomas, R., 183-EP-22 Sameshima, H., 109-EPOL-1/ESYS-1 Schwabacher, M., 132-APS-3 Slater, J., 59-ABPSI-2 Su, W., 170-TM-4 Thorpe, D., 80-APC-1 Sammet, T., 61-EDU-2, 93-SR-3 Schwaiger, M., 138-APC-3 Smeltzer, M., 52-TES-1 Subramanian, S., 134-GTE-18 Thrasher, J., 72-ITAR-1 Sanal Kumar, V., 108-APC-2, 109-EPOL-1/ESYS-1, Schwer, D., 157-HSABP-8/PC-9 Smith, B., 13-EP-3, 119-ECS-1 Sugita, Y., 131-EP-18 Thumann, A., 116-LP-14 111-ABPSI-7, 118-SR-4, 146-HSABP-6 Scoccimarro, D., 151-SR-6 Smith, C., 109-EPOL-1/ESYS-1 Sugiu, N., 26-PC-2 Thurman, D., 44-GTE-6, 163-GTE-22 Sanchez, L., 4-PSTR-1, 115-LP-13, 176-LP-18 Scott, J., 51-EC-2 Smith, D., 101-EP-15 Surmacz, P., 58-LP-7 Tian, B., 29-EP-1 Sánchez Martínez, V., 95-EP-13 Scroggins, A., 114-LP-12 Smith, J., 44-GTE-6 Surzhikov, S., 160-PC-11 Tian, D., 76-GTE-11 Sanders, A., 61-EDU-2 Seal, S., 93-SR-3 Smith, K., 81-EC-3 Sutliff, T., 21-APS-1 Tian, L., 57-LP-6, 113-HSABP-4, 176-LP-18 Sandifer, C., 21-APS-1 Sebastian, J., 55-GTE-5 Smith, L., 75-GTE-10, 173-PC-10 Suzuki, T., 95-EP-13 Tidhar, I., 62-EP-8 Sankaran, K., 101-EP-15 Sedano, N., 147-LP-15, 176-LP-18 Smith, M., 72-EP-10 Suzuki, Y., 166-HSABP-10 Tilley, S., 158-EP-20 Sedwick, R., 4-PSTR-1, 43-NFF-2 Smoraldi, A., 179-LP-21 Swanson, R., 58-LP-7 Tillman, G., 76-GTE-11 Author/Session Chair Index Ting, Y., 54-PC-4 Votta, R., 179-LP-21 Willits, J., 90-LP-9 Yeboah, S., 82-TM-2 Zinnecker, A., 46-GTE-8, 162-GTE-21, 172-SCP-3 Toftul, A., 36-EP-4 Vuillot, F., 71-SR-5 Wills, D., 138-APC-3 Yedavalli, R., 77-GTE-12 Zoltowski, M., 112-PC-8 Tomioka, S., 146-HSABP-6, 166-HSABP-10 Wada, A., 58-LP-7 Wills, R., 55-GTE-5 Yehia, M., 110-TM-3 Zuckerman, Z., 108-APC-2 Tompkins, D., 150-ABPSI-9 Walker, A., 169-EC-5 Wilson, A., 32-LP-4 Yetter, R., 25-PC-1 Topal, A., 45-GTE-7 Walker, J., 100-EP-14 Wilson, D., 136-HSABP-7/ABPSI-8 Yim, J., 141-EP-23, 148-LP-16 Toson, E., 79-HR-3 Walker, M., 12-EP-2, 73-EP-11, 100-EP-14, 120- Wilson, J., 107-HR-4 Yin, C., 104-GTE-15/ABPSI-4 Tournes, C., 147-LP-15 EP-16 Wilson, S., 139-EC-4, 169-EC-5 YingQing, G., 77-GTE-12 Trammell, M., 102-NFF-4 Walker, S., 107-HR-4 Winglee, R., 4-PSTR-1, 95-EP-13 Yongsheng, Z., 88-HSABP-3, 106-HSABP-5, Trase, L., 132-APS-3 Walmsley, N., 110-TM-3 Winters, B., 99-ITAR-2, 129-ITAR-4 166-HSABP-10 Trefny, C., 117-ABPSI-6 Wan-sheng, N., 57-LP-6 Wirz, R., 41-EP-6, 131-EP-18, 153-EP-19 Yoon, C., 15-GTE-1 Trejo, A., 179-LP-21 Wang, L., 19-HSABP-1 Wolfe, C., 60-SCP-1 Yoon, W., 93-SR-3 Tretjakov, P., 160-PC-11 Wang, Q., 19-HSABP-1 Wolford, D., 22-EC-1 Yoon, Y., 4-PSTR-1, 112-PC-8 Trezzolani, F., 4-PSTR-1 Wang, X., 4-PSTR-1, 110-TM-3, 180-ABPSI-10 Won, J., 53-PC-3 Young, J., 12-EP-2 Trivedi, D., 60-SCP-1 Wang, Z., 17-GTE-3 Won, S., 25-PC-1, 85-PC-6 Young, M., 132-APS-3 Trujillo, A., 179-LP-21 Wanser, K., 126-NFF-5 Wong, E., 77-GTE-12 Yu, K., 166-HSABP-10, 173-PC-10 Tseng, K., 172-SCP-3 Wargnier, Q., 176-LP-18 Wong, W., 139-EC-4, 169-EC-5 Yu, N., 49-HR-2 Tsikata, S., 41-EP-6 Warren, J., 74-NFF-3, 102-NFF-4 Wongyai, P., 107-HR-4 Yu, X., 81-EC-3 Tsukizaki, R., 159-EP-21 Watanabe, H., 13-EP-3, 131-EP-18 Woods, A., 119-ECS-1 Yungster, S., 85-PC-6, 103-GTE-14/PC-7 Tucker, D., 102-NFF-4 Watanabe, T., 78-APS-2 Woodward, J., 126-NFF-5 Yuzhen, L., 106-HSABP-5, 166-HSABP-10 Tuladhar, L., 140-TES-2 Watanabe, Y., 117-ABPSI-6, 170-TM-4 Woodward, R., 115-LP-13 Zabaykin, V., 160-PC-11 Tuncer, O., 45-GTE-7 Watiotienne, T., 114-LP-12 Wordingham, C., 130-EP-17 Zahn, M., 112-PC-8 Turkoz, E., 4-PSTR-1 Waxman, B., 143-HR-6 Wrbanek, J., 161-GTE-20, 172-SCP-3 Zaki, A., 82-TM-2

99 Ueno, K., 168-APC-4 Webb, R., 132-APS-3 Wu, G., 81-EC-3 Zakrajsek, J., 21-APS-1 Uhl, D., 81-EC-3 Weber, D., 60-SCP-1 Wu, J., 49-HR-2 Zametaev, E., 176-LP-18 Unruh, B., 101-EP-15, 158-EP-20 Wegener, J., 32-LP-4 Wulff, D., 59-ABPSI-2 Zapata, E., 80-APC-1 Urbano, A., 112-PC-8 Wei, F., 57-LP-6 Xiaojun, C., 106-HSABP-5 Zein-Sabatto, M., 46-GTE-8 Uslu, S., 26-PC-2, 45-GTE-7 Wei, L., 106-HSABP-5, 166-HSABP-10 Xiaolei, C., 77-GTE-12 Zeng, P., 49-HR-2 Usrey, M., 46-GTE-8 Wei, S., 49-HR-2 Xisto, C., 138-APC-3 Zha, G., 126-NFF-5 Uzol, O., 26-PC-2 Wei, Z., 19-HSABP-1 Xu, J., 161-GTE-20 Zhang, H., 104-GTE-15/ABPSI-4 Valenzuela, J., 56-LP-5 Weiser, V., 116-LP-14 Xu, K., 173-PC-10 Zhang, M., 92-ABPSI-3/GTE-13 Van Horn, E., 181-SR-7 Weitzberg, A., 102-NFF-4 Xu, X., 4-PSTR-1, 54-PC-4, 57-LP-6, 113-HSABP-4, Zhang, S., 160-PC-11 Van Muijden, J., 170-TM-4 Welch, G., 55-GTE-5, 76-GTE-11, 104-GTE-15/ 176-LP-18 Zhang, T., 35-EDU-1 Vancil, B., 130-EP-17 ABPSI-4, 163-GTE-22 Xuan, L., 57-LP-6, 113-HSABP-4, 176-LP-18 Zhang, X., 17-GTE-3, 152-ECS-2 Vanelli, C., 158-EP-20 Werner, J., 102-NFF-4 Yamada, K., 177-LP-19 Zhang, Y., 92-ABPSI-3/GTE-13 Vaudolon, J., 41-EP-6 Wernet, M., 105-GTE-16/ABPSI-5 Yamakawa, H., 168-APC-4 Zhao, B., 49-HR-2 Vaughan, D., 143-HR-6 Wey, T., 54-PC-4 Yamamoto, N., 131-EP-18 Zheng, K., 138-APC-3 Vazquez, A., 99-ITAR-2 Wheeler, C., 119-ECS-1 Yamamoto, Y., 26-PC-2 Zheng, X., 60-SCP-1 Veloo, P., 25-PC-1 White, H., 183-EP-22 Yan, W., 104-GTE-15/ABPSI-4 Zhou, H., 17-GTE-3 Verberne, C., 143-HR-6, 167-HR-7 Whitmore, S., 79-HR-3, 107-HR-4, 167-HR-7 Yan, Z., 106-HSABP-5, 166-HSABP-10 Zhou, T., 170-TM-4 Veres, J., 135-GTE-19 Whiton, J., 76-GTE-11 Yanagida, N., 36-EP-4 Zhu, S., 176-LP-18 Verrière, J., 180-ABPSI-10 Wierman, M., 112-PC-8 Yang, H., 35-EDU-1 Zhu, T., 142-SCP-2 Vieille, B., 30-LP-2 Wignall, T., 165-HSABP-9 Yang, I., 166-HSABP-10 Zhu, Y., 152-ECS-2 Vijayakumar, N., 136-HSABP-7/ABPSI-8 Wilhelm, P., 99-LP-11 Yang, L., 119-ECS-1 Ziemer, J., 94-EP-12 Vitucci, J., 4-PSTR-1 Wilhelmi, C., 176-LP-18 Yang, V., 106-HSABP-5 Zilliac, G., 143-HR-6 Vk, V., 108-APC-2 Wilkin, H., 136-HSABP-7/ABPSI-8 Yang, X., 108-APC-2 Zimmerli, G., 56-LP-5 Voland, R., 129-ITAR-4 Williams, C., 11-LP-1, 89-LP-8 Yatsko, A., 129-ITAR-4 Zimmerman, J., 143-HR-6 Von Moll, A., 172-SCP-3 Williams, G., 31-LP-3, 72-EP-10 Yazici, B., 177-LP-19 Zink, G., 75-GTE-10 Votroubek, G., 43-NFF-2 Williams, S., 187-ITAR-1 Ye, Q., 57-LP-6 Zinn, B., 91-LP-10 IntroNotes

www.aiaa-propulsionenergy.org 10041 #aiaaPropEnergy IntroVenue Map

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