ROCKET ENGINE NOZZLE SUPERSONIC SECTION Russian patent published in 2010 - IPC F02K9/97 

Abstract RU 2379540 C1

FIELD: engines and pumps.

SUBSTANCE: rocket engine supersonic section comprises carcass, erosion proof and heat insulation coats. Said carcass is made from low-melting material screen. Said erosion proof coat is arranged on carcass inner side. Said heat insulation coat is arranged outside the carcass. Aforesaid erosion proof coat is made from molded material primarily, carbon fiber-reinforced plastica, with its thickness regularly decreasing towards nozzle edge. Low-melting material of the carcass is feature melting point lower than gasification temperature of heat insulation material.

EFFECT: reduced weight, overheating protection.

2 dwg

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RU 2 379 540 C1

Authors

Solomonov Jurij Semenovich

Cherepov Vladimir Ivanovich

Lobanov Oleg Aleksandrovich

Peremyslovskaja Anna Georgievna

Dates

2010-01-20Published

2008-06-09Filed