Assessment of the Tribiological Requirements of Advanced Spacecraft Mechanisms
Abstract
A survey was conducted of existing technologies for moving mechanical assemblies used in spacecraft applications. The purpose was to identify areas where future requirements for lifetimes in excess of ten years with anticipated speeds, loads, and temperatures might not be satisfied. Some specific mechanisms, such as momentum/reaction wheels, high speed turbines, pointing and tracking mechanisms, despin mechanisms, and gimbal mechanisms, were identified as areas for potential application of existing but unused technologies. Two major problem areas identified involve boundary regime lubrication and lubricant supply (active or passive) for long life. Areas where substantial, near term improvements appear practical include the use of hybrid bearings, new synthetic fluid lubricants, new bearing retainer materials, and properly designed solid film lubricants.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 30, 1991
- Accession Number
- ADA241674
Entities
People
- Michael R. Hilton
- Paul D. Fleischauer
Organizations
- The Aerospace Corporation