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Development of graphite composite adapter for Galileo spacecraftThis paper discusses the Galileo spacecraft adapter: its interface loads and stiffness capability; configuration design/analysis methodology; verification of buckling margin, local stresses, and mass properties; and the basis for graphite-epoxy material selections and tooling approach, as well as the fabrication, layup, machining, assembly, and drilling processes.
Document ID
19850033828
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Archer, J. S. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Brown, R. L. (TRW, Inc. TRW Space and Technology Group, Redondo Beach, CA, United States)
Cowgill, P. J. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Technology vectors
Location: Reno, NV
Start Date: April 3, 1984
End Date: April 5, 1984
Accession Number
85A15979
Distribution Limits
Public
Copyright
Other

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