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A study of mass data storage technology for rocket engine dataThe results of a nine month study program on mass data storage technology for rocket engine (especially the Space Shuttle Main Engine) health monitoring and control are summarized. The program had the objective of recommending a candidate mass data storage technology development for rocket engine health monitoring and control and of formulating a project plan and specification for that technology development. The work was divided into three major technical tasks: (1) development of requirements; (2) survey of mass data storage technologies; and (3) definition of a project plan and specification for technology development. The first of these tasks reviewed current data storage technology and developed a prioritized set of requirements for the health monitoring and control applications. The second task included a survey of state-of-the-art and newly developing technologies and a matrix-based ranking of the technologies. It culminated in a recommendation of optical disk technology as the best candidate for technology development. The final task defined a proof-of-concept demonstration, including tasks required to develop, test, analyze, and demonstrate the technology advancement, plus an estimate of the level of effort required. The recommended demonstration emphasizes development of an optical disk system which incorporates an order-of-magnitude increase in writing speed above the current state of the art.
Document ID
19920004892
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ready, John F.
(Honeywell, Inc. Minneapolis, MN, United States)
Benser, Earl T.
(Honeywell, Inc. Minneapolis, MN, United States)
Fritz, Bernard S.
(Honeywell, Inc. Minneapolis, MN, United States)
Nelson, Scott A.
(Honeywell, Inc. Minneapolis, MN, United States)
Stauffer, Donald R.
(Honeywell, Inc. Minneapolis, MN, United States)
Volna, William M.
(Honeywell, Inc. Minneapolis, MN, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-185272
NAS 1.26:185272
Report Number: NASA-CR-185272
Report Number: NAS 1.26:185272
Accession Number
92N14110
Funding Number(s)
CONTRACT_GRANT: NAS3-25714
PROJECT: RTOP 582-01-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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