A comparative study of the effects of liquid- versus gaseous-oxygen injection on combustion stability in 11-inch-diameter hybrid motors
- Author(s):
- Boardman, T.A. ( Thiokol Corporation )
- Carpenter, R.L.
- Claflin, S.E.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 1997
- Pub. Year:
- 1997
- No.:
- 97-2936
- Paper no.:
- 97-2936
- Page(from):
- 1
- Page(to):
- 22
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Design and Testing of an Upper Stage Hybrid Propulsion System Using Hydrogen Peroxide Oxidizer
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Overview of 10 Inch Diameter HTPB Hybrid Motor Testing with Liquid Oxygen at Stennis Space Center
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Study of Heat Transfer in a Gaseous Hydrogen Liquid Oxygen Multi-Element Combustor
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
Trans Tech Publications |