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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Official URL: https://dx.doi.org/10.1063/1.3464841
Abstract
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, NH4ClO4 with aluminium, Al and Hydroxyl Terminated Polybutadiene, HTPB as the binder. It is the aim of this research to design and fabricate a new rocket motor that will produce a thrust of 200N by using this new solid propellant. A static test is done to obtain the thrust produced by the rocket motor and analyses by observation and also calculation will be done. The experiment for the rocket motor is successful but the thrust did not achieve its required thrust.
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Uncontrolled Keywords: | rocket motor, potassium nitrate, solid propellant |
| Subjects: | T Technology > TJ Mechanical engineering and machinery |
| Divisions: | Mechanical Engineering |
| ID Code: | 15034 |
| Deposited By: | Narimah Nawil |
| Deposited On: | 20 Sep 2011 09:10 |
| Last Modified: | 20 Jul 2020 01:23 |
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