Recession Curve Generation for Space Shuttle Solid Rocket Booster Thermal Protection System Coatings.
- Author(s):
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME Joint Thermophysics and Heat Transfer Conference
- Ser. no.:
- 2002
- Pub. Year:
- 2002
- No.:
- 2002-3334
- Paper no.:
- 2002-3334
- Pages:
- 5
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Space Shuttle Thermal Protection System Repair Flight Experiment Induced Contamination Impacts
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 |
4
Technical Paper
EFFECTS OF NATURAL ENVIRONMENT ON FIRST GENERATION SOLID ROCKET BOOSTER THERMAL PROTECTION SYSTEM MATERIALS
National Aeronautics and Space Administration |
10
Technical Paper
Real-Time Inhbitor Recession Measurements in Two Space Shuttle Reusable Solid Rocket Motors
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Qualification of ion vapor deposition aluminum coating as a replacement for cadmium plating in bolts used in nozzles of space shuttle solid rocket boosters
American Institute of Aeronautics and Astronautics |
11
Technical Paper
A THERMAL-FLOW CODE FOR MODELING GAS DYNAMICS AND HEAT TRANSFER IN SPACE SHUTTLE SOLID ROCKET MOTOR JOINTS
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
12
Technical Paper
Shearographic Non-Destructive Evaluation of Space Shuttle Thermal Protection Systems
National Aeronautics and Space Adminstration |