Hydroxyl amine based staged combustion hybrid rocket motor

Details Hydroxyl amine based staged combustion hybrid rocket motor Hydroxyl amine based staged combustion hybrid rocket motor

2011-06-28

2011-06-28

Cuff, Michael (Department: 3741)

Power plants

Reaction motor

Method of operation

C060S253000

Reexamination Certificate

active

07966805

ABSTRACT:
A new rocket motor assembly configuration is disclosed. Amine based oxidizer is decomposed in the presence of a metallic catalyst to generate an oxygen rich hot gas stream. The hot gas stream is used to trigger a Magnesium based solid fuel in the combustion chamber. The thrust of the rocket motor may be regulated at multiple points. This design thus offers an IM compliant, thrust-adjustable rocket motor that is of a low hazard classification without compromising its performance.

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