LOW-THRUST LIQUID PROPELLANT ROCKET ENGINE CHAMBER Russian patent published in 2014 - IPC F02K9/62 

Abstract RU 2532640 C2

FIELD: engines and pumps.

SUBSTANCE: chamber comprises a mixing head with tracts of fuel components supply and nozzle elements, a flange for fixation to an object, bodies of the chamber with the combustion chamber and the nozzle, attached to the mixing head via an adapter. According to the invention the flange for fixation of the chamber to the object is installed on the adapter near the combustion chamber and is located in the zone of the seating surface of the adapter and the mixing head, the adapter is connected to the mixing head along the outer seating surface, and end and inner cylindrical sections have a gap between appropriate surfaces of the mixing head.

EFFECT: reduced thermal flows towards an object.

2 cl, 2 dwg

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Authors

Kazankin Filipp Andreevich

Beshenev Jurij Aleksandrovich

Semkin Evgenij Vladimirovich

Dates

2014-11-10Published

2010-11-17Filed