Transient Analysis of the LE-7A Rocket Engine Using the Rocket Engine Dynamic Simulator (REDS)
- Author(s):
Yamanishi, N. ( Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, Japan ) Kimura, T. Takahashi, M. Okita, K. Atsumi, M. ( Mitsubishi Heavy Industries, Komaki, Aichi, Japan ) Negishi, H. ( Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, Japan ) - Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 40th
- Pub. Year:
- 2004
- No.:
- 2004-3850
- Paper no.:
- AIAA Paper 2004-3850
- Pub. info.:
- [Reston, Va.]: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200413 [CD-ROM 2004 Disc 13]
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Elastodynamic Analysis of Fluid-Induced Vibration in the LE-7A Liquid Hydrogen Pump
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Numerical Analysis of Flow-Induced Structural Vibration in the LE-7A Liquid Hydrogen Pump
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Numerical Analysis of Plume Heating Environment for H-IIA Launch Vehicle During Powered Ascent
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Feasibility Study of Multi Objective Shape Optimization for Rocket Engine Turbopump Blade Design
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Influence of a Gap for Film Cooling on Transient Flow Characteristics of Rocket Engine Nozzles.
American Institute of Aeronautics and Astronautics |