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Integrated monopropellant thrusterApplication of vortex amplifier principles to throttling of monopropellant thrusters is described. Integration of flow control, catalyst bed, and thruster nozzle is accomplished by design of thruster. Diagrams of thrusters are provided to show details of construction and operation.
Document ID
19720000501
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mangion, C. (TRW Systems Group)
Date Acquired
August 6, 2013
Publication Date
August 1, 1972
Subject Category
Mechanics
Report/Patent Number
NPO-12004
Report Number: NPO-12004
Accession Number
72B10502
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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