Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant
The development of rocket motor using potassium nitrate, carbon and sulphur mixture has successfully been developed by researchers and students from UTM and recently a new combination for solid propellant is being created. The new solid propellant will combine a composition of Ammonium perchlorate,...
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| Format: | Conference or Workshop Item |
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2009
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