Injector research for shuttle OMS upgrade using LOX/ethanol propellants
- 著者名:
Woodward, R.D. ( The Pennsylvania State University, Propulsion Engineering Research Center ) Miller, K.L. ( The Pennsylvania State University, Propulsion Engineering Research Center ) Bazarov, V.G. ( The Pennsylvania State University, Propulsion Engineering Research Center ) Guerin, G.F. ( The Pennsylvania State University, Propulsion Engineering Research Center ) Pal, S. ( The Pennsylvania State University, Propulsion Engineering Research Center ) Santoro, R.J. ( The Pennsylvania State University, Propulsion Engineering Research Center ) - 掲載資料名:
- AIAA paper
- シリーズ名:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- シリーズ巻号:
- 1998
- 発行年:
- 1998
- 通号:
- 98-3816
- ペーパー番号:
- 98-3816
- 開始ページ:
- 1
- 終了ページ:
- 13
- 総ページ数:
- 13
- 出版情報:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- 言語:
- 英語
- 請求記号:
- A07400
- 資料種別:
- テクニカルペーパー
類似資料:
1
テクニカルペーパー
LOX/GH2 Shear Coaxial Injector Atomization Studies: Effect of Recess and Non-Concentricity
American Institute of Aeronautics and Astronautics |
7
テクニカルペーパー
Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non-Intrusive Laser Diagnostics
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
テクニカルペーパー
Deflagration to Detonation Transition Study Using Simultaneous Schlieren And OH PLIF Images
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
テクニカルペーパー
Experimental investigation of oxygen rich LOX/GH2 combustion using linewise Raman imaging
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
Influence of propellant injector stationary and dynamic parameters on high frequency combustion stability
American Institute of Aeronautics and Astronautics |