SOLID-PROPELLANT ROCKET ENGINE Russian patent published in 2005 - IPC

Abstract RU 2267024 C1

FIELD: rocketry.

SUBSTANCE: proposed solid-propellant rocket engine contains combustion chamber with front and nozzle faces, powder charge with unrestricted nozzle end face and igniter on nozzle face. Igniter in arranged in space formed by unrestricted nozzle end face of charge and cavity in nozzle face. Support made of flexibly deformable material is installed on front face of combustion chamber.

EFFECT: improved efficiency of nozzle igniter.

2 dwg

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RU 2 267 024 C1

Authors

Bol'Shakov A.N.

Krejer K.V.

Dates

2005-12-27—Published

2004-03-30—Filed