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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| creator | HARRIS, III JOHN A JOHNSON BRADLEY C GEHRON MICHAEL J |
| description | An injector assembly for a rocket engine includes a thermal insulating layer adjacent to an oxidizer cavity. |
| format | Patent |
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| language | eng |
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| subjects | 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 |
| title | ROCKET ENGINE INJECTOR ASSEMBLY WITH CRYOGENIC CAVITY INSULATION |
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