ROCKET ENGINE ADJUSTABLE NOZZLE Russian patent published in 2005 - IPC

Abstract RU 2244147 C2

FIELD: rocket engine.

SUBSTANCE: proposed nozzle is made from carbon-to-carbon composite material; nozzle is provided with stationary bell mouth, extensible attachment mounted on load-bearing ring for locking the extensible attachment of collet. Load-bearing ring is provided with T-shaped slots in which collets are inserted. Collects are also made from carbon-to-carbon composite material and are secured by means of thermo-resistant adhesive.

EFFECT: enhanced tightness of nozzle at low mass of collet joint; enhanced operational reliability.

3 dwg

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RU 2 244 147 C2

Authors

Smol'Nikov V.V.

Luzhkov Ju.M.

Dates

2005-01-10Published

2002-08-26Filed