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Actions for Development of deployable structures for large space platform systems, part 1.
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Development of deployable structures for large space platform systems, part 1.
Author
Nelson, R. A.
Published
Oct 25, 1982.
Physical Description
1 electronic document
Additional Creators
Cox, R. L.
Online Version
hdl.handle.net
, Connect to this object online.
Full Text available online
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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Eight 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.
Other Subject(s)
SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19830007075.
Accession ID: 83N15346.
REPT-2-32300/2R-53215-PT-1.
NASA-CR-170690.
NAS 1.26:170690.
Terms of Use and Reproduction
No Copyright.
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