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Space Station long term lubrication analysis. Phase 1 preliminary tribological surveyIncreases in the size, complexity, and life requirements of satellites and space vehicles have put increasing demands on the lubrication requirements for trouble-free service. Since the development costs of large systems are high, long lives with minimum maintenance are dictated. The Space Station represents the latest level of size and complexity in satellite development; it will be nearly 100 meters in major dimensions and will have a life requirement of thirty years. It will have numerous mechanisms critical to its success, some of which will be exposed to the space environment. Designing long-life lubrication systems and choosing appropriate lubricants for these systems will be necessary for their meeting the requirements and for avoiding failures with associated dependent mechanisms. The purpose of this program was to identify the various critical mechanisms and review their designs during the overall design and development stage so that problem areas could be avoided or minimized prior to the fabrication of hardware. The specific objectives were fourfold: (1) to perform a tribology survey of the Space Station for the purpose of documenting each wear point as to materials involved, environmental conditions, and operating characteristics; (2) to review each wear point (point of relative motion) as to the lubrication used and substrate materials selected in the context of its operating characteristics and the environmental conditions imposed; (3) to make recommendations for improvement in areas where the lubricant chosen and/or where the substrate (materials of the wear couple) are not considered optimum for the application; and (4) to make or recommend simulated or full scale tests in tribological areas where the state-of-the-art is being advanced, in areas where new designs are obviously being employed and a critical review would indicate that problems are a strong possibility, and/or where excessive wear, a malfunction, or excessive leakage would create fluid systems problems or contamination of exposed optical equipment.
Document ID
19920024972
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dufrane, K. F. (Battelle Columbus Labs. OH, United States)
Kannel, J. W. (Battelle Columbus Labs. OH, United States)
Lowry, J. A. (Battelle Columbus Labs. OH, United States)
Montgomery, E. E. (Spectra Research Systems, Inc., Huntsville AL., United States)
Date Acquired
September 6, 2013
Publication Date
September 21, 1990
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.26:184365
NASA-CR-184365
Accession Number
92N34216
Funding Number(s)
CONTRACT_GRANT: NAS8-36655
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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