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Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant

Ab Wahid, Mastura and Wan Ali, Wan Khairuddin (2009) Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant. In: The 2nd International Meeting on Advances in Thermo-Fluids (IMAT) 2009 , 2009, Taman Safari, Bogor, Indonesia.

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Item Type:Conference or Workshop Item (Paper)
Subjects:T Technology > TJ Mechanical engineering and machinery
Divisions:Mechanical Engineering
ID Code:15034
Deposited By: Liza Porijo
Deposited On:20 Sep 2011 09:10
Last Modified:20 Sep 2011 09:10

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