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Spacelab output processing system architectural studyTwo different system architectures are presented. The two architectures are derived from two different data flows within the Spacelab Output Processing System. The major differences between these system architectures are in the position of the decommutation function (the first architecture performs decommutation in the latter half of the system and the second architecture performs that function in the front end of the system). In order to be examined, the system was divided into five stand-alone subsystems; Work Assembler, Mass Storage System, Output Processor, Peripheral Pool, and Resource Monitor. The work load of each subsystem was estimated independent of the specific devices to be used. The candidate devices were surveyed from a wide sampling of off-the-shelf devices. Analytical expressions were developed to quantify the projected workload in conjunction with typical devices which would adequately handle the subsystem tasks. All of the study efforts were then directed toward preparing performance and cost curves for each architecture subsystem.
Document ID
19780008697
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
December 8, 1977
Subject Category
Computer Operations And Hardware
Report/Patent Number
NASA-CR-156679
Report Number: NASA-CR-156679
Accession Number
78N16640
Funding Number(s)
CONTRACT_GRANT: NAS5-23438
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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