Aerothermodynamic Optimization of Re-Entry Heat Shield Shapes for a Crew Exploration Vehicle
- Author(s):
- J. Johnson ( University of Maryland, College Park, MD )
- R. Starkey
- M. Lewis
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Atmospheric Flight Mechanics Conference
- Ser. no.:
- 2006
- Pub. Year:
- 2006
- No.:
- 2006-6273
- Paper no.:
- AIAA Paper 2006-6273
- Pub. info.:
- Reston, Va: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200619 [CD-ROM 2006 Disc 19]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Aerodynamic Stability of Re-Entry Heat Shield Shapes for a Crew Exploration Vehicle
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Horizontal Launch Vehicle Weight Modeling for Future Lunar Exploration-Class Payloads
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Crew Exploration Vehicle Environmental Control and Life Support Design Reference Missions.
Society of Automotive Engineers |
5
Technical Paper
Aerothermodynamic Testing of Protuberances and Penetrations on the NASA Crew Exploration Vehicle Heat Shield
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Global Heat-Transfer Measurements on the NASA Crew Exploration Vehicle at AEDC Tunnel 9
American Institute of Aeronautics and Astronautics |