Hybrid rocket system

Details Hybrid rocket system Hybrid rocket system

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 9/72 (2006.01) F02K 9/08 (2006.01) F02K 9/26 (2006.01) F02K 9/84 (2006.01)

Patent

CA 2633097

The present invention describes a hybrid rocket motor that includes a first solid reactant and at least one thrust nozzle and at least one moveable combustion control member within the hybrid rocket motor that restricts the contact of a first fluid re-actant to the solid reactant in the combustion chamber. In this way it is then possible to regulate the exposure of the solid reactant to the fluid reactant and thus control thrust.

La présente invention décrit un moteur fusée hybride qui comprend un premier réactif solide et au moins une tuyère de poussée et au moins un organe de réglage de combustion mobile à l'intérieur du moteur fusée hybride qui restreint le contact d'un premier réactif fluide avec le réactif solide à l'intérieur de la chambre de combustion. Ainsi il est alors possible de réguler l'exposition du réactif solide au réactif fluide et donc de régler la poussée.

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