A rocket engine has: a combustion chamber having a chamber inlet for receiving an oxidizer and a chamber outlet for expelling combustion gases in an environment outside the combustion chamber; a manifold having a manifold inlet fluidly connectable to a source of the oxidizer and a manifold outlet; a catalyst having a catalyst inlet fluidly connected to the manifold outlet and a catalyst outlet; and an injector plate having a injector inlet fluidly connected to the catalyst outlet and an injector outlet fluidly connected to the chamber inlet.
Rocket engine with integrated oxidizer catalyst in manifold and injector assembly
2024-08-13
Patent
Electronic Resource
English
Variable-flow hybrid rocket oxidizer injector
AIAA | 2001
|Oxidizer-Rich Preburner for Advanced Rocket Engine Application
British Library Conference Proceedings | 1994
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