Design and theoretical performance prediction of hydrogen peroxide hybrid thruster
A design procedure to realize a hybrid rocket engine that uses hydrogen peroxide as the oxidizer and a solid polymer as the fuel is presented. In the design procedure, the products of decomposition and of combustion at different stations are calculated by linking a standard complex chemical-equilibr...
保存先:
| 主要な著者: | , , , |
|---|---|
| フォーマット: | Conference or Workshop Item |
| 出版事項: |
2009
|
| 主題: | |
| オンライン･アクセス: | http://eprints.utm.my/id/eprint/15036/ |
| タグ: |
タグ追加
タグなし, このレコードへの初めてのタグを付けませんか!
|