Rocket engine and method for controlling combustion in the...

F - Mech Eng,Light,Heat,Weapons – 02 – K

Patent

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F02K 9/58 (2006.01) F02K 9/28 (2006.01) F02K 9/32 (2006.01) F02K 9/72 (2006.01) F02K 9/95 (2006.01)

Patent

CA 2726212

Supply of a liquid component in a combustion chamber of a rocket engine is controlled by a feed valve provided with an obturator mobile between a pen position and a closed position of at least one supply pipe, which has an inlet that communicates with a tank for containing the liquid component and an outlet that communicates with the combustion chamber; the displacement of the obturator from its closed position to its open position being triggered by a pressurized fluid supplied to the outlet of the supply pipe.

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