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Quasi-elastic failure analysis of a solid- propellant rocket motor under thermal variations.Elastic failure analysis method for solid propellant rocket motors, considering crack growth under thermally induced stresses
Document ID
19680063743
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Knauss, W. G.
Date Acquired
August 4, 2013
Publication Date
November 1, 1968
Subject Category
Structural Mechanics
Meeting Information
Meeting: SOLID PROPELLANT ROCKET CONFERENCE
Location: WASHINGTON, DC
Country: US
Start Date: July 18, 1966
End Date: July 20, 1966
Sponsors: INTERAGENCY CHEMICAL ROCKET PROPULSION GROUP, AIAA
Accession Number
68A44715
Funding Number(s)
CONTRACT_GRANT: NSG-172-60
Distribution Limits
Public
Copyright
Other

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