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: | |
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| Format: | Thesis |
| Language: | English |
| Published: |
2004
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| 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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| Summary: | 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. |
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