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Dynamic loads analysis of space vehicle systems - Launch and exit phaseDynamic loads analysis of space vehicle systems - analytical techniques, ground wind induced loads, engine start and shutdown and launch, atmospheric disturbance, and frequency response
Document ID
19660022640
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Appleby, B. A.
Martin, J. D.
Schuett, R. H.
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
GDC-DDE66-012
NASA-CR-76502
Accession Number
66N31930
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: JPL-950994
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FREQUENCY RESPONSE
SPACE VEHICLE
STRUCTURAL DYNAMICS
DYNAMIC LOAD

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