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Conceptual design study. Science and Applications Space Platform (SASP). Final briefingThe modularity, shape, and size of the recommended platform concept offers a low investment, early option to demonstrate the system; flexibility to conservative growth; adaptability to great variety of multi or dedicated payload groups; and good dispersion and viewing freedom for payloads. Platform configuration effectively supports 80 to 85% of the NASA/OSS and OSTA payloads. The subsystem approaches recommended are based on cost effective distribution of functions.
Document ID
19840015602
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:173520
MDC-G9300
NASA-CR-173520
Report Number: NAS 1.26:173520
Report Number: MDC-G9300
Report Number: NASA-CR-173520
Accession Number
84N23670
Funding Number(s)
CONTRACT_GRANT: NAS8-33592
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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