ROCKET Russian patent published in 2002 - IPC

Abstract RU 2183816 C2

FIELD: rocketry. SUBSTANCE: the rocket has an engine with a stabilizing device in the form of a body with hinged blades consisting of a base and a plate. The engine is made of composite material, a heat-erosion-resistant coating is made on the rear part of the engine surface in the point of opening of the blades, and the base of each blade is beveled at an angle to the rocket axis and in parallel with the rear part of the engine surface with the heat-erosion-resistant coating, the bevel cross-section is made a triangle one. EFFECT: enhanced reliability of rocket with an engine of composite material in flight at a supersonic flow over of it by gas flow. 3 dwg

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RU 2 183 816 C2

Authors

Shipunov A.G.

Kuznetsov V.M.

Kapustin A.S.

Makhonin V.V.

Maksimov F.A.

Dates

2002-06-20—Published

2000-01-05—Filed