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Hex ball torque testA series of torque tests were performed on four flight-type hex ball universal joints in order to characterize and determine the actual load-carrying capability of this device. The universal joint is a part of manual actuation rods for scientific instruments within the Hubble Space Telescope. It was found that the hex ball will bind slightly during the initial load application. This binding did not affect the function of the universal joint, and the units would wear-in after a few additional loading cycles. The torsional yield load was approximately 50 ft-lb, and was consistent among the four test specimens. Also, the torque required to cause complete failure exceeded 80 ft-lb. It is concluded that the hex ball universal joint is suitable for its intended applications.
Document ID
19860014502
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Robinson, B. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Foster, C. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-86534
NAS 1.15:86534
Report Number: NASA-TM-86534
Report Number: NAS 1.15:86534
Accession Number
86N23973
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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