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Effect of oxidizer-fuel ratio and chamber pressure to the burning characteristic of AP/HTPB/AL composite propellant

Wan Ali, Wan Khairuddin and Abdul Aziz , Amir (2010) Effect of oxidizer-fuel ratio and chamber pressure to the burning characteristic of AP/HTPB/AL composite propellant. In: 2nd Conference on Engineering and Technology Education,, 10th August 2010, Kuching.

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Item Type:Conference or Workshop Item (Paper)
Subjects:T Technology > TJ Mechanical engineering and machinery
Divisions:Mechanical Engineering
ID Code:23940
Deposited By: Liza Porijo
Deposited On:26 Sep 2012 06:35
Last Modified:26 Sep 2012 06:35

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