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Propellant side feedNew solid-propellant configurations increase thrust-to-power ratio of pulsed plasma microthruster and provide possibility of varying thrust. Techniques are adaptable to sputter coating of polymeric material or pulsed ablating light sources.
Document ID
19760000094
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Guman, W. J. (Fairchild Hiller Corp.)
Date Acquired
August 8, 2013
Publication Date
March 1, 1976
Publication Information
Publication: NASA Tech Briefs
Volume: 1
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-11082
Report Number: LAR-11082
ISSN: 0145-319X
Accession Number
76B10094
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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