Gimbal Caging Mechanism.
Abstract
This note describes a mechanism for caging a single-axis gimbal for a satellite application. The caging mechanism consists of two pivoted links that clamp the gimbal shaft in the nominal position. The clamping load is produced by a double toggle mechanism. A nonreusable actuator releases the mechanism on command; a caging override permits unlimited manual release. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 16, 1978
- Accession Number
- ADA056903
Entities
People
- Cornelius M. Sullivan
Organizations
- Massachusetts Institute of Technology