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Standardization and program effect analysis (Study 2.4). Volume 2: Equipment commonality analysisThe feasibility and cost savings of using flight-proven components in designing spacecraft were investigated. The components analyzed were (1) large space telescope, (2) stratospheric aerosol and gas equipment, (3) mapping mission, (4) solar maximum mission, and (5) Tiros-N. It is concluded that flight-proven hardware can be used with not-too-extensive modification, and significant savings can be realized. The cost savings for each component are presented.
Document ID
19760015169
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Shiokari, T.
(Aerospace Corp. El Segundo, CA, United States)
Date Acquired
September 3, 2013
Publication Date
July 31, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-147106
ATR-76(7364)-1-VOL-2
Report Number: NASA-CR-147106
Report Number: ATR-76(7364)-1-VOL-2
Accession Number
76N22257
Funding Number(s)
CONTRACT_GRANT: NASW-2727
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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