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...
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| Format: | Thesis |
| Language: | English |
| Published: |
2006
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| Online Access: | https://ir.uitm.edu.my/id/eprint/37346/1/37346.pdf |
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