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UJIAN PEMBAKARAN PROPELAN ROKET PEPEJAL
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نویسنده
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Jaafar Mohammad Nazri Mohd. ,Wan Ali Wan Khairuddin ,Zahri Ahmad Saufi Mohamed
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منبع
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jurnal teknologi - 2010 - دوره : 52 - - کد همایش: - صفحه:13 -28
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چکیده
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The composition of lacquer and fuel used during fabrication of solid propellant affects the burning rates. this study shows the effect of varying the percentage composition of both items. results obtained show that the burning rates reduce with increase in laker percentage when fuel was set constant at 29%. however, when lacquer was set constant at 22% and at varied fuel compositions, the burning rates show a parabolic plot with the optimum composition at 28.6% fuel.
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کلیدواژه
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Kalium nitrate; sulfur; aluminium; burning rate; solid rocket
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آدرس
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Universiti Teknologi Malaysia, Fakulti Kejuruteraan Mekanikal, Jabatan Kejuruteraan Aeronautik, Malaysia, Universiti Teknologi Malaysia, Fakulti Kejuruteraan Mekanikal, Jabatan Kejuruteraan Aeronautik, Malaysia, Universiti Teknologi Malaysia, Fakulti Kejuruteraan Mekanikal, Jabatan Kejuruteraan Aeronautik, Malaysia
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Authors
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