Coolable rocket nozzle for a rocket engine

Power plants – Combustion products used as motive fluid – With addition of steam and/or water

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Details

60 3956, 60 3959, F02C 700

Patent

active

055820000

ABSTRACT:
This invention relates to rocket engines which have a rocket nozzle for expanding hot, highly pressurized rocket gases and more particularly, to a high expansion ratio nozzle for such an engine by flowing the water along a wall to provide additional cooling.

REFERENCES:
patent: 3734639 (1973-05-01), Short
patent: 3921389 (1975-11-01), Kawaguchi
patent: 4537023 (1985-08-01), Nakamura et al.
patent: 4550561 (1985-11-01), Coffinberry
patent: 4662171 (1987-05-01), Jackson et al.
patent: 4928478 (1990-05-01), Maslek
patent: 4982564 (1991-01-01), Hines
patent: 5133180 (1992-07-01), Horner et al.

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