Method for controlling the utilization of fluid bipropellant in

Power plants – Reaction motor – Method of operation

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Details

60240, 60259, A02K 950

Patent

active

047221836

ABSTRACT:
A method is provided for controlling the utilization of a fluid bipropellant including two respective constituents separately in respective tanks aboard a spacecraft for consumption by a spacecraft rocket engine, comprising the steps of actuating the rocket engine; during the actuation of the rocket engine, providing a flow of bipropellant constituents to the rocket engine in a first proportion; after the actuation of the rocket engine, measuring the amount of at least one bipropellant constituent in a bipropellant tank containing the constituent; adjusting a pressure level within at least one bipropellant tank relative to a pressure level within another bipropellant tank based upon the amount of said at least one bipropellant constituent in a bipropellant tank containing said at least one constituent; after the measuring step, actuating the rocket engine; during the actuation of the rocket engine after the measuring step, providing a flow of bipropellant constituents to the rocket engine in a second proportion based upon said adjusted pressure level within said at least one bipropellant tank relative to a pressure level within said another bipropellant tank.

REFERENCES:
patent: 2849015 (1958-08-01), Colson
patent: 2860651 (1958-11-01), Davies
patent: 2860652 (1958-11-01), Badger
patent: 3058043 (1962-10-01), Schroeder
patent: 3058303 (1962-10-01), Mulready
patent: 3073110 (1963-01-01), Dillaway
patent: 3080876 (1963-03-01), Adamson
patent: 3095740 (1963-07-01), Peacock
patent: 3114381 (1963-12-01), Klose
patent: 3172254 (1965-03-01), Wright
patent: 3745338 (1973-07-01), Joyce
patent: 4541238 (1985-09-01), Scheller

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