ROCKET ENGINE INJECTOR ASSEMBLY WITH CRYOGENIC CAVITY INSULATION

An injector assembly for a rocket engine includes a thermal insulating layer adjacent to an oxidizer cavity.

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Bibliographische Detailangaben
Hauptverfasser:	HARRIS, III JOHN A, JOHNSON BRADLEY C, GEHRON MICHAEL J
Format:	Patent
Sprache:	eng
Schlagworte:	APPLYING LIQUIDS OR OTHER FLUENT MATERIALS TO SURFACES, IN GENERAL ATOMISING APPARATUS BLASTING COMBINED OPERATIONS COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINE TOOLS MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR NOZZLES OTHER WORKING OF METAL PERFORMING OPERATIONS SPRAYING APPARATUS SPRAYING OR ATOMISING IN GENERAL TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS
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