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
Link To Document :
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