Ballistic Range Launch; A Low-Cost Free-Flight Scramjet Test Technique
- Author(s):
Tyll, J.S. ( GASL, Inc. ) Bakos, R.J. Modroukas, D. Bell, L.P. Jones, G.R. Purnell, M.G. - Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA Aerodynamic Measurement Technology and Ground Test Conference
- Ser. no.:
- 2000
- Pub. Year:
- 2000
- No.:
- 2000-2442
- Paper no.:
- 00-2442
- Page(from):
- 1
- Page(to):
- 16
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Design, fabrication, and calibration of a mach 6.5 hypersonic shock tunnel nozzle for scramjet testing applications
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Experiments on a RBCC ejector scramjet with integrated, staged secondary-fuel injection
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Concurrent Aerodynamic Shape/Cost Design of Magnetic Levitation Vehicles Using MDO Techniques
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Flight Results from a Program to Develop a Freeflight Atmospheric Scramjet Test Technique
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
12
Technical Paper
Experiments on a RBCC Ejector Scramjet with Integrated, Staged Secondary-Fuel Injection
American Institute of Aeronautics and Astronautics |