COMPOSITE MATERIALS HOUSING OF SOLID PROPELLANT ROCKET ENGINE

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 wit...

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Bibliographische Detailangaben
Hauptverfasser:	MEDVEDEV A.A, ROMANOV A.F, MAJOROV B.G, ZAKHAROV V.A, ALEEV V.A
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	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