Design and fabrication of a rocket engine powered by kerosene with compressed oxygen as an oxidiser / Rusli Abdul Aziz
This paper presents the design, fabrication and testing of a bi - propellant rocket engine with a thrust of 250N. Kerosene and oxygen, in liquid and gaseous form respectively, are used as propellants. The test engine is fabricated from solid round bars of stainless steel on a lathe machine. A test s...
Saved in:
| 主要作者: | |
|---|---|
| 格式: | Thesis |
| 語言: | English |
| 出版: |
2006
|
| 主題: | |
| 在線閱讀: | https://ir.uitm.edu.my/id/eprint/37346/1/37346.pdf |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|