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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Bibliographic Details
Main Author: Sadarudin, Noor Edzwan Hishamuddin
Format: Thesis
Language:English
Published: 2004
Online Access:https://ir.uitm.edu.my/id/eprint/78233/1/78233.PDF
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