Kimsin, Intan Noryanah and Mohd. Jaafar, Mohammad Nazri and Wan Ali, Wan Khairuddin (2008) Development of a burning rate test rig for solid propellant performance investigation. In: 2nd Regional Conference on Vehicle Engineering & Technology, 15 - 16 July 2008, Hotel Istana, Kuala Lumpur.
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The main idea behind this study is to develop a burning rate test rig to test solid propellant performance. This paper describes the development of the burning rate test rig and the experimental tests on burning propellant. Burning rate test was conducted on a standard strand burner test rig under atmospheric pressure. The results obtained from the test were then analyzed. From the result, it was found that the burning rate of the propellant ranges from 3.2 cm/s to 3.6 cm/s.
|Item Type:||Conference or Workshop Item (Paper)|
|Uncontrolled Keywords:||solid rocket, potassium nitrate, burning rate, igniter, timer.|
|Subjects:||T Technology > TJ Mechanical engineering and machinery|
|Deposited By:||Dr Abd Rahim Abu Bakar|
|Deposited On:||15 Dec 2008 08:27|
|Last Modified:||15 Dec 2008 08:27|
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