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System applications of the fault tolerant memoryConventional memory technologies currently employed in aerospace applications contribute at least fifty percent to system unreliability (where the system includes CPU, I/O and memory). A fault tolerant memory performs both error correction and memory replacement at the bit plane level. To determine the effects of system design of using a fault tolerant memory in space applications, analysis was performed to determine tradeable hardware configurations that meet the reliability goals of each program. The candidate configurations, which included redundant elements of the computer system with both conventional and fault tolerant memories, were then traded in terms of selection criteria of cost, weight, volume, and power. These trade studies demonstrated that a fault tolerant memory provided significant advantages in terms of cost, weight, and volume. The memory selected for this analysis was a recently developed five fault tolerant memory.
Document ID
19760029877
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murphy, L. J.
(IBM Corp. Federal Systems Div., Huntsville, Ala., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Subject Category
Computer Operations And Hardware
Report/Patent Number
AAS PAPER 75-296
Report Number: AAS PAPER 75-296
Meeting Information
Meeting: Meeting on Space Shuttle Missions of the 80''s
Location: Denver, CO
Start Date: August 26, 1975
End Date: August 28, 1975
Sponsors: AAS, AIAA, IEEE, ORSA, and IMS,
Accession Number
76A12843
Funding Number(s)
CONTRACT_GRANT: NAS8-31312
Distribution Limits
Public
Copyright
Other

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