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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Bibliographic Details
Main Authors: Muhalim, Noor Muhammad Feizal, Krishnan, Subramanian, Mohd. Jaafar, Mohammad Nazri, Wan Ali, Wan Khairuddin
Format: Conference or Workshop Item
Published: 2009
Subjects:
Online Access:http://eprints.utm.my/id/eprint/15036/
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