DocumentCode
1329263
Title
Maintainability Design Requirements for Future Space Systems
Author
Peterson, Elmer L.
Author_Institution
Space and Information Systems Division, North American Aviation, Inc., Downey, Calif.
Issue
1
fYear
1966
fDate
5/1/1966 12:00:00 AM
Firstpage
17
Lastpage
21
Abstract
Design requirements which consider maintenance capability can be expected to be quite different for space system application when compared to those currently in use for today´s weapon systems. Needs will vary, as will the base for the definition of quantized criteria. Maximum urgency is placed on crew safety, mission success, and meeting a launch window. The expressions for quantitative maintainability design criteria will shift from the familiar ``Meantime´´ base to one of ``Allowable Time,´´ ``Probability of Repair Within Time Limits,´´ and ``Expenditure of Human Energy.´´ This paper explores the operational requirements for maintainability in future space systems, discusses interface problems, and defines quantized maintainability objectives for the different applications of 1) spacecraft, 2) space stations, 3) boosters, and 4) support equipment.
Keywords
Current measurement; Extraterrestrial measurements; Fault diagnosis; Humans; Maintenance; Safety; Space missions; Space stations; Space vehicles; Weapons;
fLanguage
English
Journal_Title
Reliability, IEEE Transactions on
Publisher
ieee
ISSN
0018-9529
Type
jour
DOI
10.1109/TR.1966.5217585
Filename
5217585
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