The Effect of High Concentration Guanidinium Azo-Tetrazolate on Thrust and Specific Impulse of a Hybrid Rocket
- 著者名:
Wright, A. ( Department of Physics Hendrix College ) Foley, P. Tilahun, D. Reason, M. Bryant, C. Patton, J. Hudson, M. K. - 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:
- 2000
- 発行年:
- 2000
- 通号:
- 2000-3885
- ペーパー番号:
- 00-3885
- 開始ページ:
- 1
- 終了ページ:
- 10
- 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
A Thrust and Impulse Study of Guanidinium Azo-Tetrazolate as an Additive for Hybrid Rocket Fuel
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
テクニカルペーパー
A thrust and impulse study of Guanidinium Azo-Tetrazolate as an additive for hybrid rocket fuel
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 |
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
Initial Experiments on a Dual-Stage 4-Grid Ion Thruster for Very High Specific Impulse and Power
American Institute of Aeronautics and Astronautics |