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Development of deployable structures for large space platform systems, part 1Eight deployable platform design objectives were established: autodeploy/retract; fully integrated utilities; configuration variability; versatile payload and subsystem interfaces; structural and packing efficiency; 1986 technology readiness; minimum EVA/RMS; and Shuttle operational compatibility.
Document ID
19830007075
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cox, R. L. (Vought Corp. Dallas, TX, United States)
Nelson, R. A. (Vought Corp. Dallas, TX, United States)
Date Acquired
September 4, 2013
Publication Date
October 25, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-170690
NAS 1.26:170690
REPT-2-32300/2R-53215-PT-1
Report Number: NASA-CR-170690
Report Number: NAS 1.26:170690
Report Number: REPT-2-32300/2R-53215-PT-1
Accession Number
83N15346
Funding Number(s)
CONTRACT_GRANT: NAS8-34678
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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