Design, Fabrication And Testing Of A Solid Propellant Rocket Motor

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dc.contributor.authorAng, Kiang Long
dc.date.accessioned2018-08-14T02:16:58Z
dc.date.available2018-08-14T02:16:58Z
dc.date.issued2011-06
dc.description.abstractThe objectives of this paper are to design, fabricate and test a solid propellant rocket motor. First, Literature studies on rocket motor fundamental which covered existing motor designs and theories for determining the properties of the rocket motor. Next, the numerical analysis in grain material and dimension for the rocket motor are included in this report. The simulation result by computer aids software (SolidWorks 2008) for the flow characteristics especially in the nozzle area is presented. The fabrication techniques and the Non-Destructive Test (NDT) on solid propellant also included in this thesis. Two solid propellant grain configurations were designed in this project to studies their effect on the rocket performance. Thrust profile of each grain configuration was determined through experiment measurements in static test. Repeatability test was done to determine the reliability of the experimental results. It was found that the single perforated grain profile given a higher total impulse compared to tri-perforated grain, although tri-perforated grain produced almost twice thrust value of single perforated grain in static test.en_US
dc.identifier.urihttp://hdl.handle.net/123456789/6292
dc.language.isoenen_US
dc.publisherUniversiti Sains Malaysiaen_US
dc.subjectTo design, fabricate and testen_US
dc.subjecta solid propellant rocket motoren_US
dc.titleDesign, Fabrication And Testing Of A Solid Propellant Rocket Motoren_US
dc.typeThesisen_US
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