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Program For Monday, 12-Jul-2004
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0800 - 0900 |
Plenary Session: Keynote Address
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Floridian Ballroom |
| The 2004 Joint Propulsion Conference Keynote Address will be given jointly by:
Walter Bylciw, President, Pratt & Whitney Space Propulsion and Russian Operations;
James Kennedy, Director, NASA John F. Kennedy Space Center; and
George Ebbs, President, Embry-Riddle Aeronautical University. |
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0900 - 1100 |
Shuttle Return to Flight – Status and Implementation Plans
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Floridian Ballroom |
As the safe return of the Space Shuttle Program to flight approaches, the world continues to closely monitor its progress. This panel session will bring together a NASA Space Shuttle Program Deputy, an astronaut, a U.S. Senator (invited) and industry officials to discuss their perspectives on the resumption of shuttle flights. Aviation Week & Space Technology Senior Editor Craig Covault will moderate this panel session and bring burning issues to the forefront.
Panelists:
Michael C. Kostelnik (ret. Air Force Major General), NASA, Deputy Associate Administrator for Shuttle and International Space Station Programs
Bob Crippen, Former Astronaut and Former Director of Kennedy Space Center
Howard DeCastro, United Space Alliance, Vice President, Program Manager
U.S. Senator Bill Nelson (invited) |
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| Session
1-
ABP-1
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Air Breathing Propulsion for High Speed Flight
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316 |
|
Chaired by: J. DATKO, Air Force Research Laboratory, Wright-Patterson AFB, OH, and L. BURNS, Universal Technology Corporation, Springboro, OH
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|
| Session
2-
ABP-2
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Engine Systems - Analysis & Test
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317 |
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Chaired by: C. ARANA and B. KIEL, Air Force Research Laboratory, Wright-Patterson AFB, OH
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0900
AIAA-2004-3306
Experimental Investigation and Numerical Simulation of Secondary Chamber Flow in SDR
J. Hu, Z. Xia, Z. Wang, J. Guo and W. Zhang, National University of Defense Technology, Changsha, China (prc)
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0930
AIAA-2004-3307
Computational and Experimental Study of NOx Formation in Hydrogen- Fueled Pulse Detonation Engines
S. Yungster and K. Radhakrishnan, Ohio Aerospace Institute, Cleveland, OH; K. Breisacher, NASA Glenn Research Center, Cleveland, OH
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1000
AIAA-2004-3308
Heat Exchanger Influence on Off- Design Performances of Regenerative Jet Engines
R. Andriani and U. Ghezzi, Polytechnic of Milan, Milan, Italy
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1030
AIAA-2004-3310
Technology Demonstration of ATR with a Ramjet Test Facility
Y. Shimada and K. Miyata, Technical Research and Development Institute Japan Defense Agency, Tachikawa, Tokyo, Japan
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1100
AIAA-2004-3311
Performance Cycle Analysis of a Two- Spool, Separate- Exhaust Turbofan with Interstage Turbine Burner
K. Liew, E. Urip and S. Yang, Michigan Technological University, Houghton, MI; J. Mattingly, Mattingly Consulting, Bothell, WA; C. Marek, NASA Glenn, Cleveland, OH
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| Session
3-
ABP-3
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Propulsion System Development I
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318 |
|
Chaired by: R. BRUCKNER, NASA Glenn Research Center, Cleveland, OH, and J. SHEELEY, Aerospace Testing Alliance/AEDC, Arnold AFB, TN
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0900
AIAA-2004-3314
Optimum Propulsion System Selection for Long Range Civil Transport Aircraft
S. Sane and P. Tagade, Indian Institute of Technology Bombay, Mumbai, India; V. Sanghi, Infotech Enterprises, Bangalore, India
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0930
AIAA-2004-3315
Initial Development and Calibration of a Design Guide for Jet Noise Reduction
J. Stone, E. Krejsa, B. Clark and J. Berton, Modern Technologies Corporation, Middleburg Heights, OH
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1000
AIAA-2004-4227
Technological Developments in European Programs Aimed at Reducing Air Transport Noise and Emissions
A. Coutrot, Snecma Group, Paris, France
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1030
AIAA-2004-4189
A Propulsion System Analysis of Oil Free Turbomachinery for Aviation Turbofan Engines
R. Bruckner, NASA Glenn Research Center, Cleveland, OH
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1100
AIAA-2004-4204
Development of Mixing Analogy for Investigation of Injectant Mixing in Supersonic Flow
A. Gonor, M. Gilinsky and V. Khaikine, Hampton University, Hampton, VA; I. Blankson, NASA Glenn Research Center, Cleveland, OH
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1130
AIAA-2004-4208
A Study on New Ramp Injectors with Slotted Nozzle for Improvement of Supersonic Mixing
K. Inoue and S. Aso, Kyushu University, Fukuoka, Japan
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| Session
4-
ECS-1
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Energetic Component Performance
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209 |
|
Chaired by: B. NEYER, PerkinElmer Optoelectronics, Miamisburg, OH, and R. SAULSBERRY, White Sands Testing Facility, Las Cruces, NM
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|
0900
AIAA-2004-3318
Exploding Pyrotechnic Myths Part I: Reliable SMDC Energy Transfer
J. Glass, PSEMC, Hollister, CA
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| Session
5-
EDU-1
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University Propulsion Programs
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304 |
|
Chaired by: R. FREDERICK, University of Alabama in Huntsville, Huntsville, AL, and R. SANTORO, Pennsylvania State University, University Park, PA
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0900
AIAA-2004-3322
University Propulsion Programs at Penn State
R. Santoro, Pennsylvania State University, University Park, PA
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0930
AIAA-2004-3323
University Propulsion Programs at the University of Alabama in Huntsville
C. Hawk and R. Frederick, University of Alabama in Huntsville, Huntsville, AL
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1000
AIAA-2004-3324
Propulsion Educational Programs and Facilities at Purdue University
S. Heister, S. Meyer, W. Anderson, I. Hrbud and C. Merkle, Purdue University, West Lafayette, IN
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1030
AIAA-2004-3326
University Propulsion Programs at Auburn University
W. Foster, R. Hartfield and R. Jenkins, Auburn University, Auburn, AL
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1100
AIAA-2004-3325
University Propulsion Programs at Georgia Tech
J. Jagoda, Georgia Institute of Technology, Atlanta, GA
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| Session
6-
EP-1
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Electric Propulsion Overview
|
Palm A & B |
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Chaired by: F. WILSON, Aerojet, Redmond, WA
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|
0900
AIAA-2004-3328
An Overview of Electric Propulsion Activities at NASA
J. Dunning, J. Hamley, R. Jankovsky and S. Oleson, NASA Glenn, Cleveland, OH
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0930
AIAA-2004-3329
Electric Propulsion in ESA
G. Saccoccia, European Space Agency, Noordwijk, The Netherlands; J. Gonzalez, ESTEC, Noordwijk, The Netherlands
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1000
AIAA-2004-3330
Overview of Electric Propulsion Activities in Russia
S. Tverdokhlebov, A. Semenkin, V. Garkusha, A. Korsun, E. Tverdokhlebova and G. Karabadxhak, TSNIIMASH, Moscow, Russia
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1030
AIAA-2004-3331
Overview of Major U.S. Industrial Electric Propulsion Programs
R. Myers, Aerojet-Redmond, Redmond, WA
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1100
AIAA-2004-3332
Review of the EP Activities of US Academia
L. King, Michigan Technological University, Houghton, MI
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1130
AIAA-2004-3334
A Critical History of Electric Propulsion: The First Fifty Years (1906- 1956)
E. Choueiri, Princeton University, Princeton, , NJ
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| Session
7-
HIS-1
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Space and Aviation History
|
220 |
|
Chaired by: J. BLANTON, GE Aircraft Engines, Cincinnati, OH, and I. HALLIWELL, Modern Technologies Corporation, Middleburg Heights, OH
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|
0900
AIAA-2004-3335
The Persistent Occurence of Number Three in the History of Space Mechanics
M. Ananthasayanam, Indian Institute of Science, Bangalore, India
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0930
AIAA-2004-3337
The Long and Illustrious Life of the Aerobee Rocket - From Probing the Earth's Atmosphere to the Edge of Space to Evaluating Underwater Launch Concepts
C. Ehresman, Purdue University, West Lafayette, IN; C. Hawk, Aerojet, Azusa, CA
|
1000
AIAA-2004-3339
Leading Russian Liquid Rocket Engines Company (to 75th Anniversary of NPO Energomash)
B. Katorgin, V. Chvanov, V. Sudakov and V. Rakhmanin, NPO Energomash, Khimky, Moscow area, Russia
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1030
AIAA-2004-3336
The History of Hurricane Mesa Test Facility
H. McSpadden and R. Higgins, Goodrich/UPCO, Phoenix, AZ
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1100
AIAA-2004-4228
A Brief History of Rolls- Royce in the United States
D. Jensen and M. Evans, Rolls-Royce Heritage Trust, Indianapolis, IN
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| Session
8-
HYP-1
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Ramjet/Scramjet Engine System Analysis Design & Test
|
223 |
|
Chaired by: R. MERCIER, Air Force Research Laboratory, Wright-Patterson AFB, OH, and R. FAULKNER, Pratt & Whitney Space Propulsion, West Palm Beach, FL
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|
0900
AIAA-2004-3341
Gas- sampling Survey from Exhaust Flows in Scramjet Engines at Mach- 6 Flight Condition
T. Hiraiwa, K. Kobayashi, S. Tomioka and M. Izumikawa, Japan Aerospace Exploration Agency, Kakuda, Miyagi, Japan; S. Watanabe, Kakuda Research Center, Kakuda, Miyagi, Japan
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0930
AIAA-2004-3343
Scramjet Optimization for Maximum Off- Design Performance
R. Starkey, University of Maryland, College Park, MD
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1000
AIAA-2004-3344
LEA Flight Test Program - Status in 2004
F. Falempin, MBDA, Chatillon, France; L. Serre, ONERA, Toulouse, France
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1030
AIAA-2004-3345
Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG and Comparison with Flight Data
A. Gardner, DLR German Aerospace Center, Göttingen, Germany; J. Steelant, ESA/ESTEC, Noordwijk, The Netherlands; A. Paull, University of Queensland, St. Lucia, Australia; K. Hannemann, DLR German Aerospace Center, Göttingen, Germany
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| Session
9-
ISP-1
|
Tether and Plasma Propulsion
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305 |
|
Chaired by: J. BONOMETTI, NASA Marshall Space Flight Center, Huntsville, AL, and B. GILCHRIST, University of Michigan, Ann Arbor, MI
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|
0900
AIAA-2004-3501
Review of the ProSEDS Electrodynamic Tether Mission Development
J. Vaughn and L. Curtis, NASA Marshall, Huntsville, AL; B. Gilchrist, Univ. of Michigan, Ann Arbor, MI; S. Bilen, Pennsylvania State University, University Park, PA; E. Lorenzini, Smithsonian Astrophysical Observatory, Cambridge, MA
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0930
AIAA-2004-3351
Increasing Launch Site Capability Using a Motorized Momentum Exchange Tether
C. Draper, D. McKenzie and M. Cartmell, University of Glasgow, Glasgow, Great Britain
|
1000
AIAA-2004-3352
Assessing the Motorized Momentum Exchange Tether’s Operational Lifetime: The Multi- Dimensional Casualty Area Concept
C. Draper and M. Cartmell, University of Glasgow, Glasgow, Great Britain
|
1030
AIAA-2004-3502
Numerical Study on Thrust Production Mechanism of a Magnetoplasma Sail
R. Asahi, University of Tsukuba, Tsukuba, Japan; I. Funaki, H. Ogawa, H. Yamakawa and K. Fujita, Japan Aerospace Exploration Agency, Sagamihara, Japan; Y. Nakayama, National Defense Academy, Yokosuka, Japan
|
1100
AIAA-2004-3495
Electron Emission for Electrodynamic Tether Systems in Space
K. Fuhrhop, D. Morris and B. Gilchrist, University of Michigan, Ann Arbor, MI
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| Session
10-
LP-1
|
Booster and Main Engines I
|
221 |
|
Chaired by: R. BALLARD, NASA Marshall Space Flight Center, Huntsville, AL, and W. ANDERSON, Purdue University, West Lafayette, IN
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|
0900
AIAA-2004-3353
Snecma High Thrust Cryogenic Engines for the Next 20 Years
J. Couteau, A. Beaurain and A. Souchier, Snecma Moteurs, Vernon, France
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0930
AIAA-2004-3354
Development and Flight- Testing of Liquid Propellant Aerospike Engines
E. Besnard, California State University, Long Beach, CA; J. Garvey, Garvey Spacecraft Corp., Huntington Beach, CA
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1000
AIAA-2004-3356
A Comparison Between Two Possible Thermodynamic Schemes for Reusable LOX/LCH4 Engines
L. Boccaletto, Centre National d'Etudes Spatiales, Evry, France
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1030
AIAA-2004-3358
Using Pressure- Fed Propulsion Technology to Lower Space Transportation Costs
S. Chakroborty and T. Bauer, Microcosm Inc., El Segundo, CA
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| Session
11-
LP-2
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Liquid Rocket Engine Combustion Devices
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222 |
|
Chaired by: J. CALVIGNAC, Northrop Grumman Space Technology, Redondo Beach, CA, and B. GORIN, ARDE Inc, Gaithersburg, MD
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0900
AIAA-2004-3359
Cold Flow Analysis of a Vortex Chamber Engine for Gelled Propellant Combustor Applications
M. Anderson and C. Rom, University of Wisconsin - Madison, Madison, WI; M. Chiaverini, Obitec, Madison, WI
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0930
AIAA-2004-3360
Liquid Film Cooling Using Swirl in Rocket Combustors
Y. Yu, R. Schuff and W. Anderson, Purdue University, West Lafayette, IN
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1000
AIAA-2004-3363
Development of Fuel Rich Gas Generator for 10 ton f Liquid Rocket Engine
S. Kwon, C. Lee and J. Lee, Konkuk University, Seoul, South Korea
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1030
AIAA-2004-3364
Stability Rating Tests of KSR- III Baffled Chamber Using Pulse Gun
H. Kim, K. Lee, S. Seo, Y. Han, W. Seol and S. Lee, Korea Aerospace Research Institute, Daejeon, South Korea
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| Session
12-
LPCS-1
|
Yesterday’s Methods, Today’s Materials, and Tomorrow’s Spacecraft
|
203/204 |
|
Chaired by: K. RATHGEBER, Honeywell, Las Cruces, NM, and M. MCPHERSON, Aerojet, Sacramento, CA
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|
| Session
13-
PC-1
|
Fundamental Combustion Processes I
|
207 |
|
Chaired by: Y. JU, Princeton University, Princeton, NJ, and P. PENKO, NASA Glenn Research Center, Cleveland, OH
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|
0900
AIAA-2004-3370
A Shock- Tube Study of the Oxidation of C2H6/O2/AR and C2H6/SiH4/O2/AR Mixtures
J. deVries, J. Hall and E. Petersen, University of Central Florida, Orlando, FL; D. Kalitan and M. Rickard, The Aerospace Corporation, El Segundo, CA
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0930
AIAA-2004-3371
Flammability Limits of Hydrogen and Oxygen in Confined Spaces
Y. Villegas, M. Moser and H. Coleman, University of Alabama in Huntsville, Huntsville, AL
|
1000
AIAA-2004-3373
A Model for Thermal Decomposition of Hydrogen Peroxide
J. Corpening, S. Heister and W. Anderson, Purdue University, West Lafayette, IN; B. Austin, IN Space LC, West Lafayette, IN
|
1030
AIAA-2004-3374
Oxygen- Enhanced High Temperature Laminar Coflow Flames
Z. Cheng and R. Pitz, Vanderbilt University, Nashville, TN; B. Bennett and M. Smooke, Yale University, New Haven, CT
|
1100
AIAA-2004-3375
Simulation of Flame Spread and Turbulent Separated Flows in Solid Rockets
V. R.Sanalkumar and H. D.Kim, Andong National University, Andong, South Korea; C. Unnikrishnan, Vikram Sarabhai Space Centre, Trivandrum, India; B. N.Raghunandan, Indian Institute of Science, Bangalore, India; T. Setoguchi, Saga University, Saga, Japan
|
1130
AIAA-2004-3372
Combustion of Periodic Laminate Propellants
R. Fitzgerald and M. Brewster, University of Illinois at Urbana-Champaign, Urbana, IL
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| Session
14-
PC-2
|
Spray Combustion
|
208 |
|
Chaired by: M. ANAND, Rolls-Royce, Indianapolis, IN, and H. MONGIA, GE Aircraft Engines, Cincinnati, OH
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|
0900
AIAA-2004-3378
Measurements of Spray Characteristics Produced by Effervescent Atomizers
A. Mostafa, M. Fouad, M. Enayet and S. Osman, Cairo University, Cario, Egypt
|
0930
AIAA-2004-3379
Characteristics of Sprays Produced by a High Shear Atomizer
A. Mostafa, Cario University, Cario, Egypt
|
1000
AIAA-2004-3381
LES of Supercritical Combustion in a Gas Turbine Engine
N. Tramecourt and S. Menon, Georgia Institute of Technology, Atlanta, GA; J. Amaya, , Atlanta, GA
|
1030
AIAA-2004-3382
Effect of Variable Properties in Modeling the Spray Droplet Burning in Mixed Convective Environment
V. Raghavan, V. Babu and T. Sundararajan, Indian Institute of Technology Madras, Chennai, India
|
1100
AIAA-2004-3383
Controllable Injection for Supercritical Combustion
M. Lal and M. Oljaca, nGImat Co., Atlanta, GA; E. Lubarsky, D. Shcherbik, A. Bibik and S. Menon, Georgia Institute of Technology, Atlanta, GA
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| Session
15-
SR-1
|
Solid Rocket Technologies
|
301/302 |
|
Chaired by: S. WALLACE, ATK Tactical Systems Co LLC, Rocket Center, WV, and J. CLARKE, Lockheed Martin, Mansfield, TX
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|
0900
AIAA-2004-3384
Unsteady CFD Calculation for Validation of a Multi- Vane Thrust Vector Control System
P. Rainville, A. deChamplain and D. Kretschmer, Laval University, Quebec, QC, Canada; R. Farinaccio and R. Stowe, DRDC Valcartier, Quebec, QC, Canada
|
0930
AIAA-2004-3385
Advanced Materials and Processes for Boost Phase Nozzles
R. Hickman and T. McKechnie, Plasma Processes Inc., Huntsville, AL
|
1000
AIAA-2004-3386
Design and Performance Evaluation of Components of Micro Solid Propellant Thruster
J. Lee, D. Lee and S. Kwon, Korea Advanced Institute of Science and Technology, Daejeon, South Korea
|
1030
AIAA-2004-3387
On the Development and Testing of a 120 mm Caliber Double Pulse Motor (DPM)
S. Schilling, P. Trouillot and A. Weigand, Bayern-Chemie/Protac, Aschau, Germany
|
1100
AIAA-2004-3388
Experimental Study of the Surface Regression Rate to the Heat Transfer
T. Lee, Agency for Defence Development, Daejon, South Korea
|
| Session
16-
VS-1
|
Air Collection and Enrichment Systems (ACES): The Gryphon Concept
|
315 |
|
Chaired by: W. ESCHER and J. HUNT, Science Applications International Corporation, Huntsville, AL
|
|
0900
AIAA-2004-3389
Comparison of Gryphon HTHL RLV to Shuttle on Key Figures of Merit
A. Crocker, Andrews Space Inc., Seattle, WA; G. Sadler and J. Roche, NASA Glenn Research Center, Cleveland, OH
|
0930
AIAA-2004-3390
Cryogenic Composite Tank Design for Next Generation Launch Technology
G. Abumeri, QSS Group Inc, Cleveland, OH; D. Kosareo, ZIN Technologies, Brookpark, OH; J. Roche, NASA Glenn Research Center, Cleveland, OH
|
1000
AIAA-2004-3391
Gryphon: A Feasible Horizontal Takeoff Next Generation Architecture Concept
G. Sadler and W. Taylor, NASA Glenn, Cleveland, OH; A. Crocker, Andrews Aerospace Inc., Seattle, WA; J. Roche, NASA Glenn, Cleveland, OH; A. Wuerl, Andrews Space Inc., Seattle, WA
|
1030
AIAA-2004-3392
Investigation of Enhanced Vortex Tube Air Separators for Advanced Space Transportation
A. Crocker, D. Cassisi and G. Sutphin, Andrews Space Inc., Seattle, WA
|
1100
AIAA-2004-3394
Structural Sizing of a Horizontal Take- off Launch Vehicle with an Air Collection and Enrichment System
D. McCurdy, QSS Group Inc., Cleveland, OH; J. Roche, NASA Glenn Research Center, Cleveland, OH
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|
1300 - 1500 |
Air Breathing Propulsion – The Future Awaits
|
Palm A & B |
Gas turbine technology continues to advance as new generations of engines are being conceived. This session will aim to better define ongoing technical activities and opportunities for gas turbine technology development. Aviation Week & Space Technology Assistant Managing Editor Stanley Kandebo will moderate this session that includes leading worldwide industry and U.S. government propulsion representatives.
Panelists:
Simeon Austin, Pratt & Whitney, Director of Advanced Programs
Alain Coutrot, Snecma, Vice President, Technology Strategy and Partnerships
Art Morrish, DARPA, Director, Tactical Technology Office (invited)
Richard Christiansen, NASA Glenn Research Center, Deputy Director
James Engle, Air Force Science, Technology and Engineering, Deputy Assistant |
|
| Session
17-
ABP-4
|
Engine Systems: PDE I
|
316 |
|
Chaired by: B. SEKAR, Air Force Research Laboratory, Wright-Patterson AFB, OH, and M. MAWID, Engineering Research and Analysis Company, Dayton, OH
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|
1300
AIAA-2004-3395
Deconstructing Detonation: Analytical Calculation of Unsteady Thrust in a PDE
T. Scott, Saint Louis University, Saint Louis, MO
|
1330
AIAA-2004-3396
Thermal Load Considerations for Detonative Combustion- Based Gas Turbine Engines
D. Paxson and H. Perkins, NASA Glenn Research Center, Cleveland, OH
|
1400
AIAA-2004-3397
Studies of Overdriven Detonation Wave Transition in a Gradual Area Expansion for PDE Applications
C. Conrad, S. Saretto, S. Lee and R. Santoro, Pennsylvania State University, University Park, PA
|
1430
AIAA-2004-3398
Thrust Augmentation Measurements for a Pulse Detonation Engine Driven Ejector
R. Shehadeh, S. Saretto, S. Lee and R. Santoro, Pennsylvania State University, University Park, PA
|
1500
AIAA-2004-3400
Design Methodology for a Pulse Detonation Engine as a Ramjet Replacement
P. Harris, R. Stowe and S. Guzik, DRDC Valcartier, Val-Belair, Quebec, Canada
|
1530
AIAA-2004-3401
Liquid Hydrocarbon Detonation Branching in a Pulse Detonation Engine
K. Panzenhagen, P. King and K. Tucker, Air Force Institute of Technology, Wright-Patterson AFB, OH; F. Schauer, Air Force Research Laboratory, Wright-Patterson AFB, OH
|
1600
AIAA-2004-3402
Performance Trends for a Product Scale Pulse Detonation Engine
S. Anderson, J. Tonouchi, G. Lidstone, K. Lupkes and J. Alfonso, Pratt & Whitney, Bellevue, WA
|
| Session
18-
ABP-5
|
Inlets
|
317 |
|
Chaired by: P. ORKWIS, University of Cincinnati, Cincinnati, OH, and L. CHENAULT, Ohio Aerospace Institute, Beavercreek, OH
|
|
1300
AIAA-2004-3403
Intake Performance During Rolling Take- off in Natural Crosswind
C. Hall, Cambridge University, Cambridge, Great Britain; N. Humphreys, Rolls-Royce plc, Derby, Great Britain
|
1330
AIAA-2004-3404
CFD Methods for Computing the Performance of Supersonic Inlets
J. Slater, NASA Glenn Research Center, Cleveland, OH
|
1400
AIAA-2004-3405
Corrected Waverider Design for Inlet Applications
M. Chauffour and M. Lewis, University of Maryland, College Park, MD
|
1430
AIAA-2004-3406
Computational Study of the Aerodynamic Performance of Subsonic Scarf Inlets
J. Abbott, NASA Glenn Research Center, Cleveland, OH
|
1500
AIAA-2004-3407
Multi- Row Disk Arrangement Concept for Spike of Axisymmetric Air Inlet
Y. Maru, University of Tokyo, Sagamihara, Kanagawa, Japan; N. Tanatsugu, T. Sato, H. Kobayashi, T. Kojima and K. Okai, Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
|
1530
AIAA-2004-3408
Effects of Engine Intake and Nozzle Design on the Performance of a Low- Signature Reconnaissance UAV
M. Wallin, T. Grönstedt and U. Håll, Chalmers University of Technology, Gothenburg, Sweden
|
1600
AIAA-2004-3409
Research on Inlet Precooling for Mini- Turbojet Engines
F. Buysschaert and P. Hendrick, Royal Military Academy of Belgium, Brussels, Belgium
|
| Session
19-
ABP-6
|
Turbomachinery Technology - Gas Turbine Performance and Modeling
|
318 |
|
Chaired by: G. ZHA, University of Miami, Coral Gables, FL, and F. KAUSER, California State University, Pomona, Pomona, CA
|
|
1300
AIAA-2004-3412
A Semi- Viscous Method for Compressor Performance Prediction
M. Attia, Embry Riddle Aeronautical University, Daytona Beach, FL
|
1330
AIAA-2004-3413
Development of a Transient Viscous Flow Solver Based on Conservation Element- Solution Element Framework
B. Venkatachari and G. Cheng, University of Alabama at Birmingham, Birmingham, AL; S. Chang, NASA Glenn Research Center, Cleveland, OH
|
1400
AIAA-2004-3414
Influence of Axial Velocity Density Ratio in Cascade Testing of Supercritical Compressor Blades
B. Song and W. Ng, Virginia Tech, Blacksburg, VA
|
1430
AIAA-2004-3415
Integrated Simulations for Multi- Component Analysis of Gas Turbines:RANS Boundary Conditions
S. Kim, J. Alonso, J. Schluter, X. Wu and H. Pitsch, Stanford University, Stanford, CA
|
1500
AIAA-2004-3416
Gas Turbine Compressors Mid and Aft Stage Radial Clearance Control
J. Burge, AGILIS Group, Jupiter, FL
|
1530
AIAA-2004-3417
Coupled RANS- LES Computation of a Compressor and Combustor in a Gas Turbine Engine
J. Schluter, X. Wu, S. Kim, J. Alonso and H. Pitsch, Stanford University, Stanford, CA
|
| Session
20-
ECS-2
|
Energetic Component Test Methods
|
209 |
|
Chaired by: J. BURCHETT and M. SAWCHAK, Naval Surface Warfare Center, Indian Head, MD
|
|
1300
AIAA-2004-3419
Uses and Abuses of Accelerated Age Testing of Pyrotechnic Devices
J. Glass, Pacific Scientific Energetic Materials Company, Hollister, CA
|
1330
AIAA-2004-3420
Satisfying Temperature Firing Requirements for Ordnance Devices
D. Jackson, Lockheed Martin, Littleton, CO
|
1400
AIAA-2004-3421
A Study on Closed- Bomb Method of Validating Energetic Components
H. Lee, Scot Inc, Downers Grove, IL
|
1430
AIAA-2004-3422
Determination of Practical Lower Limits on Frequency and Lower- Frequency Acceleration Amplitude for Ordnance- Excited Pyrotechnic Shock Testing
W. Ramm and S. Keon, Ensign-Bickford Aerospace & Defense Company, Simsbury, CT
|
1500
AIAA-2004-3423
Testing of Minuteman II Safety and Arming Device with Improved Testing Technicques
L. Yang and M. Dao-Randall, Northrop Grumman, San Bernardino, CA; D. Pham and M. Jones, U.S.Army, White Sands Missile Range, NM; T. Kuennen, U.S.Air Force, Kirtland AFB, NM; J. Seward, U.S. Air Force Space and Missile Systems Center, Kirtland Air Force Base, NM
|
1530
AIAA-2004-3424
FAI and the Pyro Detective's Toolkit
J. Glass, PSEMC, Hollister, CA
|
| Session
21-
EP-2
|
Cathode Technology & Characterization
|
113 |
|
Chaired by: G. SOULAS, NASA Glenn Research Center, Cleveland, OH, and J. HAAS, Air Force Research Laboratory, Edwards AFB, CA
|
|
1300
AIAA-2004-3425
On the Operational Status of the ISS Plasma Contactor Hollow Cathodes
C. Carpenter, QSS Group Inc., Cleveland, OH
|
1330
AIAA-2004-3427
Testing of Carbon Nanotube Field Emission Cathodes
C. Gasdaska, P. Falkos, M. Robin, V. Hruby, N. Demmons and R. McCormick, Busek Co., Natick, MA
|
1400
AIAA-2004-3429
Centrospazio Progress on MPDT Hollow Cathodes
P. Rossetti, F. Paganucci and M. Andrenucci, Centrospazio, Pisa, Italy; M. Signori, University of Pisa, Pisa, Italy
|
1430
AIAA-2004-3430
Hollow Cathode and Keeper- Region Plasma Measurements Using Ultra- Fast Miniature Scanning Probes
D. Goebel, I. Katz, R. Watkins and K. Jameson, Jet Propulsion Laboratory, Pasadena, CA
|
1500
AIAA-2004-3431
Lithium- Fed Hollow Cathode Theory
L. Cassady and E. Choueiri, Princeton University, Princeton, NJ
|
1530
AIAA-2004-3432
Measurement of Ion Energy Distributions Produced within an NSTAR Discharge Chamber
C. Farnell and J. Williams, Colorado State University, Fort Collins, CO
|
| Session
22-
EP-3
|
Electric Propulsion Flight Programs
|
114 |
|
Chaired by: D. LICHTIN, Lockheed Martin, Denver, CO
|
|
1300
AIAA-2004-3433
Status of the Dawn Ion Propulsion System
J. Brophy, M. Marcucci, J. Gates, C. Garner, B. Nakazono and G. Ganapathi, Jet Propulsion Laboratory, Pasadena, CA
|
1330
AIAA-2004-3435
The Smart- 1 Electric Propulsion Subsystem In Flight Experience
C. Koppel and F. Marchandise, Snecma Moteurs, Moissy Cramayel, France; D. Estublier, ESA/ESTEC, Noordwijk, The Netherlands; L. Jolivet, Centre National d'Etudes Spatiales, Toulouse, France
|
1400
AIAA-2004-3436
SMART1 Electric Propulsion Operations
D. Milligan, D. Gestal and O. Camino, European Space Agency, Darmstadt, Germany; D. Estublier, ESA/ESTEC, Noordwijk, The Netherlands; C. Koppel, Snecma Moteurs, Moissy Cramayel Cedex, France
|
1430
AIAA-2004-3437
Charge- Exchange Plasma Contamination on SMART- 1: First Measurements and Model Verification
M. Tajmar, ARC Seibersdorf Research, Seibersdorf, Austria; B. Foing and J. Gonzalez, ESA/ESTEC, Noordwijk, The Netherlands; G. Noci, Label Proel, Firenze, Italy; W. Schmidt, Finnish Meteorological Institute, Helsinki, Finland; F. Darnon, Centre National d'Etudes Spatiales, Toulouse, France
|
1500
AIAA-2004-3438
Flight Status of Cathode- Less Microwave Discharge Ion Engines Onboard HAYABUSA Asteroid Explorer
H. Kuninaka, K. Nishiyama, Y. Shimizu and K. Toki, Japan Aerospace Exploration Agency, Sagamihara, Japan
|
1530
AIAA-2004-3439
Microthrust Propulsion for the LISA Mission
J. Ziemer, Jet Propulsion Laboratory, Pasadena, CA; S. Merkowitz, NASA GOddard Space Flight Center, Greenbelt, MD
|
1600
AIAA-2004-3440
Propulsion Options for the LISA Mission
E. Cardiff, NASA Goddard, Greenbelt, MD; G. Marr, NASA Goddard Space Flight Center, Greenbelt, MD
|
| Session
23-
EP-4
|
Electric Propulsion Special Test & Material Topics
|
118/119 |
|
Chaired by: K. DIAMANT, The Aerospace Corporation, Los Angeles, CA, and C. KOPPEL, Snecma, Vernon, France
|
|
1300
AIAA-2004-3441
Thrust Stand for Electric Propulsion Performance Evaluation
T. Markusic, J. Jones and M. Cox, NASA Marshall Space Flight Center, Huntsville, AL
|
1330
AIAA-2004-3444
A Microscale Quadrupole Mass Spectrometer for Ion Species Analysis
S. Deshmukh, Aerophysics Inc., Calumet, MI; L. King, Michigan Technological University, Houghton, MI; C. Monroe, University of Michigan, Ann Arbor, MI
|
1400
AIAA-2004-3445
Plasma Jet Velocimetry by Cross- Correlation of Plasma Emission Oscillations
Z. Li, C. Hawk and S. Vasudevan, University of Alabama in Huntsville, Huntsville, AL
|
1430
AIAA-2004-3446
Preliminary Sputter- Erosion Characterization of Multiwalled Carbon Nanotubes
L. King, Y. Yap, J. Menda, L. Vanga, V. Kayastha and J. Wang, Michigan Technological University, Houghton, MI
|
| Session
24-
EP-5
|
Project Prometheus I
|
122 |
|
Chaired by: S. OLESON, NASA Glenn Research Center, Cleveland, OH, and J. FISHER, Aerojet, Redmond, WA
|
|
1300
AIAA-2004-3449
Electric Propulsion Technology Development for the Jupiter Icy Moon Orbiter Project
S. Oleson, NASA Glenn Research Center, Cleveland, OH
|
1330
AIAA-2004-3450
An Overview of the Nuclear Electric Xenon Ion System (NEXIS) Activity
T. Randolph and J. Polk, Jet Propulsion Laboratory, Pasadena, CA
|
1400
AIAA-2004-3453
An Overview of the High Power Electric Propulsion (HiPEP) Project
F. Elliott, NASA Glenn, Cleveland, OH; J. Foster and M. Patterson, NASA Glenn Research Center, Cleveland, OH
|
1430
AIAA-2004-3452
Power Processing for a Conceptual Project Prometheus Electric Propulsion System
J. Scina, F. Hewitt and S. Gerber, ZIN Technologies Inc., Brook Park, OH; M. Elbuluk, University of Akron, Akron, OH; M. Aulisio and L. Miller, Zin Technologies, Brook Park, OH
|
1500
AIAA-2004-3812
The High Power Electric Propulsion (HiPEP) Ion Thruster
J. Foster, NASA Glenn, Cleveland, OH; T. Haag, H. Kamhawi, M. Patterson, S. Malone and F. Elliot, NASA Glenn Research Center, Cleveland, OH
|
| Session
25-
EP-6
|
Pulsed Plasma Thruster I
|
123 |
|
Chaired by: N. GATSONIS, Worcester Polytechnic Institute, Worcester, MA, and E. PENCIL, NASA Glenn Research Center, Cleveland, OH
|
|
1300
AIAA-2004-3455
Overview of NASA's Pulsed Plasma Thruster Development Program
E. Pencil, H. Kamhawi and L. Arrington, NASA Glenn Research Center, Cleveland, OH
|
1330
AIAA-2004-3458
Evaluation of Pulsed Plasma Thruster Micropulsing
L. Arrington, QSS Group Inc., Cleveland, OH
|
1400
AIAA-2004-3460
A Pulsed Plasma Thruster Using Water as the Propellant
H. Koizumi and Y. Furuta, University of Tokyo, Tokyo, Japan; K. Watanabe, Tohoku University, Sendai, Japan; K. Komurasaki, University of Tokyo, Tokyo, Japan; A. Sasoh, Tohoku University, Sendai, Japan; Y. Arakawa, University of Tokyo, Tokyo, Japan
|
| Session
26-
EP-7
|
Pulsed Plasma Thruster II
|
124 |
|
Chaired by: R. BURTON, University of Illinois at Urbana-Champaign, Urbana, IL
|
|
1300
AIAA-2004-3462
Effects of Post- Pulse Surface Temperature on Micro- Pulsed Plasma Thruster Operation
E. Antonsen and R. Burton, University of Illinois at Urbana-Champaign, Urbana, IL; G. Spanjers, Air Force Research Laboratory, Kirtland AFB, NM; G. Reed, W.E. Research, Rosamond, CA
|
1330
AIAA-2004-3463
Canted Current Sheet Mass Leakage and its Impact on Pulsed Plasma Thruster Performance
E. Choueiri and J. Berkery, Princeton University, Princeton, NJ
|
1400
AIAA-2004-3464
Prospects of Plasma Flow Modeling and Control for Micro Pulsed Plasma Thrusters
N. Gatsonis and M. Demetriou, Worcester Polytechnic Institute, Worcester, MA
|
1430
AIAA-2004-3465
Pulsed Plasma Thruster Based Moon Orbiter Propulsion System
H. Wagner and M. Auweter-Kurtz, University of Stuttgart, Stuttgart, Germany
|
1500
AIAA-2004-3466
Slug Model and Snowplow Model for Pulsed Plasma Thruster Description
H. Wagner and M. Auweter-Kurtz, University of Stuttgart, Stuttgart, Germany
|
| Session
27-
EP-8
|
Very High Power I
|
125 |
|
Chaired by: M. LAPOINTE, NASA Glenn Research Center, Cleveland, OH, and H. WAGNER, University of Stuttgart, Stuttgart, Germany
|
|
1300
AIAA-2004-3467
High Power MPD Thruster Performance Measurements
M. LaPointe, Ohio Aerospace Institute, Cleveland, OH; E. Strzempkowski and E. Pencil, NASA Glenn Research Center, Cleveland, OH
|
1330
AIAA-2004-3468
Fundamental Scaling Laws for Electric Propulsion Concepts - Part 2: MPD Thrusters
M. Andrenucci and F. Paganucci, Centrospazio, Pisa, Italy
|
1400
AIAA-2004-3469
Self- consistent Electrode Model for Magnetoplasmadynamic Thrusters
S. Roy, Kettering University, Flint, MI
|
1430
AIAA-2004-3470
System- Level Models of Self- and Applied- Field MPD Thrusters
J. Gilland, Ohio Aerospace Institute, Brookpark, OH
|
1500
AIAA-2004-3471
Three- Dimensional Simulations of High- Power Magnetoplasmadynamic Thrusters Using the MACH3 Code
P. Mikellides and B. Parma, Arizona State University, Tempe, AZ
|
1530
AIAA-2004-3473
Kink Instabilities in a Magnetoplasmadynamic Thruster With and Without External Magnetic Field
F. Paganucci, P. Rossetti and M. Andrenucci, Centrospazio, Pisa, Italy; M. Zuin, G. Serianni and V. Antoni, Consorzio RFX, Padova, Italy
|
| Session
28-
HR-1
|
Hybrid Rockets I
|
207 |
|
Chaired by: M. CHIAVERINI, Orbitec, Madison, WI, and G. STORY, NASA Marshall Space Flight Center, Huntsville, AL
|
|
1300
AIAA-2004-3474
Inviscid Models of the Classic Hybrid Rocket
J. Majdalani and A. Vyas, University of Tennessee Space Institute, Tullahoma, TN
|
1330
AIAA-2004-3475
Rotational Axisymmetric Mean Flow for the Vortex Injection Hybrid Rocket Engine
J. Majdalani and A. Vyas, University of Tennessee Space Institute, Tullahoma, TN
|
1400
AIAA-2004-3477
Modular Solutions for Very High Energy Solid Propellants
R. Lo and H. Adirim, Aerospace Institute, Berlin, Germany; S. Poller, ICT, Berghausen, Germany
|
1430
AIAA-2004-3479
Effects of Swirling Liquid Oxygen Flow on Combustion of a Hybrid Rocket Engine
K. Kitagawa, T. Mitsutani, T. Ro and S. Yuasa, Tokyo Metropolitan Institute of Technology, Hino, Tokyo, Japan
|
| Session
29-
HYP-2
|
Hypersonic Engine Component Design Evaluation & Test
|
223 |
|
Chaired by: H. CIKANEK, NASA Glenn Research Center, Cleveland, OH, and G. MACK, Pratt & Whitney Space Propulsion, West Palm Beach, FL
|
|
1300
AIAA-2004-3480
Performance of Supersonic Combustors with Fuel Injection in Diverging Section
S. Tomioka, K. Kobayashi, K. Kudo, A. Murakami and T. Mitani, Japan Aerospace Exploration Agency, Kakuda, Japan
|
1330
AIAA-2004-3481
An Aerodynamic Redesign of the SR- 71 Inlet with Applications to Turbine Based Combined Cycle Engines
J. Colville and M. Lewis, University of Maryland, College Park, MD
|
1400
AIAA-2004-3482
Performance of a Dual- Mode Combustor with Multi- Staged Fuel Injection
K. Kobayashi, S. Tomioka, K. Kato, A. Murakami, K. Kudo and T. Mitani, Japan Aerospace Exploration Agency, Kakuda, Japan
|
1430
AIAA-2004-3483
Optimization of Microwave Air Plasma Apparatus for Hydrocarbon Combustion Enhancement Experiments
K. Fisher and M. Micci, Pennsylvania State University, University Park, PA
|
1500
AIAA-2004-3484
Experimental Verification of Ultra- High- Performance, Advanced Propulsion Heat Exchangers
G. Michna, Y. Zhong, K. Brown, A. Jacobi and R. Burton, University of Illinois at Urbana-Champaign, Urbana, IL
|
1530
AIAA-2004-3485
Performance of a Supersonic Model Combustor Using Vaporized Kerosene Injection
X. Fan, G. Yu, J. Li and X. Zhang, Chinese Academy of Sciences, Beijing, China (prc); C. Sung, Case Western Reserve University, Cleveland, OH
|
1600
AIAA-2004-3486
Enhancing Heavy Lift Booster Performance by Exploiting Zeotropic Condensation of Air
K. Brown, Y. Zhong, G. Michna, A. Jacobi and R. Burton, University of Illinois at Urbana-Champaign, Urbana, IL
|
1630
AIAA-2004-3487
Investigation of Hydrocarbon Fuels Combustion in Supersonic Combustor
A. Mathur, The Boeing Company, Huntington Beach, CA; M. Goldfeld, A. Mishunin and A. Starov, Institute of Theoretical and Applied Mechanics, Novosibirsk, Russia
|
| Session
30-
ISP-2
|
Advanced Chemical and Materials I
|
304 |
|
Chaired by: C. GUERNSEY, Jet Propulsion Laboratory, Pasadena, CA, and F. LU, Aerojet, Redmond, WA
|
|
1300
AIAA-2004-3834
A Comparison of Transportation Systems for Human Missions to Mars
B. Thomas, D. Vaughan and G. Woodcock, Gray Research Inc., Huntsville, AL; B. Drake, NASA Johnson Space Center, Houston, TX; B. Griffin, Gray Research Inc., Huntsville, AL; L. Johnson, NASA Marshall Space Flight Center, , United States
|
1330
AIAA-2004-3488
Advanced Space Storable Propellants for Outer Planet Exploration
D. Thunnissen, User Technology Associates Inc., Pasadena, CA; C. Guernsey, R. Baker and R. Miyake, Jet Propulsion Laboratory, Pasadena, CA
|
1400
AIAA-2004-3491
Preliminary Experimental Studies of Water- Energy- Cycle Space Propulsion System
Y. Hashimoto and K. Toki, Japan Aerospace Exploration Agency, Kanagawa, Japan; T. Ishii, Jisedaitech L P., Kanagawa, Japan; T. Fujita, AEC Fugita, Nagasaki, Japan
|
1430
AIAA-2004-3494
Advanced Chemical Propulsion Study
G. Woodcock, Gray Research, Huntsville, AL; D. Byers, Science Applications International Corporation, Huntsville, AL; L. Alexander and A. Krebsbach, NASA Marshall, Huntsville, AL
|
1500
AIAA-2004-4195
Modeling of Spacecraft Advanced Chemical Propulsion Systems
M. Benfield and J. Belcher, Science Applications International Corporation, Huntsville, AL
|
| Session
31-
ISP-3
|
Space Tethers Propulsion
|
305 |
|
Chaired by: J. BONOMETTI, NASA Marshall Space Flight Center, Huntsville, AL, and B. GILCHRIST, University of Michigan, Ann Arbor, MI
|
|
1300
AIAA-2004-3496
Poisson- Vlasov Modeling of Parallel Cylinders in Ionospheric Plasmas
E. Choiniere and B. Gilchrist, University of Michigan, Ann Arbor, MI
|
1330
AIAA-2004-3497
Electron Emission for Electric Propulsion: Reducing Power by Mitigating Space Charge Limits
D. Morris and B. Gilchrist, University of Michigan, Ann Arbor, MI
|
1400
AIAA-2004-3498
Field Emission Cathodes used in the FEGI Get- Away- Special Shuttle Mission
C. Deline, H. Goldberg, D. Morris, B. Gilchrist and R. Ramos, University of Michigan, Ann Arbor, MI
|
1430
AIAA-2004-3499
Cold- Cathode Electron Field Emission of Boron Nitride Thin Film with a MEMS- based Gate for Space Applications
H. Goldberg, P. Encarnación, D. Morris, B. Gilchrist and R. Clarke, University of Michigan, Ann Arbor, MI
|
| Session
32-
LP-3
|
Liquid Propellant Feed Systems & Tankage I
|
208 |
|
Chaired by: I. BALLINGER, IAB Consulting, Rugeley, Great Britain, and K. PUGMIRE, Spincraft/Standex International, Huntington Beach, CA
|
|
1300
AIAA-2004-3504
Designing and Testing a Lighter, Simpler, Less Expensive Liquid Propellant Pump
A. Knight, Andrew Knight Space Propulsion, Arlington, VA
|
1330
AIAA-2004-3505
Development of a Composite Wrapped Propellant Tank
M. Debreceni, Pressure Systems Inc., Commerce, CA; D. Jaekle, PMD Technology, North Andover, MA; T. Kuo, Pressure Systems Inc., Commerce, CA
|
1400
AIAA-2004-3506
Finite Element Analysis of a Composite Overwrapped Pressure Vessel
D. Gray, Abaqus South Inc., Flower Mound, TX; D. Moser, Compositex Inc., Sandy, UT
|
1430
AIAA-2004-3507
Design and Manufacture of a Composite Overwrapped Elastomeric Diaphragm Tank
W. Tam, Pressure Systems Inc., Commerce, CA; I. Ballinger and P. Kohorst, Pressure Systems Inc., Commerce, CA
|
1500
AIAA-2004-3508
New Design of Composite/Metal Gas Storage Vessels and Propellant Tanks
A. Cherevatsky, Shafir Productions System, Modiin, Israel; S. Cherevatsky, Nitzanim Initiative Center, Modiin, Israel; H. Dayan, Shafir Productions System, Rehovot, Israel; A. Stepanov, Nitzanim Initiative Center, Beit Shemesh, Israel
|
1530
AIAA-2004-3511
Design Modification of a Diaphragm Propellant Tank for a Pressurant Tank Application
J. Benton, Pressure Systems Inc, Commerce, CA; M. Debreceni, Pressure Systems Inc., Commerce, CA
|
| Session
33-
LP-4
|
Liquid Rocket Engine & Propulsion System Modeling I
|
220 |
|
Chaired by: G. MAGGIO, Science Applications International Corporation, New York, NY, and M. NARAGHI, Manhattan College, Riverdale, NY
|
|
1300
AIAA-2004-3514
REDTOP- 2: Rocket Engine Design Tool Featuring Engine Performance, Weight, Cost, and Reliability
J. Bradford, A. Charania and B. St. Germain, SpaceWorks Engineering Inc., Atlanta, GA
|
1330
AIAA-2004-3515
A Methodology to Rapidly and Effectively Assess the Reliability of Conceptual Advanced Rocket Engines
G. Maggio, D. Sen and F. Hark, Science Applications International Corporation, New York, NY
|
1400
AIAA-2004-3516
On Nonlinear Combustion Instability in Liquid Propellant Rocket Engines
G. Flandro, University of Tennessee Space Institute, Tullahoma, TN; J. Sims, NASA Marshall Space Flight Center, Huntsville, AL; J. Majdalani, University of Tennessee Space Institute, Tullahoma, TN
|
1430
AIAA-2004-3517
Studies of High Frequency Combustion Instabilities with the Method of Pattern Dynamics
W. Zhao, National University of Defense Technology, Changsha, China (prc); S. Hu, School of Computer National University of Defence Technoloty, Changsha, China (prc); F. Zhuang, National University of Defence Technoloty, Changsha, China (prc)
|
1500
AIAA-2004-3518
High Frequency Combustion Instabilities Associated with Collective Interactions in Liquid Propulsion
C. Rey, S. Ducruix, P. Scouflaire and F. Richecoeur, Laboratoire EM2C, Chatenay-Malabry, France; L. Vingert, ONERA, Palaiseau, France; S. Candel, Laboratoire EM2C, Chatenay-Malabry, France
|
1530
AIAA-2004-3519
Controlling Factors of Pressure- Coupled Combustion Responses in a High Pressure Combustion Chamber
G. Lee and W. Yoon, Yonsei University, Seoul, South Korea
|
| Session
34-
LP-5
|
Liquid Rocket Engine Injectors & Ignition I
|
221 |
|
Chaired by: B. GORIN, ARDE Inc, Gaithersburg, MD, and K. KREINER, Boeing Satellite Systems, Los Angeles, CA
|
|
1300
AIAA-2004-3521
The Characteristics of Swirl Coaxial Injector Under Varying Geometric and Environmental Conditions
D. Kim, W. Jeong, J. Im and Y. Yoon, Seoul National University, Seoul, South Korea
|
1330
AIAA-2004-3522
Effect of Chamber Pressure Variation on High- Frequency Hydrodynamic Instability of Shear Coaxial Injector
B. Kim, University of Illinois at Urbana-Champaign, Urbana, IL; S. Heister, Purdue University, West Lafayette, IN
|
1400
AIAA-2004-3524
Oxidizer- Rich Staged Combustion Cycle Preburner and Main Chamber Injector Testing at Purdue University
M. Long and W. Anderson, Purdue University, West Lafayette, IN
|
1430
AIAA-2004-3525
A Computational Characterization of the Supersonic Coherent Jet
M. Jeong, V. Kumar and H. Kim, Andong National University, Andong, South Korea; T. Setoguchi and S. Matsuo, Saga University, Saga, Japan
|
1500
AIAA-2004-3526
Breakup Characteristics of Laminar and Turbulent Liquid Sheets Formed by Impinging Jets in High Pressure Environments
K. Jung, B. Lim, T. Khil and Y. Yoon, Seoul National University, Seoul, South Korea
|
| Session
35-
LP-6
|
Upper-Stage Rocket Engines
|
222 |
|
Chaired by: K. COSTE, The Aerospace Corporation, Los Angeles, CA, and P. HOAR, FAA - Commercial Space Transportation, Washington, DC
|
|
1300
AIAA-2004-3527
CADB and Pratt & Whitney: A Decade of Cooperation
Y. Demiyanenko, A. Dmitrenko, V. Rachuk and A. Shostak, CADB, Voronezh, Russia; T. Hajek and A. Minick, Pratt & Whitney, East Hartford, CT
|
1330
AIAA-2004-3528
Hot Firing Tests of Liquid Rocket Engine Using LOX/LNG
Y. Cho and H. Chang, Rotem Co., Yongin, South Korea
|
1400
AIAA-2004-3529
RL60 - The Next Step in the Evolution of Upperstage Engines
J. Santiago and J. Bullock, Pratt & Whitney, West Palm Beach, FL
|
1430
AIAA-2004-3530
Development Status of the Vinci Engine for the Ariane 5 Upper Stage
P. Alliot and F. Lassoudiere, Snecma Moteurs, Vernon, France; J. Ruault, Centre National d'Etudes Spatiales, Evry, France; J. Delange, Snecma Moteurs, Vernon, France
|
1500
AIAA-2004-3531
Status of the Vinci Combustion Chamber Vacuum Ignition Tests
W. Oechslein, EADS Space Transportation GmbH, Munich, Germany
|
1530
AIAA-2004-4210
Conceptual Investigations for a Methane- Fueled Expander Rocket Engine
C. Brown, Pratt & Whitney, West Palm, FL
|
1600
AIAA-2004-3532
Thermodynamic Analysis of a Cryogenic Upper Stage Supercritical Tank
H. Nguyen, The Boeing Company, Huntington Beach, CA
|
| Session
36-
NFF-1
|
Fusion Propulsion
|
203/204 |
|
Chaired by: T. KAMMASH, University of Michigan, Ann Arbor, MI
|
|
1300
AIAA-2004-3533
Engineering Challenges in Inertial Confinement Fusion Propulsion
B. Cassenti, Pratt & Whitney, East Hartford, CT
|
1330
AIAA-2004-3534
Application of Recommended Design Practices for Conceptual Nuclear Fusion Space Propulsion Systems
C. Williams, NASA Glenn Research Center, Cleveland, OH
|
1400
AIAA-2004-3535
Tool for Sharing and Assessing Models of Fusion- Based Space Transportation Systems
S. Carpenter, Engineering Design Environments, Cupertino, CA; J. Cannady, Nova Southeastern University, Fort Lauderdale, FL
|
1430
AIAA-2004-3536
The Role of Ambipolar Potential in the Propulsive Performance of the GDM Thruster
T. Kammash and R. Tang, University of Michigan, Ann Arbor, MI
|
1500
AIAA-2004-3537
The Finite Transition Layer in Bounded Current- Carrying Plasmas
J. Siegel and A. Goff, Novatia Inc., Folsom, CA
|
1530
AIAA-2004-3538
Plasma Instabilities in the Gasdynamic Mirror Propulsion Experiment
W. Emrich, NASA Marshall Space Flight Center, Huntsville, AL
|
| Session
37-
PC-3
|
Arthur H. Lefebvre Memorial Session (Invited)
|
301/302 |
|
Chaired by: D. BALLAL, University of Dayton, Dayton, OH, and A. GUPTA, University of Maryland, College Park, MD
|
|
1300
AIAA-2004-3539
Arthur H. Lefebvre (1923- 2003)—A Tribute
D. Ballal, University of Dayton, Dayton, OH; A. Gupta, University of Maryland, College Park, MD
|
1330
AIAA-2004-3540
Fuel Atomization Effects on Combustor Performance
N. Rizk, Rolls-Royce Corporation, Indianapolis, IN
|
1400
AIAA-2004-3541
The Behavior of an Ultra- Compact Combustor (UCC) Based on Centrifugally- Enhanced Turbulent Burning Rates
J. Zelina, Air Force Research Laboratory, Wright-Patterson AFB, OH; G. Sturgess, Innovative Scientific Solutions Inc, Beavercreek, OH; D. Shouse, Air Force Research Laboratory, Wright-Patterson AFB, OH
|
1430
AIAA-2004-3543
Combustion Effciency and the Theta- Parameter in the Design and Developpment of Gas Turbine Combustors
D. Lilley, Oklahoma State University, Stillwater, OK; A. Gupta, University of Maryland, College Park, MD
|
1500
AIAA-2004-3544
Combining Lefebvre Correlations with Combustor CFD
H. Mongia, GE Aircraft Engines, Cincinnati, OH
|
1530
AIAA-2004-3545
Characterization of Flameholding Tendencies in Premixer Passages for Gas Turbine Applications
G. Samuelsen and V. McDonell, University of California Irvine, Irvine, CA; P. Couch, University of California, Irvine, CA
|
1600
AIAA-2004-3546
Combustor Stability & Lean Blowout
D. Ballal, University of Dayton, Dayton, OH
|
1630
AIAA-2004-4198
Water Injection of Commercial Aircraft to Reduce Airport Emissions
D. Daggett and L. Fucke, Boeing Commercial Airplanes, Seattle, WA; R. Hendricks, NASA Glenn, Cleveland, OH; D. Eames, Rolls-Royce Corporation, Indianapolis, IN
|
| Session
38-
SCP-1
|
Sensors and Measurement Technology
|
210 |
|
Chaired by: J. WRBANEK, NASA Glenn Research Center, Cleveland, OH, and M. PALMER, Luna Innovations, Blacksburg, VA
|
|
1300
AIAA-2004-3547
Validation of Stream Thrust Probes for Direct- Connect Turbine Engine Testing
R. Hiers and H. MacKinnon, Aerospace Testing Alliance, Arnold AFB, TN
|
1330
AIAA-2004-3548
Sensor Requirements to Monitor the Real Time Performance of a Gas Turbine Engine Undergoing Compressor Blade Erosion
S. Scala, M. Konrad, R. Mason and J. Semick, Concurrent Technologies Corporation, Largo, FL; D. Skelton, U.S. Army Industrial Ecology Center, Picatinny Arsenal, NJ
|
1400
AIAA-2004-3549
Development of Thin Film Ceramic Thermocouples for High Temperature Environments
J. Wrbanek, G. Fralick and S. Farmer, NASA Glenn Research Center, Cleveland, OH; A. Sayir, Case Western Reserve University, Cleveland, OH; C. Blaha and J. Gonzalez, Akima Corporation, Brook Park, OH
|
1430
AIAA-2004-3550
Effect of Rotor Solidity on Stall Inception and Growth in Axial Flow Fan
S. Sane and P. Tagade, Indian Institute of Technology Bombay, Mumbai, India
|
1500
AIAA-2004-3551
Skin Friction Measurements in a Duct in the X3 Superorbital Expansion Tube
T. Silvester, R. Morgan and P. Jacobs, University of Queensland, Brisbane, Australia
|
1530
AIAA-2004-4190
High- Frequency, Fiber- Optic Total Temperature Sensors for Air Breathing Propulsion Inlet Distortion Characterization
M. Palmer, R. Fielder and K. Stinson-Bagby, Luna Innovations, Blacksburg, VA; J. Schetz and M. Tonks, Virginia Polytechnic Institute and State University, Blacksburg, VA
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| Session
39-
SR-2
|
Mars Exploration Rover (MER) Propulsion (Joint ASME and AIAA Special Session)
|
Floridian Ballroom |
|
Chaired by: D. LINNE, NASA Glenn Research Center, Cleveland, OH, and C. CARR, Alliant Techsystems, Elkton, MD
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|
| Session
40-
VS-2
|
Earth-to-Orbit Vehicle Reusability
|
315 |
|
Chaired by: R. SACKHEIM, NASA Marshall Space Flight Center, Huntsville, AL
|
|
1300
AIAA-2004-3559
Human Space Transportation and Logistic Activities at ESA
M. Caporicci, European Space Agency, Noordwjik, The Netherlands
|
1330
AIAA-2004-3561
Propulsion Economic Considerations for Next Generation Space Launch
C. Taylor, Jupiter Research & Development, Houston, TX
|
1400
AIAA-2004-3562
Launch Vehicle Design Features for Minimum Cost
R. Portz, University of Florida, Gainesville, FL
|
1430
AIAA-2004-3563
Human Spaceflight of Next Generation
P. Morgan, Lockheed Martin Space Systems Company, Denver, CO
|
|
1500 - 1700 |
On Orbit Servicing – An Untapped Opportunity
|
Palm A & B |
Extending satellite-service life impacts millions of dollars on the bottom line for space-based service businesses. The potential market for on-orbit servicing is a prime untapped opportunity to explore. Space News Deputy Editor Warren Ferster will moderate a session with government and industry leaders to find out the likelihood that this opportunity will ever be realized on a large scale and the logistics required to make it happen.
Panelists:
Ron Sega, U.S. Department of Defense, Director, National Aerospace Initiative
Stephen Wax, DARPA, Director, Defense Science Office (invited)
Thomas B. McDonald, Vice President, Transformational Space Systems, The Boeing Company (invited)
Walt Anderson, CEO, Orbital Recovery Corporation |
|
| Session
41-
NFF-2
|
Future Flight I
|
Palm A |
|
Chaired by: M. LAPOINTE, Ohio Aerospace Institute, Cleveland, OH
|
|
1900
AIAA-2004-3567
Beamed- Momentum LightSails for Interstellar Missions: Mission Applications and Technology Requirements
R. Frisbee, Jet Propulsion Laboratory, Pasadena, CA
|
1945
AIAA-2004-3568
The Interstellar Ramjet
B. Cassenti, Pratt & Whitney, East Hartford, CT
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