Design, Fabricate and Test a Solid Propellant Rocket Motor

dc.contributor.author	Kamarul Arifin Ahmad
dc.date.accessioned	2017-08-04T08:29:04Z
dc.date.available	2017-08-04T08:29:04Z
dc.date.issued	2011
dc.description.abstract	In this paper we summarize the work done on experimental solid propellant at lab-scale in order to develop an alternative source for solid propulsion application. The propellants that we are concerned with comprise Potassium Nitrate and Ferric Oxide embedded in a binder such as epoxy. The influence of epoxy mixing ratio on the samples density was observed in the experiment. <l:>servation on the crack surface of the cured propellants was done using scanning elect ron microscope ( S:M). Two solid propellant grain configurations were casted in this experiment to study their influences on the performance in term of thrust produced. Non-destructive test (X-ray radiography) was used for the understanding of the cured propellant internal structure. Thrust curvesoftheexperimental solid propellants obtained in statictest were presented in this paper	en_US
dc.identifier.uri	http://hdl.handle.net/123456789/4326
dc.title	Design, Fabricate and Test a Solid Propellant Rocket Motor	en_US
dc.type	Technical Report	en_US

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