ROCKET ENGINE ADJUSTABLE NOZZLE

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...

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Bibliographische Detailangaben
Hauptverfasser: SMOL'NIKOV V.V, LUZHKOV JU.M
Format: Patent
Sprache:eng ; rus
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Beschreibung
Zusammenfassung: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