Design and theoretical performance prediction of hydrogen peroxide hybrid thruster
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-equilibr...
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Main Authors: | Muhalim, Noor Muhammad Feizal, Krishnan, Subramanian, Mohd. Jaafar, Mohammad Nazri, Wan Ali, Wan Khairuddin |
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Format: | Conference or Workshop Item |
Published: |
2009
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Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/15036/ |
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