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AX-5 space suit reliability modelThe AX-5 is an all metal Extra-vehicular (EVA) space suit currently under consideration for use on Space Station Freedom. A reliability model was developed based on the suit's unique design and on projected joint cycle requirements. Three AX-5 space suit component joints were cycled under simulated load conditions in accordance with NASA's advanced space suit evaluation plan. This paper will describe the reliability model developed, the results of the cycle testing, and an interpretation of the model and test results in terms of projected Mean Time Between Failure for the AX-5. A discussion of the maintenance implications and life cycle for the AX-5 based on this projection is also included.
Document ID
19900062339
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reinhardt, AL
(NASA Ames Research Center Moffett Field, CA; USAF, Office of Scientific Research, Washington, DC, United States)
Magistad, John
(San Jose State University CA, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Man/System Technology And Life Support
Report/Patent Number
SAE PAPER 901361
Accession Number
90A49394
Distribution Limits
Public
Copyright
Other

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