Low thrust monopropellant engine

Power plants – Reaction motor

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60 3946M, F02K 944

Patent

active

042889820

ABSTRACT:
A low thrust monopropellant engine having a conventional body and nozzle configuration wherein the monopropellant fuel is fed into the thruster with dual injection tubes via an injector shell with dual spray jets formed therein. The spray jets are positioned generally opposed to each other. A heater-screen pack combination thermally decomposes the fuel after injection into the combustion chamber of the thruster.

REFERENCES:
patent: 981481 (1911-01-01), Shoenberg
patent: 2378348 (1945-06-01), Wilmes et al.
patent: 3054252 (1962-09-01), Beckett et al.
patent: 3236699 (1966-02-01), Pugh et al.
patent: 3312539 (1967-04-01), Marshall et al.
patent: 3361599 (1968-01-01), Barganier
patent: 3375109 (1968-03-01), Peters
patent: 3696616 (1972-10-01), Lucas
"Monopropellant Hydrazine Resistojet", TRW Report 20266-6024-RO-00; Mar., 1973.

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