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Transient loads from thrust excitation - Space vehicle design criteria /structures/Analysis of transient loads produced by ignition of rocket engine during launch and flight operations for solid and liquid propellant rocket engines
Document ID
19710014805
Acquisition Source
Legacy CDMS
Document Type
Special Publication (SP)
Date Acquired
September 2, 2013
Publication Date
February 1, 1969
Subject Category
Structural Mechanics
Report/Patent Number
NASA-SP-8030
Accession Number
71N24281
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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