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New approach for evaluating transient loads for environmental testing of spacecraftEvaluation of transient loads for environmental testing of spacecraft using multiple degree of freedom model
Document ID
19670015843
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Howlett, J. T. (NASA Langley Research Center Hampton, VA, United States)
Raney, J. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Structural Mechanics
Accession Number
67N25172
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRANSIENT LOAD
MATHEMATICAL MODEL
SPACECRAFT MODEL
MULTIPLE-DEGREE-OF-FREEDOM SYSTEM
ENVIRONMENTAL TESTING

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