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Viking orbiter 1975 articulation control actuatorsThe articulation subsystem actuators were rigorously tested in severe environments. They were operated through temperature ranges from -73 C to +121 C. In each case the temperature rate of change was at maximum. The actuator under test at room temperature was put into a pre-chilled or preheated chamber. Satisfactory performance was obtained throughout this full temperature range and under the temperature shock conditions above. However, at temperatures below -78 C some leakage was experienced through the O-ring seal around the shaft. The actuators were subjected to severe vibration and 500 g shock test with a time duration of 0.0007 seconds. The scan actuator was life tested by operating it from stop to stop through 2,000 cycles with 20,000 start-stop procedures randomly distributed through the 2,000 cycles.
Document ID
19740003582
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Perkins, G. S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 7, 2013
Publication Date
October 1, 1973
Publication Information
Publication: NASA. Langley Res. Center The 8th Aerospace Mech. Symp.
Subject Category
Machine Elements And Processes
Accession Number
74N11695
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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