Regulated combustion chamber as a thrust initiator / Noor Edzwan Hishamuddin Sadarudin

This project most likely as laboratory simulation of small rocket engines system as well. In this thesis, chapter 1 addresses the introduction to the project. It deals with the propulsion system. Apart from that, the objectives of this project are described as well as the scope of project. Chapter 2...

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书目详细资料
主要作者: Sadarudin, Noor Edzwan Hishamuddin
格式: Thesis
语言:English
出版: 2004
在线阅读:https://ir.uitm.edu.my/id/eprint/78233/1/78233.PDF
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