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Hyperelastic Behavior Of Solid Rocket PropellantsOne-page report discusses study of uniaxial stress-vs.-strain relationships of typical highly-filled HTPB solid rocket-propellant materials.
Document ID
19950065461
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Beyer, Rodney (Atlantic Research Corp.)
Graham, Phillip (Atlantic Research Corp.)
Date Acquired
August 17, 2013
Publication Date
June 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 6
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
MFS-28880
Report Number: MFS-28880
ISSN: 0145-319X
Accession Number
95B10302
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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