NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Design of a high-speed reliable ball bearingA high-speed, reliable ball bearing has been designed for at least fifteen years of operation in space effectors, MWA's, and RWA's. Advanced bearing concepts have been used in this design, such as: no ball retainer, which eliminates all retainer-related problems; an external lubricazing system that will supply the lubricant at a specified flow rate; and a cartridge assembly that will allow the instrument user to purchase a ready to use bearing assembly, with lubricator. Currently, two assemblies are on life test at 12,000 RPM and have accumulated over 20,000 hours each, with consistent low-torque losses. This paper will describe each of the salient features.
Document ID
19940028808
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Singer, Herbert B.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Gelotte, Erik
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Publication Information
Publication: NASA. Lewis Research Center, The 28th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
94N33314
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available