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The Design And Development Of Pneumatic Impulse Rocket For Night Parachute Search Lighting

Kee, Low Chit (2009) The Design And Development Of Pneumatic Impulse Rocket For Night Parachute Search Lighting. Project Report. UTeM, Melaka, Malaysia. (Submitted)

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Abstract

Design of pneumatic impulse rocket for night parachute search lighting is considered as an aerodynamic and also mechanical field of engineering study. Since the use of brimstone and burnt or explosive material to produce force in rocket has caused pollution during the process of launching the rocket for night parachute search lighting, an environmental friendly solution needed to be searched, thus pneumatic impulse rocket for night parachute search lighting had been proposed and designed. It is a device used to carry night parachute search lighting to the sky and it uses pneumatic impulse to create launching force instead of using brimstone burnt or explosive material hich had cause pollution. The method used in preparing this project include the preparing of project mission statement, project outline, research, data analysis, product design specification (PDS), functional model analysis, generate concepts, metrics evaluation, concept selection, detail design, fabrication and hardware procurement,implementation and modification. When the part of product had been fabricated and assembled, experimental testing will be conducted before project realisation and verification started. This project will end by verification of supervisor and panel of seminal. The design of pneumatic impulse rocket for night parachute search lighting that work efficiently and environmental friendly has been successfully designed in the end of this project. It is able to carry night parachute search lighting to the sky and by just using pneumatic impulse to create launching force. Lastly, I recommend for those who interested to proceed with this project, they should try to modify the design using more suitable material which is cheaper but at the same time has the equal or better quality design.

Item Type: Final Year Project (Project Report)
Uncontrolled Keywords: Rocket engines, Microspacecraft
Subjects: T Technology > T Technology (General)
T Technology > TL Motor vehicles. Aeronautics. Astronautics
Divisions: Library > Final Year Project > FKM
Depositing User: Rohana Hashim
Date Deposited: 07 Mar 2012 02:46
Last Modified: 28 May 2015 02:20
URI: http://digitalcollection.utem.edu.my/id/eprint/967

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