Theoretical and experimental research on the throat to port area ratio in a solid rocket motor
- Author(s):
- Wang, N.F. ( Xi'an Modern Chemistry Research Institute )
- Li, X.L.
- Feng, W.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 1996
- Pub. Year:
- 1996
- No.:
- 96-3056
- Paper no.:
- 96-3056
- Page(from):
- 1
- Page(to):
- 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 |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Experimental Rocket Motor Applied in Evaluate the Ablation Performance of Ablation Resistance Materials
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
The Analysis on the Rising Section of Experimental Pressure in Variable Thrust Pintle Solid Rocket Motor
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Experimental and Numerical Characterizations of Unstable Sources in a Solid Rocket Motor
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Comprehensive studies on flame spread with sudden expansions of ports of solid rocket motors under elevated pressure
American Institute of Aeronautics and Astronautics |