COMPOSITE MATERIALS HOUSING OF SOLID PROPELLANT ROCKET ENGINE Russian patent published in 1998 - IPC

Abstract RU 2108476 C1

FIELD: mechanical engineering; solid propellant rocket engines. SUBSTANCE: housing has load bearing shell 1 with flanges 2,3 located at pole holes of bottom plates 4,5. Shell is lined with rubber-like heat-shielding coating 6 from inside. Ring belt zones 7 are found between coating 6 and shell 1 with flanges in bottom plates. Flanges are connected with load bearing shell by flexibly elastic gaskets 9. EFFECT: improved quality, reliability and strength of engine housing provided by use of proposed method of fastening of heat-shielding coating and shell. 2 cl, 2 dwg

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RU 2 108 476 C1

Authors

Majorov B.G.

Medvedev A.A.

Romanov A.F.

Aleev V.A.

Zakharov V.A.

Dates

1998-04-10Published

1996-01-24Filed