Process for igniting a rocket engine and rocket engine

Details Process for igniting a rocket engine and rocket engine Process for igniting a rocket engine and rocket engine

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 9/95 (2006.01) F02K 9/96 (2006.01)

Patent

CA 2546371

A process for igniting a rocket motor or a rocket engine with a free, molecular oxygen containing hot gas obtained by decomposing at least one ignition system liquid (1) is presented.The rocket motor contains a fuel rich propellant mixture based on fuel and oxidizer, the fuel in the mixture being selected from the group of aluminium, HTBP, GAP, Poly Nimmo and BAMO.The rocket engine uses fuel rich streams of propellant, which streams of propellant are based on a combination of fuel and oxidizer, said fuel being selected from the group of hydrogen, methane and kerosene.

L'invention concerne un procédé permettant d'allumer un moteur de fusée ou un moteur de fusée utilisant un gaz chaud contenant un oxygène à molécules libres obtenu par décomposition d'au moins un liquide (1) de système d'allumage. Ledit moteur de fusée comprend un mélange de propergol riche en carburant à base de carburant et de comburant, le carburant dudit mélange étant sélectionné dans le groupe constitué par aluminium, HTBP, GAP, Poly Nimmo et BAMO. Ce moteur de fusée utilise des flux de comburant riches en carburant, lesdits flux de comburant étant à base d'une combinaison de carburant et de comburant, et le carburant étant sélectionné dans le groupe constitué par hydrogène, méthane et kérosène.

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