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Nonlinear stability analysis of Apollo aft heat shieldNonlinear structural analysis of stress and buckling pressures of aft heat shield of Apollo spacecraft
Document ID
19680019209
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stricklin, J. A. (Texas A&M Univ. College Station, TX, United States)
Date Acquired
August 4, 2013
Publication Date
June 28, 1968
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-95490
REPT.-68-59
Report Number: NASA-CR-95490
Report Number: REPT.-68-59
Accession Number
68N28681
Funding Number(s)
CONTRACT_GRANT: NGL-44-001-044
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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