Regulated combustion chamber as a thrust initiator / Mohd Nur Affendi Sallehuddin
This project most likely as laboratory simulation of small rocket engines system as well. In this thesis, chapter 1 addresses the introduction to theproject. 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...
محفوظ في:
| المؤلف الرئيسي: | |
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| التنسيق: | أطروحة |
| اللغة: | English |
| منشور في: |
2004
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| الوصول للمادة أونلاين: | https://ir.uitm.edu.my/id/eprint/78171/1/78171.PDF |
| الوسوم: |
إضافة وسم
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
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| الملخص: | This project most likely as laboratory simulation of small rocket engines system as well. In this thesis, chapter 1 addresses the introduction to theproject. 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 die chamber, hi diis chapter the related equation of designing the combustion chamber are presented. Chapter 4 is discussed about the testing equipments 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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