Muhalim, Noor Muhammad Feizal and Krishnan, Subramanian and Mohd. Jaafar, Mohammad Nazri and Wan Ali, Wan Khairuddin (2009) Design and theoretical performance prediction of hydrogen peroxide hybrid thruster. In: Conference on Aerospace Technology of the XXI Century (AEROTECH2009), 2009, Novotel Kuala Lumpur City Center.
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Abstract
A design procedure to realize a hybrid rocket engine that uses hydrogen peroxide as the oxidizer and a solid polymer as the fuel is presented. In the design procedure, the products of decomposition and of combustion at different stations are calculated by linking a standard complex chemical-equilibrium program of NASA. For the designed basic-configuration, applying the mass conservation principle, theoretical performance results are presented with propellant-tank pressure and grain port length as parameters.
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Uncontrolled Keywords: | hybrid rocket engine, propellant-tank pressure |
| Subjects: | T Technology > TJ Mechanical engineering and machinery |
| Divisions: | Mechanical Engineering |
| ID Code: | 15036 |
| Deposited By: | Narimah Nawil |
| Deposited On: | 20 Sep 2011 09:10 |
| Last Modified: | 20 Jul 2020 01:23 |
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