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Cold solid propellant motor has stop-restart capabilitySolid propellant rocket is kept and fired at low temperatures in launch vehicles or spacecraft. The motor is capable of developing a specific impulse comparable to that of liquid propellant motors, is started, stopped, and restarted, and is stored in space without solar radiation causing hot spots on the motor casing.
Document ID
19660000671
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Hendel, F. J.
Date Acquired
August 3, 2013
Publication Date
December 1, 1966
Subject Category
Materials
Report/Patent Number
JPL-836
Report Number: JPL-836
Accession Number
66B10673
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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