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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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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
https://ir.uitm.edu.my/id/eprint/78233/
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spelling my.uitm.ir.782332023-11-06T04:52:54Z https://ir.uitm.edu.my/id/eprint/78233/ Regulated combustion chamber as a thrust initiator / Noor Edzwan Hishamuddin Sadarudin Sadarudin, Noor Edzwan Hishamuddin 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 introduces the thrust concept and theory of thrust developed by propulsion system is presented in brief. All the theories are based on the thermodynamics and fluid mechanics point of view. In this chapter, the relevant equations that is important for the thrust is defined. Chapter 3 was discussed in brief of the chamber. In this chapter the related equation of designing the combustion chamber are presented. Chapter 4 is discussed about the testing equipment's required in this project. Test stand was review in chapter 5 where the design is developed. Chapter 6 relates to the safety requirements while doing this project. This section focus on operation of the system before and at the same time as the testing is operated. The ignition system and how it operates is discussed in chapter 7. Testing and analyzing of thrust developed by combustion system was discussing in chapter 8. The discussion, conclusion and recommendation are imparted in chapter 9,10 and 11 respectively. 2004 Thesis NonPeerReviewed text en https://ir.uitm.edu.my/id/eprint/78233/1/78233.PDF Regulated combustion chamber as a thrust initiator / Noor Edzwan Hishamuddin Sadarudin. (2004) Degree thesis, thesis, Universiti Teknologi Mara (UiTM).
institution Universiti Teknologi Mara
building Tun Abdul Razak Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Mara
content_source UiTM Institutional Repository
url_provider http://ir.uitm.edu.my/
language English
description 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 introduces the thrust concept and theory of thrust developed by propulsion system is presented in brief. All the theories are based on the thermodynamics and fluid mechanics point of view. In this chapter, the relevant equations that is important for the thrust is defined. Chapter 3 was discussed in brief of the chamber. In this chapter the related equation of designing the combustion chamber are presented. Chapter 4 is discussed about the testing equipment's required in this project. Test stand was review in chapter 5 where the design is developed. Chapter 6 relates to the safety requirements while doing this project. This section focus on operation of the system before and at the same time as the testing is operated. The ignition system and how it operates is discussed in chapter 7. Testing and analyzing of thrust developed by combustion system was discussing in chapter 8. The discussion, conclusion and recommendation are imparted in chapter 9,10 and 11 respectively.
format Thesis
author Sadarudin, Noor Edzwan Hishamuddin
spellingShingle Sadarudin, Noor Edzwan Hishamuddin
Regulated combustion chamber as a thrust initiator / Noor Edzwan Hishamuddin Sadarudin
author_facet Sadarudin, Noor Edzwan Hishamuddin
author_sort Sadarudin, Noor Edzwan Hishamuddin
title Regulated combustion chamber as a thrust initiator / Noor Edzwan Hishamuddin Sadarudin
title_short Regulated combustion chamber as a thrust initiator / Noor Edzwan Hishamuddin Sadarudin
title_full Regulated combustion chamber as a thrust initiator / Noor Edzwan Hishamuddin Sadarudin
title_fullStr Regulated combustion chamber as a thrust initiator / Noor Edzwan Hishamuddin Sadarudin
title_full_unstemmed Regulated combustion chamber as a thrust initiator / Noor Edzwan Hishamuddin Sadarudin
title_sort regulated combustion chamber as a thrust initiator / noor edzwan hishamuddin sadarudin
publishDate 2004
url https://ir.uitm.edu.my/id/eprint/78233/1/78233.PDF
https://ir.uitm.edu.my/id/eprint/78233/
_version_ 1783882150873923584
score 13.211869

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