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Optimization of armored spherical tanks for storage on the lunar surfaceA redundancy strategy for reducing micrometeroid armoring mass is investigated, with application to cryogenic reactant storage for a regenerative fuel cell (RFC) on the lunar surface. In that micrometeoroid environment, the cryogenic fuel must be protected from loss due to tank puncture. The tankage must have a sufficiently high probability of survival over the length of the mission so that the probability of system failure due to tank puncture is low compared to the other mission risk factors. Assuming that a single meteoroid penetration can cause a storage tank to lose its contents, two means are available to raise the probability of surviving micrometeoroid attack to the desired level. One can armor the tanks to a thickness sufficient to reduce probability of penetration of any tank to the desired level or add extra capacity in the form of space tanks that results in survival of a given number out of the ensemble at the desired level. A combination of these strategies (armor and redundancy) is investigated.
Document ID
19930041869
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bents, D. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Knight, D. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: IECEC '92; Proceedings of the 27th Intersociety Energy Conversion Engineering Conference, San Diego, CA, Aug. 3-7, 1992. Vol. 1 (A93-25851 09-44)
Publisher: Society of Automotive Engineers, Inc.
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
93A25866
Funding Number(s)
PROJECT: RTOP 326-81-10
Distribution Limits
Public
Copyright
Other

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