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Long-duration life tests of slip ring capsule assemblies for inertial guidance platformsEight slip ring capsules, each having 80 or 100 circuits, were operated for time periods ranging from 14,300 hours to 24,700 hours. The test mode simulated the motion of gimbal axes of the Saturn inertial guidance the platform in an organic free nitrogen environment. Computer-compiled noise data (approximately 45,000 recordings) were graphed as a function of test time and position within the capsules and as extreme probability distributions. Greater than ninety-nine percent of the noise measurements for the capsules with sufficient lubrication were less than 10 milliohms. Capsules with glass dielectrics did not perform significantly differently than those with filled epoxy dielectrics. The initial wear mode of prow formation was followed by rider wear. After 10 to the 8th power wipes, ring wear depth did not exceed the surface finish and the radial rider wear depth was less than 13 microns.
Document ID
19740021004
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cole, S. R.
(Poly-Scientific Div., Litton Precision Products, Inc. Blacksburg, VA, United States)
Glossbrenner, E. W.
(Poly-Scientific Div., Litton Precision Products, Inc. Blacksburg, VA, United States)
Date Acquired
September 3, 2013
Publication Date
March 6, 1974
Subject Category
Navigation
Report/Patent Number
MO-16673
NASA-CR-138948
Report Number: MO-16673
Report Number: NASA-CR-138948
Accession Number
74N29117
Funding Number(s)
CONTRACT_GRANT: NAS8-29199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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