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Payload shrouds structural optimization study Final reportComputer programs for synthesizing structural arrangements for ring-stiffened, honeycomb sandwich, and ring-stringer stiffened methods of construction for Saturn nose fairings
Document ID
19670016428
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hendrix, E. S. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
August 3, 2013
Publication Date
November 30, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-83809
LMSC/HREC-A712615
Report Number: NASA-CR-83809
Report Number: LMSC/HREC-A712615
Accession Number
67N25757
Funding Number(s)
CONTRACT_GRANT: NAS8-15485
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STRUCTURAL DESIGN
FAIRING
COMPUTER PROGRAM
SATURN LAUNCH VEHICLE
NOSE CONE

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