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Low thrust monopropellant engineThe engine has a conventional body and nozzle configuration. The monopropellant fuel is fed into the thruster with dual injection tubes via an injector shell with dual spray jets. 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.
Document ID
19820010440
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Kuenzly, J. D. (TRW, Inc., Redondo Beach Calif., United States)
Date Acquired
September 4, 2013
Publication Date
September 15, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-819029
Patent Application Number: US-PATENT-APPL-SN-971474
Patent Number: NASA-CASE-GSC-12194-2
Patent Number: US-PATENT-4,288,982
Accession Number
82N18314
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-GSC-12194-2|US-PATENT-4,288,982
Patent Application
US-PATENT-APPL-SN-819029|US-PATENT-APPL-SN-971474

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