Transient Analysis of the LE-7A Rocket Engine Using the Rocket Engine Dynamic Simulator (REDS)
- 著者名:
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 ) - 掲載資料名:
- AIAA meeting papers on disc
- シリーズ名:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- シリーズ巻号:
- 40th
- 発行年:
- 2004
- 通号:
- 2004-3850
- ペーパー番号:
- AIAA Paper 2004-3850
- 出版情報:
- [Reston, Va.]: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- 言語:
- 英語
- 請求記号:
- A07400/200413 [CD-ROM 2004 Disc 13]
- 資料種別:
- テクニカルペーパー
類似資料:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
テクニカルペーパー
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
テクニカルペーパー
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
テクニカルペーパー
Feasibility Study of Multi Objective Shape Optimization for Rocket Engine Turbopump Blade Design
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
Influence of a Gap for Film Cooling on Transient Flow Characteristics of Rocket Engine Nozzles.
American Institute of Aeronautics and Astronautics |