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Program For Monday, 03-Aug-2009
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0745 - 0945 |
Joint IECEC/JPC Opening Panel: 40th Apollo Anniversary Panel
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Korbel 4 |
| Chaired by: R. DICKMAN, AIAA Executive Director, Reston, VA |
Panelists:
Arnie Aldrich
Gerry Griffin
Glynn Lunney
Frank Van Rensselaer
J.R. Thompson
Harrison "Jack" Schmitt
Bob Sieck
Followed By: Lt. Governor Barbara O'Brien
'Workforce Development and the Future of Aerospace in Colorado' |
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1000 - 1230 |
Innovation in Launch Vehicle Applications - Boosters
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Korbel 4 |
Chaired by: Ray Johnson, Vice President Space Launch Operations, Aerospace Corporation
Panelists:
James Sponnick, VP Delta Programs, United Launch Alliance
Max Vozoff, Director, Civil Business Development, SpaceX
Bruce Tiller, Deputy Manager, Ares I First Stage, NASA Marshall Space Flight Center
Randolph L. Kendall, General Manager, Launch Systems Division, Aerospace Corporation
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|
| Session
1-
ABP-1
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ABPI Subsystem, Performance and Optimization
|
403 |
|
Chaired by: R. DAEBELLIEHN, Aerojet, Sacramento, CA, and D. KISLING, Belcan Corporation, North Palm Beach, FL
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|
1000
AIAA-2009-4800
Performances Analysis of High By Pass Jet Engine with Intercooling and Regeneration
R. Andriani and U. Ghezzi, Politecnico di Milano, Milan, Italy
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1030
AIAA-2009-4801
Numerical Study of a Gas Turbine Engine Ground Vortex
J. Barata, A. Maneta, and A. Silva, Universidade Beira Interior, Covilhã, Portugal
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1100
AIAA-2009-4802
Turbofan Volume Dynamics Model for Investigations of Aero- Propulso- Servo- Elastic Effects in a Supersonic Commercial Transport
J. Connolly and G. Kopasakis, NASA Glenn Research Center, Cleveland, OH; K. Lemon, Witchita State University, Wichita, KS
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1130
AIAA-2009-4803
Next Generation Propulsion & Air Vehicle Considerations
B. McKay, Lockheed Martin Aeronautics, Marietta, GA
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| Session
2-
APC-1
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Advanced Propulsion Concepts I
|
707 |
|
Chaired by: J. ROBINSON and F. CHANDLER, The Boeing Company, Huntington Beach, CA
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|
1000
AIAA-2009-4805
An Overview of Advanced Concepts for Near Space Systems
M. Young and S. Keith, U.S. Air Force Research Laboratory, Edwards AFB, CA; and A. Pancotti, ERC, Inc., Edwards AFB, CA
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1030
AIAA-2009-4806
Inlet Aerodynamics and Ram- Drag of Laser- Propelled Lightcraft Vehicles
T. Langener, L. Myrabo, and Z. Rusak, Rensselaer Polytechnic Institute, Troy, NY
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1100
AIAA-2009-4808
Multivariable PI Control for Tip- Jet Reaction Drive Systems
B. Kestner, J. Tai and D. Mavris, Georgia Institute of Technology, Atlanta, GA
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1130
AIAA-2009-4809
MAV Propulsion System Using the Coanda Effect
M. Schroijen and M. van Tooren, Delft University of Technology, Delft, The Netherlands
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1200
AIAA-2009-4807
Advanced MagLev Propulsion System and Its Economic Impact
T. Sharma, B. Mitra, C. Chatwin, R. Young, and P. Birch, University of Sussex, Brighton, Great Britain
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| Session
3-
EP-1
|
Cylindrical Hall Thrusters and Cusped Field Modeling
|
506 |
|
Chaired by: Y. RAITSES, Princeton University, Princeton, NJ, and J. MAKELA, Michigan Technological University, Houghton, MI
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|
1000
AIAA-2009-4810
Operation and Plume Measurements of Miniaturized Cylindrical Hall Thrusters with Permanent Magnets
Y. Raitses, E. Merino, J. Parker, and N. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ
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1030
AIAA-2009-4811
Investigation of Electron Transport in a Cylindrical Hall Thruster using a Kinetic Code
L. Brieda and M. Keidar, George Washington University, Washington, DC; Y. Raitses and N. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ
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1100
AIAA-2009-4812
Performance of a Permanent- Magnet Cylindrical Hall- Effect Thruster
K. Polzin, E. Sooby, and A. Kimberlin, NASA Marshall Space Flight Center, Huntsville, AL; Y. Raitses, E. Merino, and N. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ
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1130
AIAA-2009-4813
Spectroscopic and Electrostatic Investigation of the Diverging Cusped- Field Thruster
T. Matlock, R. Daspit, O. Batishchev, P. Lozano, and M. Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA
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1200
AIAA-2009-4814
Fully Kinetic Modeling of Divergent Cusped Field Thrusters
S. Gildea, O. Batishchev, and M. Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA
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| Session
4-
EP-2
|
Micropropulsion I
|
507 |
|
Chaired by: I. HRBUD, Purdue University, West Lafayette, IN, and D. COURTNEY, Massachusetts Institute of Technology, Cambridge, MA
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|
1000
AIAA-2009-4820
Micro- Vacuum Arc Thruster with Extended Lifetime
T. Zhuang, A. Shashurin, T. Denz, D. Chichka, and M. Keidar, George Washington University, Washington, DC
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1030
AIAA-2009-4823
Hollow Cathode Thrust Production Mechanisms
A. Grubisic and S. Gabriel, University of Southampton, Southampton, Great Britain
|
1100
AIAA-2009-4824
A Review of High Thrust, High Delta- V Options for Microsatellite Missions
D. Scharfe, ERC, Inc, Edwards AFB, CA; and A. Ketsdever, U.S. Air Force Research Laboratory, Edwards AFB, CA
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| Session
5-
EP-3
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NASA's Evolutionary Xenon Thruster (NEXT) and Other Gridded Ion Techology Development
|
505 |
|
Chaired by: M. CROFTON, The Aerospace Corporation, El Segundo, CA, and C. FARNELL, Colorado State University, Fort Collins, CO
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|
1000
AIAA-2009-4816
NEXT Single String Integration Test Results
G. Soulas, M. Patterson, and L. Pinero, NASA Glenn Research Center, Cleveland, OH; D. Herman, ASRC Aerospace Corporation, Cleveland, OH; and J. Snyder, Jet Propulsion Laboratory, Pasadena, CA
|
1030
AIAA-2009-4819
Near- Term High Power Ion Propulsion Options for Earth- Orbital Applications
M. Patterson and L. Pinero, NASA Glenn Research Center, Cleveland, OH; and J. Sovey, Alpha-Port, Inc., Cleveland, OH
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1100
AIAA-2009-4815
Characterization of the NASA NEXT Thruster
M. Crofton, J. Pollard, E. Beiting, R. Spektor, K. Diamant, X. Eapen, and R. Cohen, Aerospace Corporation, Los Angeles, CA; and M. Patterson, NASA Glenn Research Center, Cleveland, OH
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1130
AIAA-2009-4818
Particle- Based Plasma Simulation of NEXT Ion Engine
M. Jonell and J. Menart, Wright State University, Dayton, OH; and S. Mahalingam, Tech-X Corporation, Boulder, CO
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1200
AIAA-2009-5001
Thermo- Elastic Analyses of Ion- Thruster Grids
Y. Hayakawa, H. Yoshida, K. Miyazaki, and Y. Ohkawa, Japan Aerospace Exploration Agency, Chofu, Japan; H. Nagano, Japan Aerospace Exploration Agency, Tsukuba, Japan; and S. Kitamura, Japan Aerospace Exploration Agency, Chofu, Japan
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| Session
6-
GT-1
|
Ground Test I
|
401 |
|
Chaired by: K. MOLDER, 46th Test Wing, Eglin AFB, FL, and E. MARQUART, Raytheon, Tucson, AZ
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|
1000
AIAA-2009-4825
Biannular Airbreathing Nozzle Rig Facility Development at Purdue University
A. Sandroni, C. Cummings, Y. Matsutomi, S. Meyer, J. Sullivan, and S. Heister, Purdue University, West Lafayette, IN
|
1030
AIAA-2009-4826
Numerical Investigation of Inlet Induced Distortions of a Turbofan Engine Within an Indoor Test Facility
B. Muth, S. Bindl, C. Lehmann and R. Niehuis, University of the German Federal Armed Forces, Munich, Germany
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1100
AIAA-2009-4827
Mass and Size Distribution Measurements of Particulates from a Gas Turbine Combustor Using Modern Mobility Analyzer and Particle Sizer
Y. Sevcenco and P. Bowen, Cardiff University, Cardiff, Great Britain; M. Johnson, Rolls-Royce plc, Derby, Great Britain; M. Hilton and M. Welch, Reading University, Reading, Great Britain; and M. Miller, QinetiQ, Farnborough, Great Britain
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1130
AIAA-2009-4828
Experimental Investigations on Macro- Aerodynamics Within a Jet Engine Ground Test Facility
S. Bindl, B. Muth and R. Niehuis, University of Federal Armed Forces Munich, Neubiberg, Germany
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| Session
7-
GTE-1
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Combustors I - Combustor Design
|
405 |
|
Chaired by: B. SEKAR, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
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|
1000
AIAA-2009-4829
Parametric Study of Liquid Atomization by Slinger Injectors
C. Sescu, B. Kucinschi, A. Afjeh, C. Masiulaniec, and A. Sescu, University of Toledo, Toledo, OH
|
1030
AIAA-2009-4830
Experiments and Simulation Study on Flow Field and LBO of TVC With H/L Changed
F. Xing, Zhejiang University, Hangzhou, China (prc); W. Fan and M. Yang, Beihang University, Beijing, China (prc)
|
1100
AIAA-2009-4831
Effects of Fueling Scheme on the Performance of a Trapped Vortex Combustor Rig
Y. Liu, R. Li, H. Liu, and M. Yang, Beihang University, Beijing, China (prc)
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1130
AIAA-2009-4832
Internal Flow Simulation of Dump Diffusers for Modern Aircraft Engines
V. Sanalkumar, Kumaraguru College of Technology, Coimbatore, India; S. Sahoo, Indian Institiute of Science, Bangalore, India; and S. Raghunathan, Quenn's University of Belfast, Belfast, Ireland
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| Session
8-
GTE-2
|
Turbines - Advanced Design Concepts
|
404 |
|
Chaired by: M. SUBRAMANIAN, QuEST-ASE, Inc., Cincinnati, OH
|
|
1000
AIAA-2009-4834
An Assessment of Oil Free Bearing and Electric Machine Technology for Optimized Rotorcraft Propulsion Systems
R. Bruckner, NASA Glenn Research Center, Cleveland, OH
|
1030
AIAA-2009-4835
Experimental and Numerical Investigation on Flow Characteristics of a Vaneless Counter- Rotating Turbine at Off- Design Conditions
Q. Zhao, J. Qiao, H. Wang, X. Zhao and J. Xu, Institute of Engineering Thermophysics Chinese Academy of Sciences, Beijing, China (prc)
|
1100
AIAA-2009-4836
Influence of Tip Clearance Size on Flow Characteristics of a Vaneless Counter- Rotating Turbine
Q. Zhao, J. Qiao, H. Wang, X. Zhao and J. Xu, Institute of Engineering Thermophysics Chinese Academy of Sciences, Beijing, China (prc)
|
1130
AIAA-2009-4837
Two- Combustor Engine’s Transient Performance
A. Lee, DSO National Laboratories, London, Great Britain; R. Singh and S. Probert, Cranfield University, London, Great Britain
|
1200
AIAA-2009-4838
Two- combustor Engines’ Performances Under Design and Off- Design Conditions
A. Lee, DSO National Laboratories, London, Great Britain; R. Singh and S. Probert, Cranfield University, London, Great Britain
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| Session
9-
HR-1
|
Design and Analysis of Hybrid Rocket Launch Vehicles
|
712 |
|
Chaired by: C. CARMICINO, Università di Napoli, Naples, Italy, and B. EVANS, Pennsylvania State University, University Park, PA
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|
1000
AIAA-2009-4840
Status Update Report for the Peregrine Sounding Rocket Project: Part III
E. Doran, J. Dyer, and M. Marzoña, Stanford University, Stanford, CA; A. Karabayaglu, Space Propulsion Group, Sunnyvale, CA; G. Zilliac and R. Mosher, NASA Ames Research Center, Moffett Field, CA; and B. Cantwell, Stanford University, Stanford, CA
|
1030
AIAA-2009-4841
Optimization of Hybrid Sounding Rockets for Hypersonic Testing
L. Casalino and D. Pastrone, Politecnico di Torino, Torino, Italy
|
1100
AIAA-2009-4842
Development and Launch of the Purdue Hybrid Rocket Technology Demonstrator
J. Tsohas, B. Appel, A. Rettenmaier, M. Walker, and S. Heister, Purdue University, West Lafayette, IN
|
1130
AIAA-2009-4843
Integrated Design of Hybrid Rocket Upper Stage and Launcher Trajectory
L. Casalino, Politecnico di Torino, Torino, Italy; G. Colasurdo, Università di Roma, Roma, Italy; and D. Pastrone, Politecnico di Torino, Torino, Italy
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| Session
10-
HYP-1
|
High Speed Propulsion Design Issues
|
406 |
|
Chaired by: U. MEHTA, NASA Dryden Research Center, Los Altos, CA, and L. MCKINNEY, McKinney Associates, Town & Country, MO
|
|
1000
AIAA-2009-5116
Fueling Study on Scramjet Operability Enhancement
K. Lin and C. Tam, Taitech Inc., Wright-Patterson AFB, OH; K. Jackson, P. Kennedy, S. Williams and D. Olmstead, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
|
1030
AIAA-2009-5117
Shock Positioning Controls Design for a Supersonic Inlet
G. Kopasakis and J. Connolly, NASA Glenn Research Center, Brookpark, OH
|
1100
AIAA-2009-5118
Current State of High Speed Propulsion: Gaps, Obstacles and Technological Challenges in Hypersonic Applications
T. Barber, B. Maicke and J. Majdalani, University of Tennessee Space Institute, Tullahoma, TN
|
1130
AIAA-2009-5119
Electric Power Generation Onboard Hypersonic Aircraft
P. Sforza, University of Florida, Gainesville, FL
|
| Session
11-
HYP-2
|
Scramjet Engines - Computational Investigations I
|
407 |
|
Chaired by: J. KLINGE, Lockheed Martin Aeronautics Company, Palmdale, CA, and R. MOEHLENKAMP, Pratt & Whitney Rocketdyne, West Palm Beach, FL
|
|
1000
AIAA-2009-4844
Simulations of the HyShot- II (Scramjet) Model Using High- Resolution Methods
Z. Rana, B. Thornber and D. Drikakis, Cranfield University, Cranfield, Bedfordshire, Great Britain
|
1030
AIAA-2009-4845
Isolator/Combution Chamber Interactions During Supersonic Combustion
Q. Tu and C. Segal, University of Florida, Gainesviile, FL
|
1100
AIAA-2009-4846
Automated Validation of CFD Codes for Analysis of Scramjet Propulsive Flows Using CRAVE
Z. Liu, K. Brinckman, and S. Dash, Combustion Research and Flow Technology, Inc., Pipersville, PA
|
1130
AIAA-2009-4848
Numerical Simulation of Open Active Control of Low Frequency Combustion Instability Related to Vortex Shedding in Model Ramjet Dump Combustor
Q. Fei, H. Guoqiang, L. Peijin, and L. Jiang, Northwestern Polytechnical University, Xi'an, China (prc)
|
Session 12-HYP-3
1000 - |
X-51, Prelude to the 2009 First Flight (Invited)
|
601/603 |
| Chaired by: J. CASTRO, Pratt & Whitney Rocketdyne, West Palm Beach, FL, and K. BOWCUTT, The Boeing Company, Aliso Viejo, CA |
Panelists:
George Thum: Pratt & Whitney Rocketdyne X-51 Program Manager - Propulsion (PWR's) perspective
Joe Vogel: Boeing X-51 Program Manager - Vehicle (Boeing's) perspective
Charlie Brink: USAF X-51 Program Manager - AFRL's perspective
Ming Tang: Associate Booth Allen Hamilton - DARPA (TTO's) perspective
Mark Lewis: Willis Young Prof. of Aerospace Engineering, University of Maryland; President Elect of the AIAA - Academic perspective
|
|
| Session
13-
LP-1
|
Components: Nozzles I
|
706 |
|
Chaired by: G. MAGGIO, Information Systems Laboratories, Bellmore, NY, and S. FISHER
|
|
1000
AIAA-2009-4854
Flow Separation Studies During the Transition Modes of a Sub- Scale Dual- Bell Nozzle
S. Verma, National Aerospace Laboratories, Bangalore, India; R. Stark, C. Nuerenberger-Genin, and O. Haidn, DLR, German Aerospace Research Center, Hardthausen, Germany
|
1030
AIAA-2009-4855
Experimental Study on Flow Transition in Dual Bell Nozzles
C. Nurnberger-Genin and R. Stark, DLR, German Aerospace Research Center, Lampoldshausen, Germany
|
1100
AIAA-2009-4856
Nozzle Side Load Testing and Analysis at MSFC
J. Ruf, D. McDaniels, and A. Brown, NASA Marshall Space Flight Center, Huntsville, AL
|
1130
AIAA-2009-4858
Numerical Simulation of Reacting and Non- Reacting Nozzle Flows
A. Arabshahi, R. Webster, K. Sreenivas, D. Hyams and D. Whitfield, University of Tennessee at Chattanooga, Chattanooga, TN
|
| Session
14-
LP-2
|
Feed Systems I
|
704 |
|
Chaired by: T. GIEL, Jacobs Technology, Huntsville, AL, and J. WEISS, Jet Propulsion Laboratory, Pasadena, CA
|
|
1000
AIAA-2009-4860
Cryogenic Sloshing Tests in a Pressurized Cylindrical Reservoir
T. Arndt and M. Dreyer, ZARM University of Bremen, Bremen, Germany; P. Behruzi and M. Winter, EADS Astrium Space Transportation, Bremen, Germany; A. vanForeest, DLR German Aerospace Research Center, Bremen, Germany
|
1030
AIAA-2009-4863
Implementation of the VOF Method in the DLR TAU Code
M. Gauer, V. Hannemann, and K. Hannemann, DLR, German Aerospace Research Center, Göttingen, Germany
|
| Session
15-
LP-3
|
Modeling and Simulation: Combustion Instability
|
703 |
|
Chaired by: W. WANG, The Aerospace Corporation, Los Angeles, CA, and D. COOTE, NASA Stennis Space Center, Stennis Space Center, MS
|
|
1000
AIAA-2009-4864
Combustion Instability Analysis in a Hydrogen- Oxygen Rocket Engine
S. Feng, Y. Cheng, and W. Nie, The Academy of Equipment Command and Technology, Beijing, China (prc)
|
1030
AIAA-2009-4865
Analytical and Numerical Development of a Baffled Liquid Rocket Combustion Stability Code
J. Quinlan, D. Milano, A. Kirkpatrick, C. Mitchell and T. Hinerman, Colorado State University, Fort Collins, CO
|
1100
AIAA-2009-4866
Computation of Acoustic Oscillations and Combustion Stability in a Rocket Engine with Combined Hub/Blade Baffles
D. Milano, J. Quinlan, A. Kirkpatrick, and C. Mitchell, Colorado State University, Fort Collins, CO; and T. Hinerman, Pratt & Whitney Rocketdyne, Canoga Park, CA
|
| Session
16-
LP-4
|
Systems: Hydrogen Peroxide
|
705 |
|
Chaired by: P. ALLIOT, Snecma, Vernon, France, and B. BATES, Aerospace Testing Alliance, Tullahoma, TN
|
|
1000
AIAA-2009-4849
On Shut- off Explosion of High Test Hydrogen Peroxide/RP- 1 Engine
J. Tan, T. Yang, Z. Wang and J. Liu, National University of Defence Technology, Changsha, Hunan, China (prc)
|
1030
AIAA-2009-4852
Preliminary Flight Test of Hydrogen Peroxide Retro- Propulsion Module for Lander Demonstration
S. An and S. Jo, Korea Advanced Institute of Science and Technology, Daejeon, South Korea; J. Wee and H. Yoon, Spacesolutions, Daejeon, South Korea; S. Kwon, Korea Advanced Institute of Science and Technology, Daejeon, South Korea
|
1100
AIAA-2009-4853
The Integration and Test of a 5- N Hydrazine Propulsion System
T. Yuan, B. Huang, M. Tang, and C. Chen, National Cheng Kung University, Tainan, Taiwan (roc); Y. Chen and B. Wu, National Space Organization, Tainan, Taiwan (roc)
|
| Session
17-
NFF-1
|
Plasma and Fusion Propulsion
|
702 |
|
Chaired by: T. KAMMASH, University of Michigan, Ann Arbor, MI, and L. MYRABO, Rensselaer Polytechnic Institute, Troy, NY
|
|
1000
AIAA-2009-4869
Fusion- Fission Hybrid Revisited: Potential for Space Applications
T. Kammash, R. Tang, and M. Hartman, University of Michigan, Ann Arbor, MI
|
1030
Oral Presentation
Engineering Gaseous Fusion Propulsion
A. Reisz and J. Brainerd, Reisz Engineers, Huntsville, AL
|
1100
AIAA-2009-4871
Future of Antiproton Triggered Fusion Propulsion
B. Cassenti, University of Connecticut, Storrs, CT; and T. Kammash, University of Michigan, Ann Arbor, MI
|
1130
AIAA-2009-4872
Power Generation for Beamed Microwave Propulsion Concepts
S. Hammerland, B. Cornella, H. Song, and A. Ketsdever, University of Colorado at Colorado Springs, Colorado Springs, CO
|
1200
AIAA-2009-4873
Airbreathing Hypersonic Laser Thermal Propulsion Experiments with a LightCraft Vehicle - Status
Update
I. Salvador and L. Myrabo, Rensselaer Polytechnic Institute, Troy, NY; M. Minucci, A. de Oliveira, P. Toro, and J. Channes, Instituto de Estudos Avançados, São José dos Campos, Brazil
|
| Session
18-
PC-1
|
Fundamental Combustion Processes I
|
304 |
|
Chaired by: J. LEYLEGIAN, Manhattan College, Riverdale, NY, and B. CHEHROUDI, U.S. Air Force Research Laboratory, Lancaster, CA
|
|
1000
AIAA-2009-4882
Calibration of an Impinging Jet Injector Suitable for Liquid and Gelled Hypergolic Propellants
M. James, T. Kubal, S. Son, W. Anderson and T. Pourpoint, Purdue University, West Lafayette, IN
|
1030
AIAA-2009-4883
Unsteady Extinction of Opposed Jet Ethylene / Methane HiFIRE Surrogate Fuel Mixtures vs. Air
S. Vaden, Georgia Institute of Technology, Atlanta, GA; R. Debes, University of Kansas, Lawrence, KS; E. Lash, George C. Marshall HS, Falls Church, VA; R. Burk, U.S. Air Force Academy, Colorado Springs, CO; C. Boyd, North Cross HS, Roanoke, VA; G. Pellett, NASA Langley Research Center, Hampton, VA; and L. Wilson, Lockheed Martin Space Operations, Hampton, VA
|
| Session
19-
PC-2
|
Propellant and Fuel Development I
|
708 |
|
Chaired by: F. GOULDIN, Cornell University, Ithaca, NY
|
|
1000
AIAA-2009-4874
Ballistic Characterization of ALH3- Based Propellants for Solid and Hybrid Rocket Propulsion
L. DeLuca and L. Rossettini, Politecnico di Milano, Milan, Italy; C. Kappenstein, University of Poitiers, Poitiers, France; and V. Weiser, Fraunhofer Institut fur Chemische Technologie, Pfinztal-Berghausen, Germany
|
1030
AIAA-2009-4875
A Monopropellant Gas Generator Based on N2O Decomposition for “Green” Propulsion and Power Generation
Y. Scherson, Stanford University, San Francisco, CA; K. Lohner, Stanford University, Stanford, CA; B. Lariviere, Pratt and Whitney Rocketdyne, Canoga Park, CA; B. Cantwell and T. Kenny, Stanford University, Stanford, CA
|
1100
AIAA-2009-4876
Azide- Based Fuel Additives for Ionic Monopropellants
K. Farhat and C. Kappenstein, University of Poitiers, Poiters, France; and Y. Batonneau, University of Poitiers, Poitiers, France
|
1130
AIAA-2009-4877
Aluminum- ICE (ALICE) Propellants for Hydrogen Generation and Propulsion
G. Risha, Pennsylvania State University, Altoona, PA; T. Connell, R. Yetter, and V. Yang, Pennsylvania State University, University Park, PA; T. Wood, M. Pfeil, T. Pourpoint, and S. Son, Purdue University, West Lafayette, IN
|
1200
AIAA-2009-4878
High Performance Green Propellant for Satellite Applications
K. Anflo and R. Mollerberg, ECAPS, Solna, Sweden; K. Neff and P. King, Moog, Inc., East Aurora, NY
|
| Session
20-
SCP-1
|
Propulsion Controls I
|
402 |
|
Chaired by: A. BEHBAHANI, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and R. BICKFORD, Expert Microsystems Inc., Orangevale, CA
|
|
1000
AIAA-2009-4884
Analysis of Decentralization and Fault- Tolerance Concepts for Distributed Engine Control
J. DeCastro, L. Tang and C. Byington, Impact Technologies LLC, Rochester, NY; D. Culley, NASA Glenn Research Center, Cleveland, OH
|
1030
AIAA-2009-4885
Stability of Fiber Optic Networked Decentralized Distributed Engine Control Under Time Delays
R. Belapurkar and R. Yedavalli, Ohio State University, Columbus, OH; B. Moslehi, Intelligent Fiber Optic Systems Corporation, Santa Clara, CA
|
1100
AIAA-2009-4886
Design and Implementation of a Characterization Test Rig for Evaluating High Bandwidth Liquid Fuel Flow Modulators
J. Saus, C. Chang, J. DeLaat, and D. Vrnak, NASA Glenn Research Center, Cleveland, OH
|
1130
AIAA-2009-5532
Distributed Control of Turbofan Engines
M. Pakmehr, Georgia Institute of Technology, Atlanta, GA; M. Mounier, Georgia Institute of Technology,, Atlanta, GA; N. Fitzgerald, G. Kiwada, and J. Paduano, Aurora Flight Sciences Corporation, Manassas, VA; E. Feron, Georgia Institute of Technology, Atlanta, GA; and A. Behbahani, Air Force Research Laboratory, Wright-Patterson, AFB, OH
|
| Session
21-
SR-1
|
Modeling and Simulation I
|
711 |
|
Chaired by: I. BULATHSINGHALA, The Aerospace Corporation, Los Angeles, CA
|
|
1000
AIAA-2009-4890
Feasibility Study and Demonstration of an Aluminum and Ice Solid Propellant
T. Wood, M. Pfeil, T. Pourpoint, J. Tsohas, and S. Son, Purdue University, West Lafayette, IN; T. Connell, G. Risha, and R. Yetter, Pennsylvania State University, University Park, PA
|
1030
AIAA-2009-4891
Numerical Simulation of the Aerothermostructural Response of a Composite Solid Rocket Nozzle During Motor Ignition
J. Pitot, University of KwaZulu-Natal, Durban, South Africa; E. Morozov, Australian Defence Force Academy, Canberra, Australia; and G. Bright, University of KwaZulu-Natal, Durban, South Africa
|
| Session
22-
SR-2
|
Solid Rocket Development and Combustion Characteristics I
|
710 |
|
Chaired by: I. CHANG, The Aerospace Corporation, Los Angeles, CA, and B. LEARY, ATK TP&C Allegany Ballistics Laboratory, Rocket Center, WV
|
|
1000
AIAA-2009-4893
Burning Characteristics of Composite Propellant Using Ammonium Perchlorate Modified by Ethylene Glycol
M. Kohga and H. Tsuzuki, National Defense Academy, Yokosuka, Japan
|
1030
AIAA-2009-4894
Ignition and Combustion Characteristic of Aluminum and Magnalium Particles in AP/AN Composite Propellant
T. Mano, Nihon University, Funabashi, Japan; M. Tanaka, National Defense Academy of Japan, Yokosuka, Japan; M. Tanabe and T. Kuwahara, Nihon University, Funabashi, Japan
|
1100
AIAA-2009-4896
Solid Propellant Combustion with Surface Regression by Coupled Gas- Solid Approach
J. Choi and S. Menon, Georgia Institute of Technology, Atlanta, GA
|
1130
AIAA-2009-4892
How to Design, Build and Test Small Solid Propellant Rocket Motor (Part One)
M. Ziraksaz, Islamic Azad University, Tehran, Iran
|
| Session
23-
VS-1
|
Space Transportation I
|
709 |
|
Chaired by: D. ESCHER, Rolls-Royce North American, Greenwood, IN, and D. SAUVAGEAU, ATK, Minneapolis, MN
|
|
1000
AIAA-2009-4897
Space- Based Solar Power Prototypes Enabled by a Heavy Lift Launcher
W. Rothschild and T. Talay, John Frassanito & Associates, Inc., Houston, TX; and E. Henderson, NASA Johnson Space Center, Houston, TX
|
1030
AIAA-2009-4898
Pressure- Fed Versus Pump- Fed Propulsion Trade for the Aquarius Launch Vehicle
A. Turner, Space Systems/Loral, Palo Alto, CA
|
1100
AIAA-2009-4899
On- Orbit Propulsion and Methods of Momentum Management for the International Space Station
R. Swanson, The Boeing Company, Houston, TX; V. Spencer, S. Russell and K. Metrocavage, NASA Johnson Space Center, Houston, TX; U. Kamath, The Boeing Company, Houston, TX
|
1130
AIAA-2009-4900
Propulsion in the ATV Spacecraft System - Lessons Learnt
V. L'Hullier, Astrium GmbH, Les Mureaux, France
|
|
1330 - 1530 |
Innovation in Launch Vehicle Applications - Upper Stage
|
Korbel 4 |
Chaired by: Dr. George Sowers, Vice President Business Development, United Launch Alliance
Panelists:
Mark Wilkins, VP Atlas Programs, United Launch Alliance
Max Vozoff, Director, Civil Business Development, SpaceX
Dr. Kent Chojnacki, Definition Manager, Ares I Upper Stage, NASA Marshall Space Flight Center
Bernard Kutter, Manager Advanced Programs, United Launch Alliance
|
|
| Session
24-
ABP-2
|
ABPI Inlets and Exhaust
|
403 |
|
Chaired by: D. MAYER, The Boeing Company, Tukwila, WA, and D. KISLING, Belcan Corporation, North Palm Beach, FL
|
|
1330
AIAA-2009-4901
Active Control of Flow in Serpentine Inlets for Blended Wing- Body Aircraft
A. Ferrar, W. O'Brien, and W. Ng, Virginia Polytechnic Institute and State University, Blacksburg, VA; R. Florea, United Technologies Research Center, Hartford, CT; and D. Arend, NASA Glenn Research Center, Cleveland, OH
|
1400
AIAA-2009-4902
Experimental Testing and Numerical Simulations of Shrouded Plug Nozzle Flowfields
D. Kapilavai and C. Merkle, Purdue University, West Lafayette, IN; J. Tapee, Northrop Grumman, Redondo Beach, CA; J. Sullivan, Purdue University, West Lafayette, IN; T. Wayman and T. Conners, Gulfstream Aerospace Corporation, Savannah, GA
|
1430
AIAA-2009-4903
Computation and Analysis of Dual Nozzle Flow Fields and Infrared Radiation
H. Huang, J. Zhang, and Z. Wang, Northwestern Polytechnical University, Xi'an, China (prc)
|
1500
AIAA-2009-4904
Computation of an Exhaust System Flow Field and Infrared Radiation
J. Zhang, Z. Wang, and Y. Cai, Northwestern Polytechnical University, Xi'an, China (prc)
|
| Session
25-
APC-2
|
Advanced Propulsion Concepts II
|
707 |
|
Chaired by: T. CHEN, NASA Marshall Space Flight Center, Huntsville, AL, and J. ROBINSON, The Boeing Company, Huntington Beach, CA
|
|
1330
AIAA-2009-4906
Preliminary Design of a Cable Spacecraft Connecting Mutually Tidally Locked Planetary Bodies
F. Graham, Kent State University, East LIverpool, OH
|
1400
AIAA-2009-4908
Design of an Expander Cycle Engine with J- 2 Equivalent Thrust
D. Thorpe, Thortek Labs, Mount Sterling, KY
|
1430
AIAA-2009-5539
Economics of Launch Vehicles & Two Configurations for Tremendous Cost Reductions
D. Thorpe, Thortek Labs, Irvine, KY
|
| Session
27-
EP-5
|
Hall Thruster Modeling
|
506 |
|
Chaired by: S. ROY, University of Florida, Gainesville, FL, and E. FOSSUM, Michigan Technological University, Houghton, MI
|
|
1330
AIAA-2009-4913
Implementation of the Kinetic Bohm Condition in a Hall Thruster Hybrid Code
E. Ahedo and R. Santos, ETSI Aeronáuticos Universidad Politécnica de Madrid, Madrid, Spain
|
1400
AIAA-2009-4914
Accuracy Improvements in a Hall Thruster PIC/Fluid Code
R. Santos and E. Ahedo, ETSI Aeronáuticos Universidad Politécnica de Madrid, Madrid, Spain
|
| Session
28-
EP-6
|
Xenon Flow Control and Storage
|
507 |
|
Chaired by: J. CARDIN, VACCO Industries Inc., El Monte, CA, and J. DANKANICH, Gray Research, Inc., Cleveland, OH
|
|
1330
AIAA-2009-4909
High Performance Xenon Flow System (XFS) Optimized for Low Mass, Volume, and Cost
M. Osborn and C. Netwall, U.S. Naval Research Laboratory, Washington, DC
|
1400
AIAA-2009-4910
Advanced Xenon Feed System (AXFS) Development and Hot- fire Texting
J. Dankanich, Gray Research, Inc., Cleveland, OH; J. Cardin and A. Dien, VACCO, El Monte, CA; C. Netwall and M. Osborn, U.S. Naval Research Laboratory, Washington, DC; and H. Kamhawi, NASA Glenn Research Center, Cleveland,
|
1430
AIAA-2009-4911
Xenon Flow Control System for Ion Thrusters
M. Yagnanarayana, Indian Space Research Organisation, Thiruvananthapuram, India
|
1500
AIAA-2009-4912
Cryostorage of Propellants for Electric Propulsion
O. Duchemin, Snecma, Vernon, France; D. Valentian, ITG, Paris, France; N. Cornu, Snecma, Vernon, France
|
| Session
29-
GT-2
|
Ground Test II
|
401 |
|
Chaired by: R. CASTNER, NASA Glenn Research Center, Cleveland, OH, and S. SMITH-BRITO, The Boeing Company, Bellevue, WA
|
|
1330
AIAA-2009-4921
Design and Construction of a Microjet Engine at Amirkabir University of Technology
A. Horoufi and M. Boromand, Amirkabir University of Technology, Tehran, Iran
|
1400
AIAA-2009-4922
Adding Value at Hypersonic Speed
D. Vaughn and D. Garrard, Aerospace Testing Alliance, Arnold AFB, TN; and J. Jolliffe, U.S. Air Force, Arnold AFB, TN
|
1430
AIAA-2009-5520
A Design of Experiments Approach to Turbine Engine Aeromechanical Ground Testing
J. Cox, Aerospace Testing Alliance, Arnold AFB, TN
|
| Session
30-
GTE-3
|
Combustors II - Combustion Processes
|
405 |
|
Chaired by: R. GAETA, Georgia Tech Research Institute, Atlanta, GA
|
|
1330
AIAA-2009-4924
Effect of Confinement on Colorless Distributed Combustion for Gas Turbine Engines
V. Arghode and A. Gupta, University of Maryland, College Park, MD
|
1400
AIAA-2009-4925
Investigation of the Effects of Vitiated Conditions on the Autoignition of JP- 8
C. Fuller, P. Gokulakrishnan, M. Klassen and R. Roby, CSE Inc., Columbia, MD; B. Kiel, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
|
1430
AIAA-2009-4926
Numerical Study of Stability Limits of Premixed- Swirl Flames
N. Shelil, N. Syred and A. Griffiths, Cardiff University, Cardiff, Great Britain
|
1500
AIAA-2009-4927
Injection of Supercritical Aviation Kerosene Fuel into Quiescent Atmospheric Environment
W. Gao, H. Liang, Q. Xu, and Y. Lin, Beihang University, Beijing, China (prc); and C. Sung, University of Connecticut, Storrs, CT
|
| Session
31-
GTE-4
|
Turbines - Numerical Modeling
|
404 |
|
Chaired by: A. HAMED, University of Cincinnati, Cincinnati, OH
|
|
1330
AIAA-2009-4928
Turbulence Model Comparisons for Mixing Plane Simulations of a Multistage Low Pressure Turbine Operating at Low Reynolds Number
D. Sanders, U.S. Air Force Reserach Laboratory, Wright-Patterson AFB, OH; W. O'Brien, Virginia Polytechnic Institute and State University, Blacksburg, VA; R. Sondergaard, M. Polanka, and D. Rabe, U.S. Air Force Reserach Laboratory, Wright-Patterson AFB, OH
|
1400
AIAA-2009-4929
Direct Numerical Simulation of the Turbulent Wake of an Infinitely Thin Flat Plate
N. Madavan and M. Rai, NASA Ames Research Center, Moffett Field, CA
|
1430
AIAA-2009-4930
Modeling the Influence of Inflow Turbulence on LPT Performance
M. Schwarze, M. Martinstetter, and R. Niehuis, University of the Federal Armed Forces Munich, Neubiberg, Germany
|
1500
AIAA-2009-4931
Improvement on S- A Model For predicting corner separation Based On Turbulence Transport Nature
D. Wang, L. Lu, and Q. Li, Beijing University of Areonautics and Astronautics, Beijing, China (prc)
|
| Session
32-
HIS-1
|
History I
|
303 |
|
|
|
1330
AIAA-2009-4934
Early Amateur Satellites
F. Graham, Kent State University, East Liverpool, OH
|
1400
AIAA-2009-4933
Supersonic Transport (SST) Engines
D. Jensen, Rolls-Royce Heritage Trust, Indianapolis, IN; G. Brines, Pratt & Whitney (Retired), South Glastonbury, CT; J. Blanton, GE Energy, Greenville, SC
|
| Session
33-
HR-2
|
Hybrid Rocket Motor Testing I
|
712 |
|
Chaired by: A. KARABEYOGLU, Space Propulsion Group Inc., Sunnyvale, CA, and K. KUO, Pennsylvania State University, University Park, PA
|
|
1330
AIAA-2009-4935
A Study on the Regression Rate of Parrafin- Based Hybrid Rocket Fuels
I. Nakagawa, S. Hikone, and T. Suzuki, Tokai University, Hiratsuka, Japan
|
1400
AIAA-2009-4937
Basic Aspects of the Hybrid Engine Operation
C. Carmicino, University of Naples, Naples, Italy; O. Orlandi, SNPE Matériaux Energétique, Vert-Le-Petit, France; A. Sorge, University of Naples, Naples, Italy; F. Dauch, SNPE Matériaux Energétique, Vert-Le-Petit, France; R. De Amicis, AVIO, Colleferro, Italy; and M. de Rosa, ESA ESTEC, Noordwijk, The Netherlands
|
1430
AIAA-2009-4938
Performance and Analysis of Vortex Oxidizer Injection in a Hybrid Rocket Motor
C. Jones, D. Myre, and J. Cowart, U. S. Naval Academy, Annapolis, MD
|
| Session
34-
HYP-4
|
High Speed Propulsion Modeling
|
407 |
|
Chaired by: T. O'BRIEN, Aerojet, Sacramento, CA, and R. STARKEY, University of Colorado, Boulder, CO
|
|
1330
AIAA-2009-4939
Scramjet Engine Model MASIV: Role of Mixing, Chemistry and Wave Interaction
S. Torrez, J. Driscoll, D. Dalle and D. Micka, University of Michigan, Ann Arbor, MI
|
1400
AIAA-2009-4940
Advanced Modeling of New Fuel/Air Mixing Data Sets for Scramjet Applications
R. Ungewitter, K. Brinckman, and S. Dash, Combustion Research and Flow Technology, Inc., Pipersville, PA
|
1430
AIAA-2009-4941
Effect of Chemistry Modeling on Scramjet Engine Design
R. Starkey, University of Colorado, Boulder, CO
|
| Session
35-
HYP-5
|
Pulse Detonation Engines
|
406 |
|
Chaired by: V. TANGIRALA and A. RASHEED, GE Global Research Center, Niskayuna, NY
|
|
1330
AIAA-2009-4945
Flame Sensing in Pulsed Combustion Using Ion Probes, Diodes and Visual Indications
M. Kowalkowski, Y. Matsutomi, and S. Heister, Purdue Universty, West Lafayette, IN
|
1400
AIAA-2009-4946
Flight Performance Comparison of Pulse Detonation and Ramjet- Propelled Vehicles
T. Halsmer, Y. Matsutomi, and S. Heister, Purdue University, West Lafayette, IN
|
| Session
36-
LP-5
|
Components: Heat Transfer I
|
704 |
|
Chaired by: J. SAUER, ORBITEC, Madison, WI, and S. MILLER, Aerojet, Seattle, WA
|
|
1330
AIAA-2009-4952
Control of Transition Between Two Working Modes of a Dual- Bell Nozzle by Gas Injection
T. Tomita, M. Takahashi, and M. Sasaki, Japan Aerospace Exploration Agency, Kakuda, Japan
|
1400
AIAA-2009-4953
Film Cooling Effect on Dual- Bell Nozzle Flow Transition
E. Martelli, Second University of Naples, Aversa, Italy; F. Nasuti and M. Onofri, Sapienza - Università di Roma, Rome, Italy
|
1430
AIAA-2009-5526
Compartment Venting Analyses of Ares I First Stage Systems Tunnel
Q. Wang and S. Arner, ATK Launch Systems, Brigham City, UT
|
| Session
37-
LP-6
|
Components: Inducers, Pulsator, Pump
|
705 |
|
Chaired by: G. GRAYSON, The Boeing Company, Huntington Beach, CA, and D. PRECLIK, Astrium Space Transportation, Munich, Germany
|
|
1330
AIAA-2009-4955
Experimental Performance of a Tapered Axial Inducer: Comparison with Analytical Predictions
L. Torre, A. Pasini and A. Cervone, ALTA S.p.A., Pisa, Italy; L. d'Agostino, University of Pisa, Pisa, Italy
|
1400
AIAA-2009-4956
Numerical Studies on Frequency Response to Mass Flow Rate Variations in a Hydromechanical Pulsator
M. Balasubramanyam, D. Lineberry, C. Chen, and V. Bazarov, University of Alabama in Huntsville, Huntsville, AL
|
1430
AIAA-2009-4957
Improvement on the Low Ns High- Pressure Pump
H. Kagawa, Japan Aerospace Exploration Agency, Tsukuba, Japan; A. Okayasu and T. Ota, ASIRI, Mitaka, Japan
|
| Session
38-
LP-7
|
Modeling and Simulation: Thrust Chamber
|
706 |
|
Chaired by: D. COOTE, NASA Stennis Space Center, Stennis Space Center, MS, and G. REBER, The Aerospace Corporation, Los Angeles, CA
|
|
1330
AIAA-2009-4958
Simulation of Cavitation Process in Oxidizer Pump of a Liquid Rocket Engine
D. Ramesh and H. Alimohammadi, Tehran University of Technology, Tehran, Iran
|
1400
AIAA-2009-4959
Numerical Simulation of Combustion Flow Field in RD- 170 Chamber
D. Li and X. Xu, Beijing University of Aeronautics and Astronautics, Beijng, China (prc)
|
1430
AIAA-2009-5529
Development of a 10- N Liquid Bipropellant Thruster for Geostationary Spacecraft Program of Indian Space Reseach Organization
C. Balan, S. Venkateswaran, T. Madhukumar, and C. Senan, Indian Space Research Organization, Trivandrum, India
|
| Session
39-
LP-8
|
Systems: Engines and Demonstrations I
|
703 |
|
Chaired by: S. FORDE, Aerojet, Sacramento, CA, and P. ALLIOT, Snecma, Vernon, France
|
|
1330
AIAA-2009-4947
Vulcain X Technological Demonstration Roadmap
F. Lassoudiere, J. Chopinet, P. Fayolle, and C. Verplancke, Snecma, Vernon, France; S. Guedron and P. Supie, Centre National d’Études Spatiales, Evry, France
|
1400
AIAA-2009-4948
Sea- Level Flight Demonstration and Altitude Characterization of a LO2/LCH4 Based Ascent Propulsion Lander
J. Collins, E. Hurlbert, K. Romig, and J. Melcher, NASA Johnson Space Center, Houston, TX; A. Hobson, NASA White Sands Test Facility, Las Cruces, NM; and P. Eaton, Armadillo Aerospace, Caddo Mills, TX
|
1430
AIAA-2009-4949
Liquid Oxygen / Liquid Methane Test Results of the RS- 18 Lunar Ascent Engine at Simulated Altitude Conditions at NASA White Sands Test Facility
J. Melcher, NASA Johnson Space Center, Houston, TX; and J. Allred, White Sands Test Facility, Las Cruces, NM
|
1500
AIAA-2009-4950
Design Analysis of the Ares I Pogo Accumulator
L. Swanson and T. Giel, ERC Inc., Huntsville, AL
|
| Session
40-
NFF-2
|
Future Flight I
|
702 |
|
Chaired by: B. PALASZEWSKI, NASA Glenn Research Center, Cleveland, OH, and G. MEHOLIC, The Aerospace Corporation, El Segundo, CA
|
|
1330
AIAA-2009-4961
Atmospheric Mining in the Outer Solar System: Mining Design Issues and Considerations
B. Palaszewski, NASA Glenn Research Center, Cleveland, OH
|
1400
AIAA-2009-4962
Thrust Augmentation in Solid Rocket Motors Using Beamed Microwave Energy
N. Gimelshein and S. Gimelshein, ERC, Inc., Edwards AFB, CA; and A. Ketsdever, U.S. Air Force Research Laboratory, Colorado Springs, CO
|
1430
Oral Presentation
Advanced Propulsion Concepts for Interstellar Travel Part 1: Challenges and Current Systems
G. Meholic, The Aerospace Corporation, El Segundo, CA
|
| Session
41-
PC-3
|
Fundamental Combustion Processes II
|
304 |
|
Chaired by: S. NAIK, Purdue University, West Lafayette, IN
|
|
1330
AIAA-2009-4967
Laser- Induced Fluorescence Studies of Nitric Oxide Formed in a Hydrogen- Nitrous Oxide Premixed Flame
O. Powell, C. Dreyer and P. Papas, Colorado School of Mines, Golden, CO
|
1400
AIAA-2009-4968
A Noble Kinetic Model of H2/O2 System Applicable to Liquid Rocket Engine Combustion
K. Shimizu, A. Hibi, and M. Koshi, University of Tokyo, Tokyo, Japan; Y. Morii, Graduate University for Advanced Studies, Sagamihara, Japan; and N. Tsuboi, Japan Aerospace Exploration Agency, Sagamihara, Japan
|
1430
AIAA-2009-4969
Cumulative Effect of Parent Species in a Surrogate Mixture on Flame Extinction
V. Katta, Innovative Scientific Solutions, Inc., Dayton, OH; and W. Roquemore, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
|
1500
AIAA-2009-4970
Soot Formation in Vitiated Combustion
B. Singh and W. Lear, University of Florida, Gainesville, FL
|
| Session
42-
PC-4
|
Propellant and Fuel Development II
|
708 |
|
Chaired by: J. TISHKOFF, U.S. Air Force Office of Scientific Research, Arlington, VA
|
|
1330
AIAA-2009-4963
Improvement of Catalytic Decomposition of Ammonium Nitrate with New Bimetallic Catalysts
K. Farhat, W. Cong, Y. Batonneau, and C. Kappenstein, University of Poitiers, Poitiers, France
|
1400
AIAA-2009-4964
Pd- Pt/HZSM- 5 Coating Catalyst for Supercritical Cracking and Dehydrogenation of Endothermic Fuel
F. Meng, G. Liu, X. Zhang and L. Wang, Tianjin University, Tianjin, Tianjin, China (prc)
|
1430
AIAA-2009-4966
Mixtures of Nitrous Oxide and Oxygen (Nytrox) as Oxidizers for Rocket Propulsion Applications
A. Karabeyoglu, Space Propulsion Group Inc., Sunnyvale, CA
|
| Session
43-
SCP-2
|
Sensing and Measuring Technologies I
|
402 |
|
Chaired by: K. SEMEGA, U.S. Air Force Research Laboratory, Dayton, OH
|
|
1330
AIAA-2009-4971
Development of a Flight- Worthy TDLAS- Based Oxygen Sensor for HIFiRE- 1
A. Sappey, P. McCormick, P. Masterson, Q. Zhao, L. Sutherland, I. Smith, P. VanHoudr, J. Hannam, and D. Owenby, Zolo Technologies, Boulder, CO; S. Williams and T. Barhorst, U.S. Air Force Research Laboratory, Dayton, OH
|
1400
AIAA-2009-4972
Visualization of Propellant Behavior Inside Catalyst Thruster Using Neutron Radiography
K. Kushiki, H. Kagawa, T. Nagata, and K. Kajiwara, Japan Aerospace Exploration Agency, Tsukuba, Japan; and M. Matsubayashi, Japan Atomic Energy Agency, Tokai-mura, Japan
|
1430
AIAA-2009-4973
Wireless Flight Monitoring of Pressure in Hydrazine Tanks
T. Abensur, EADS Astrium Space Transportation, Les Mureaux, France; M. Kluge and A. Friedberger, EADS Innovation Works, Munich, Germany
|
1500
AIAA-2009-4974
High- Temperature Pressure Sensor Using Optical Stress Birefringence for Distributed Engine Control
J. Mackey, ASRC Aerospace Corporation, Cleveland, OH; M. Krasowski and N. Prokop, NASA Glenn Research Center, Cleveland, OH
|
| Session
44-
SR-3
|
Material Evaluation and Testing I
|
710 |
|
Chaired by: M. BERDOYES, Snecma, Cestas, France, and D. POE, Aerojet, Gainesville, VA
|
|
1330
AIAA-2009-4975
Uncertainty of Solid Propellant Burning Rate Measurements
J. Evans, A. Penton, and R. Frederick, University of Alabama in Huntsville, Huntsville, AL
|
1400
AIAA-2009-4977
Thermochemical Erosion Analysis for Carbon- Carbon Rocket Nozzles
D. Bianchi, F. Nasuti, and M. Onofri, Sapienza - Università di Roma, Rome, Italy; and E. Martelli, University of Naples “Federico II”, Aversa, Italy
|
| Session
45-
SR-4
|
Modeling and Simulation II
|
711 |
|
Chaired by: K. NAUMANN, Bayern-Chemie GmbH, Aschau, Germany, and F. BLOMSHIELD, Naval Air Warfare Center Weapons Division, China Lake, CA
|
|
1330
AIAA-2009-4979
Study of Two- Phase Loss in Gas- Solid Flow
J. Fan, C. Hu, G. He and Y. Yang, Northwestern Polytechnic University, Xi'an, ShaanXi, China (prc)
|
1400
AIAA-2009-4980
Comparison Between Different Pressurant Gases for Ignition Transient of P80 SRM
S. Zaghi, B. Favini, A. Attili, and M. Di Giacinto, Sapienza - Università di Roma, Rome, Italy; and F. Serraglia, ESA, Frascati, Italy
|
1430
AIAA-2009-4981
Numerical Simulations of Rocket Solid Motor Engine Ignition and Duct Overpressure Waves at Reduced Scale
J. Troyes, F. Vuillot, J. Varnier and P. Malbéqui, ONERA, Châtillon, France
|
1500
AIAA-2009-4978
On the Multiplicity of Planar Solutions for Axially Traveling Waves in Simulated SRMs
J. Majdalani, University of Tennessee Space Institute, Tullahoma, TN
|
| Session
46-
VS-2
|
Future Generation Space Transportation I
|
709 |
|
Chaired by: C. EHRLICH, ,, Calabasas, CA, and W. VAN LERBERGHE, The Aerospace Corporation, Los Angeles, CA
|
|
1330
AIAA-2009-4983
Variable Element Launch System
M. Bulman, Aerojet, Sacramento, CA
|
1400
AIAA-2009-5535
Hybrid Optimization Method for Multidisciplinary Design of Air Launched Satellite Launch Vehicle
A. Rafique, H. LinShu, Q. Zeeshan, A. Kamran, K. Nisar and X. Wang, Beijing University of Aeronautics and Astronautics (BUAA), Beijing, China (prc)
|
|
1600 - 1800 |
Innovation in In-Space Propulsion
|
Korbel 4 |
| Chaired by: J. HENDERSON, Lockheed Martin Corporation, Denver, CO, and B. SMITH, Aerojet, Redmond, WA |
Panelists:
Phil Garrison: Jet Propulsion Laboratory, Deputy Director, Engineering and Science
Dave Bair: Echostar, Senior Vice President, Space Programs and Operations
Col. James A. Maestas: U.S. Air Force, AFSPC MCSW/EN |
|
| Session
47-
APC-3
|
Unique Propulsion Systems I
|
707 |
|
Chaired by: J. ROBINSON, The Boeing Company, Huntington Beach, CA, and T. CHEN, NASA, Huntsville, AL
|
|
1600
AIAA-2009-4987
Transient Translating Gas Jets in Confined Channels
S. Wijeyakulasuriya and M. Nalim, Indiana University-Purdue University Indianapolis, Indianapolis, IN
|
1630
AIAA-2009-4989
Pedaling Aerospace Technology Across America
L. Mattson, Consultant, Manhattan Beach, CA
|
| Session
48-
ECS-1
|
Energetic Systems Applications and Analysis I
|
708 |
|
Chaired by: R. SAULSBERRY, White Sands Test Facility, Las Cruces, NM, and W. SANBORN, Pacific Scientific Energetic Materials Company, Chandler, AZ
|
|
1600
AIAA-2009-4990
WITHDRAWN
Numerical Investigation of Capillary Artery Evaporator in AMTEC Cell
C. Zhou, Harbin Institute of Technology, Harbin, China (prc); Z. Ma and H. Zheng, Harbin Engineering University, Harbin, China (prc)
|
1630
AIAA-2009-4991
Development of a Pyrotechnic Cutter to Cut 2- Inch Diameter Vectran Line
K. LeVoir and A. Konst, Technical Ordinance, Inc., St. Bonifacius, MN
|
1700
AIAA-2009-4992
Implications of Dynamic Pressure Transducer Mounting Variations on Measurements in Pyrotechnic Test Apparatus
A. Dibbern, NASA Kennedy Space Center, Kennedy Space Center, FL; W. Sipes, Pyrotechnic Consultant, Canyon Country, CA; M. Hagopian, NASA Goddard Space Flight Center, Greenbelt, MD; S. McDougle, MEI Technologies, Inc., Las Cruces, NM; R. Saulsberry, NASA White Sands Test Facility, Las Cruces, NM; and J. Crisafulli, NASA Kennedy Space Center, Kennedy Space Center, FL
|
| Session
26-
EP-4
|
Electric Propulsion Thruster Wear and Life Assessment
|
505 |
|
Chaired by: D. HERMAN, ASRC Aerospace, Greenbelt, MD, and S. GILDEA, Massachusetts Institute of Technology, Cambridge, MA
|
|
1600
AIAA-2009-4920
Ion Thruster Performance Impacts Due to Cathode Wear
D. Goebel, J. Polk, and I. Mikellides, Jet Propulsion Laboratory, Pasadena, CA
|
1630
AIAA-2009-5095
Lifetime Qualification Standard for Electric Thrusters
J. Brophy and J. Polk, Jet Propulsion Laboratory, Pasadena, CA; J. Dankanich, Gray Research Inc., Cleveland, OH
|
| Session
49-
EP-7
|
Cathode Characterization and Thruster Performance Coupling
|
507 |
|
Chaired by: W. HARGUS, Air Force Research Laboratory, Edwards AFB, CA, and K. XU, Georgia Institute of Technology, Atlanta, GA
|
|
1600
AIAA-2009-5003
Experimental Characterization of Carbon Nanotube Field Emission Cathode Lifetime
L. Williams and M. Walker, Georgia Institute of Technology, Atlanta, GA; V. Kumsomboone and W. Ready, Georgia Tech Research Institute, Atlanta, GA
|
1630
AIAA-2009-5004
Hall- Effect Thruster - - Cathode Coupling Part I: Efficiency Improvements from an Extended Outer Pole
J. Sommerville and L. King, Michigan Technological University, Houghton, MI
|
1700
AIAA-2009-5005
Hall- Effect Thruster - - Cathode Coupling Part II: Ion Beam and Near- Field Plume
J. Sommerville and L. King, Michigan Technological University, Houghton, MI
|
| Session
52-
GT-3
|
Ground Test III
|
401 |
|
Chaired by: W. HAWKINS, Miratek Corporation, Arnold AFB, TN, and V. CANACCI, Jacobs Technology Inc, Westlake, OH
|
|
1600
AIAA-2009-5006
Design Evolution and Verification of the A- 3 Chemical Steam Generator
C. Kirchner, NASA Stennis Space Center, Stennis Space Center, MS
|
1630
AIAA-2009-5007
Design and Activation of a LOX/GH Chemical Steam Generator
G. Saunders, Jacobs Technology, Inc., Stennis Space Center, MS; C. Mulkey and S. Taylor, NASA, Stennis Space Center, MS
|
1700
AIAA-2009-5008
Analysis of Diffuser and Ejector Performance in a High Altitude Test Facility
R. Manikanda Kumaran, K. Vivekanand and T. Sundararajan, Indian Institute of Technology Madras, Chennai, India; S. Balasubramanian and D. Raja Manohar, Indian Space Research Organization, Mahendragiri, India
|
| Session
53-
GT-4
|
Ground Test IV
|
709 |
|
Chaired by: B. MESSER, NASA Stennis Space Center, Stennis Space Center, MS
|
|
1600
AIAA-2009-5009
An Overview of Follow- On Testing Activities of the A- 3 Subscale Diffuser Test Project
J. Ryan, NASA Stennis Space Center, Stennis Space Center, MS
|
1630
AIAA-2009-5010
A3 Subscale Diffuser Test Article Design
G. Saunders, Jacobs Technology, Inc., Stennis Space Center, MS
|
1700
AIAA-2009-5011
Error Analysis of the Surface Heat Flux Calculation for the A3 Subscale Supersonic Diffuser
J. Yen, G. Saunders and D. Wagner, Jacobs Technology Inc., Tullahoma, TN
|
1730
AIAA-2009-5012
Transient Heat Load Estimate for the A3 Subscale Supersonic Rocket Diffuser Using Surface Temperature Measurement
J. Yen, G. Saunders and D. Wagner, Jacobs Technology Inc., Tullahoma, TN
|
| Session
54-
GTE-5
|
Combustors III - Combustion Processes
|
405 |
|
Chaired by: J. SMITH, QuEST-ASE, Inc., Cincinnati, OH
|
|
1600
AIAA-2009-5014
Combustion Instability in a Turbulent Liquid- Fueled Swirl- Stabilized LDI Combustor
T. Yi and D. Santavicca, Pennsylvania State University, State College, PA
|
1630
AIAA-2009-5015
Pilot Flame Impact on Flow Fields and Combustion Performances in Swirl Inducing Burner
A. Emara, A. Lacarelle, and C. Paschereit, Institute of Fluid Mechanics and Engineering Acoustics, Berlin, Germany
|
1700
AIAA-2009-5016
Unsteady Flow Structures of a Counter- Rotating Swirl Cup
Y. Lin, Y. Lin, and G. Liu, Beihang University, Beijing, China (prc)
|
| Session
55-
GTE-6
|
Turbines - Gas Turbine Modeling
|
404 |
|
Chaired by: N. MADAVAN, NASA Ames Reserch Center, Moffett Field, CA
|
|
1600
AIAA-2009-5017
Coupled Component, Full Engine Simulation of a Gas Turbine Engine
R. Claus, NASA Glenn Research Center, Cleveland, OH; S. Townsend, Artic Slopes Regional Corp., Cleveland, OH; T. Lavelle, NASA Glenn Research Center, Cleveland, OH; and M. Turner, University of Cincinnati, Cincinnati, OH
|
1630
AIAA-2009-5018
Modeling of the Performance of a F100- PW229 Equivalent Engine under Sea- Level Static Conditions
A. Lee, DSO National Laboratories, London, Great Britain; R. Singh and S. Probert, Cranfield University, London, Great Britain
|
1700
AIAA-2009-5019
WITHDRAWN
Defect Diagnostics of Gas Turbine Engine Using SVM and RCGA Based ANN Algorithms in Off- Design Condition
D. Seo, J. Jang, T. Roh, and D. Choi, Inha University, Incheon, South Korea
|
| Session
56-
HIS-2
|
History II
|
710 |
|
|
|
1600
AIAA-2009-5022
Origins of Scientific Aircraft Navigation
J. Barata, A. Mendes, C. Morgado, F. Neves, and A. Silva, Universidade Beira Interior, Covilhã, Portugal
|
1630
AIAA-2009-5023
Review of Historic and Modern Cyclogyro Design
C. Boirum and S. Post, Bradley University, Peoria, IL
|
| Session
57-
HR-3
|
Modeling and Analysis of Hybrid Rocket Motor Internal Ballistics I
|
712 |
|
Chaired by: A. PERETZ, RAFAEL Armament Development Authority Ltd., Haifa, Israel, and B. EVANS, Pennsylvania State University, University Park, PA
|
|
1600
AIAA-2009-5025
Head- End Injected Swirling Gas Flow in a Chamber
M. Motoe, University of Tokai, Hiratuka, Japan; and T. Shimada, Japan Aerospace Exploration Agency, Sagamihara, Japan
|
| Session
58-
HYP-6
|
Scramjet Engines - Experimental Investigations I
|
407 |
|
Chaired by: R. CHASE, ANSER, Gainesville, VA, and K. BOWCUTT, The Boeing Company, Aliso Viejo, CA
|
|
1600
AIAA-2009-5028
Study on the Operability of Cavity Flameholders inside a Scramjet Combustor
K. Lin and C. Tam, Taitech, Inc., Beavercreek, OH; and K. Jackson, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
|
1630
AIAA-2009-5029
The HIFiRE Flight 2 Experiment: An Overview and Status Update
K. Jackson, M. Gruber and T. Barhorst, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
|
1700
AIAA-2009-5030
Dual Cavity Scramjet Operability and Performance Study
M. Collatz, M. Gruber, and D. Olmstead, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; R. Branam, U.S. Air Force Institute of Technology, Wright-Patterson AFB, OH; K. Lin and C. Tam, Taitech, Inc, Beavercreek, OH
|
| Session
59-
HYP-7
|
Supersonic Facilities/Instrumentation
|
406 |
|
Chaired by: D. GARRARD, Aerospace Testing Alliance, Arnold AFB, TN, and C. GOYNE, University of Virginia, Charlottesville, VA
|
|
1600
AIAA-2009-5032
Instrumentation and Performance Analysis Plans for the HIFiRE Flight 2 Experiment
M. Gruber, K. Jackson, D. Eklund, and T. Barhorst, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; N. Hass and A. Storch, NASA Langley Research Center, Hampton, VA; and J. Liu, Taitech, Inc., Dayton, OH
|
1630
AIAA-2009-5033
Optical Measurements of Pressure and Shear on a Strut in Supersonic Flow
J. Crafton, S. Fonov, and K. Hsu, Innovative Scientific Solutions, Inc., Dayton, OH; C. Carter and M. Gruber, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
|
1700
AIAA-2009-5034
Development of a Rotating Probe System for Supersonic Combustion Experiments
S. Smith and M. Gruber, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; T. Mathur, Innovative Scientific Solutions, Inc., Dayton, OH; C. Tam, Taitech, Inc., Beavercreek, OH; R. Ryman and J. Diemer, Innovative Scientific Solutions, Inc., Dayton, OH
|
1730
AIAA-2009-5035
Development and Calibration of an Axisymmetric Direct- Connect Supersonic- Combustion Flowpath
S. Smith, M. Gruber, R. Steiner, and M. Collatz, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; and T. Mathur, Innovative Scientific Solutions, Inc., Dayton, OH
|
| Session
60-
LP-9
|
Components: Injectors I
|
703 |
|
Chaired by: P. GLOYER, GT Labs, Tullahoma, TN, and S. FISHER
|
|
1600
AIAA-2009-5040
Numerical Design Studies on Internal Flow Characteristics of LOX/CH4 Swirl Injector
M. Balasubramanyam and C. Chen, University of Alabama in Huntsville, Huntsville, AL
|
1630
AIAA-2009-5041
Liquid Sheet Dynamics and Primary Breakup Characteristics at Impingement Type Injector
C. Inoue, T. Watanabe and T. Himeno, University of Tokyo, Tokyo, Japan
|
1700
AIAA-2009-5042
Large Flow Rate Shear- Coaxial Gas- Gas Injector
X. Wang, G. Cai, Y. Gao, and P. Jin, Beijing University of Aeronautics and Astronautics, Beijing, China (prc)
|
1730
AIAA-2009-5043
Forced Excitation of Swirl Injectors Using a Hydro- Mechanical Pulsator
B. Ahn, M. Ismailov, and S. Heister, Purdue University, West Lafayette, IN
|
| Session
61-
LP-10
|
Modeling and Simulation: Propellant Systems
|
704 |
|
Chaired by: S. CHIANESE, Northrop Grumman Space Technology, Redondo Beach, CA, and K. KREINER, The Boeing Company, El Segundo, CA
|
|
1600
AIAA-2009-5044
Hydrazine and Di- Nitrogen Tetroxide Combustion Model Inside Film- Cooled Bipropellant Thruster
K. Ohminami, University of Tokyo, Tokyo, Japan; S. Sawai and K. Uesugi, ISAS/JAEA, Kanagawa, Japan; N. Yamanish, JAXA, Ibaraki, Japan; and M. Koshi, University of Tokyo, Tokyo, Japan
|
1630
AIAA-2009-5045
Numerical Simulations of Gel Propellant Flow Through Orifices
C. Yoon, S. Heister, G. Xia and C. Merkle, Purdue University, West Lafayette, IN
|
| Session
62-
LP-11
|
Systems: Engines and Demonstrations II
|
705 |
|
Chaired by: C. ENGELBRECHT, Johns Hopkins University, Applied Physics Laboratory, Laurel, MD, and B. GORIN, ARDE, Gaithersburg, MD
|
|
1600
AIAA-2009-5036
From Qualification to 4th Year of Exploitation: HM7B on Ariane 5 ECA
A. Lekeux, Centre National d’Études Spatiales, Evry, France; J. Pander, Snecma, Vernon, France; and J. Mansouri, Arianespace, Evry, France
|
1630
AIAA-2009-5038
Progress of the Vinci Engine System Engineering
P. Alliot, C. Fiorentino, P. James, and J. Follet, Snecma, Vernon, France; J. Bahu and J. Bahu, Centre National d’Etudes Spatiales, Evry, France; and J. Caruana, ESA, Paris, France
|
| Session
63-
NFF-3
|
Future Flight II
|
702 |
|
Chaired by: G. MEHOLIC, The Aerospace Corporation, El Segundo, CA, and B. PALASZEWSKI, NASA Glenn Research Center, Cleveland, OH
|
|
1600
AIAA-2009-5047
Design of a Lean- Premixed Hydrogen Combustor for a Gas Turbine Engine
J. Farina and M. Perry, Virginia Polytechnic Institute and State University, Blacksburg, VA; S. LePera, U. Vandsburger, and W. O'Brian, Virginia Polytechnic Institute, Blacksburg, VA
|
1630
AIAA-2009-5048
Instrumentation, Modeling, and Testing of a Gas Turbine Engine Using Lean- Premixed Hydrogen Combustion
M. Perry and J. Farina, Virginia Polytechnic Institute and State University, Blacksburg, VA; S. LePera, W. O'Brian, and U. Vandsburger, Virginia Polytechnic Institute, Blacksburg, VA
|
1700
AIAA-2009-5049
Experiment Research of Ramjet with Cavity- Based Flameholder
Q. Li, Y. Pan, J. Tan, and Z. Wang, National University of Defense Technology, Changsha, China (prc)
|
1730
AIAA-2009-5050
A Novel Turbo- Solid Engine
M. Ziraksaz, Islamic Azad University, Tehran, Iran
|
| Session
64-
PC-5
|
Combustion Diagnostics
|
303 |
|
Chaired by: C. CARTER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
|
|
1600
AIAA-2009-5051
Unsteady Chemiluminescence Imaging of a Swirl Coaxial Injector
R. Ikard, J. Brooks and R. Frederick, UAHuntsville Propulsion Research Center, Huntsville, AL
|
1630
AIAA-2009-5052
Dual- Pump CARS Temperature and Major Species Concentration Measurements in a Gas Turbine Combustor Facility
M. Thariyan, A. Bhuiyan, N. Chai, S. Naik, R. Lucht, and J. Gore, Purdue University, West Lafayette, IN
|
1700
AIAA-2009-5053
Size Distribution Effects in Heterogeneous Shock Tube Burntime Experiments
P. Lynch, H. Krier, and N. Glumac, University of Illinois, Urbana, IL
|
1730
AIAA-2009-5054
Assessment of the Application of Hydroxyl Tagging Velocimetry (HTV) to Rocket Engine Exhausts
M. Ramsey, T. Folk, A. Perkins, and R. Pitz, Vanderbilt University, Nashville, TN; and T. Jenkins, MetroLaser, Inc., Irvine, CA
|
| Session
65-
PC-6
|
Fundamental Combustion Processes III
|
304 |
|
Chaired by: P. PENKO, Ohio State University, Berea, OH
|
|
1600
AIAA-2009-5056
Mixing Layer Characterization Due to the Impulsive Dispersion of Dense Solid Particle Clouds
K. Balakrishnan and S. Menon, Georgia Institute of Technology, Atlanta, GA
|
1630
AIAA-2009-5058
Flame Response to Equivalence Ratio Fluctuations – Relationship Between Chemiluminescence and Heat Release
S. Shreekrishna and T. Lieuwen, Georgia Institute of Technology, Atlanta, GA
|
| Session
66-
SCP-3
|
Integrated Modeling and Simulation I
|
403 |
|
Chaired by: J. DALTON, Avetec, Springfield, OH, and M. CASPERMEYER, Jansens Aircraft Systems Controls Inc., Tempe, AZ
|
|
1600
AIAA-2009-4887
A New Helicopter Transmission Model for Condition- Based Maintenance Technologies Using First Principles
D. Stringer, Vehicle Technology Directorate Army Research Lab, Cleveland, OH; P. Sheth and P. Allaire, University of Virginia, Charlottesville, VA
|
| Session
67-
SCP-4
|
Sensing and Measuring Technologies II
|
402 |
|
Chaired by: K. SEMEGA, U.S. Air Force Research Laboratory, Dayton, OH, and J. MILLER, NASA Marshall Space Flight Center, Huntsville, AL
|
|
1600
AIAA-2009-5063
Design and Testing of a Wavelength- Multiplexed TDLAS Sensor for Augmentor Performance Using an Immersed Water- Cooled Probe
A. Sappey, P. Masterson, and Q. Zhao, Zolo Technologies, Boulder, CO; B. Kiel, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; D. Knaus, R. Kazeta, and P. Magari, Creare, Inc., Hanover, NH
|
1630
AIAA-2009-5064
TDLAS Measurements of Multiple Species and Temperature of Augmented Aeroengines
A. Sappey, P. Masterson, Q. Zhao, and E. Huelson, Zolo Technologies, Boulder, CO; and K. Barlow, Naval Air Systems Command, Pax River, MD
|
1700
AIAA-2009-5065
Laser- Based Mass Flow Rate Sensor Onboard HFiRE Flight 1
S. Chen, M. Paige, and J. Silver, Southwest Sciences, Inc., Santa Fe, NM; S. Williams and T. Barhorst, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH
|
1730
AIAA-2009-5066
Thin Film Heat Flux Sensor Development for Ceramic Matrix Composite (CMC) Systems
J. Wrbanek, G. Fralick, and G. Hunter, NASA Glenn Research Center, Cleveland, OH; D. Zhu, U.S. Army Research Laboratory, Cleveland, OH; K. Laster, Sierra Lobo Inc., Cleveland, OH; J. Gonzalez, Gilcrest Electric, Cleveland, OH; and O. Gregory, University of Rhode Island, Kingston, RI
|
1800
AIAA-2009-5067
Development of an In- Flight Non- Intrusive Mass Capture System
T. Barhorst and S. Williams, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; S. Chen, M. Paige, and J. Silver, Southwest Sciences, Inc., Santa Fe, NM; A. Sappey, P. McCormick, P. Masterson, Q. Zhao, L. Sutherland, I. Smith, P. VanHoudt, J. Hannam, and D. Owenby, Zolo Technologies, Boulder, CO
|
|
1600 - 1800 |
Industry Challenges for the Next Generation Tactical Missile Propulsion System
|
601/603 |
Chaired by: Dr. Jamie Neidert, U.S. Army Aviation and Missile Research Development
Panelists:
Mr. Kevin Maikis, NAMMO/Talley
Dr. Carl Shanholtz, Raytheon
Mr. Ken Tappe, ATK/ABL
Mr. Frank Tse, NSWC/Indian Head
Mr. Bryan Waltz, Aerojet
Dr. Karl Naumann, Bayern-Chemie
Mr. Jim Fleming, Roxel UK
Mr. Jim Hurdle, General Dynamics Armament and Technical Products
|
|
| Session
68-
NFF-4
|
Breakthrough Propulsion Physics
|
601/603 |
|
Chaired by: M. MILLIS, NASA Glenn Research Center, Cleveland, OH, and B. CASSENTI, University of Connecticut, Storrs, CT
|
|
1900
Oral Presentation
Advanced Space Propulsion Concepts for Interstellar Travel Part 2: The New Paradigm in Propulsion Science
G. Meholic, The Aerospace Corporation, El Segundo, CA
|
1945
AIAA-2009-5069
Gravitational Field Propulsion
J. Hauser, University of Applied Sciences, Salzgitter, Germany; and W. Dröscher, Institut für Grenzgebiete der Wissenschaft, Innsbruck, Austria
|
2030
AIAA-2009-5070
Null Findings on Electromagnetic Inertia Thrusting Experiments Using a Torsion Pendulum
H. Brito, R. Marini, and E. Galian, Instituto Universitario Aeronautico, Cordoba, Argentina
|
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