Missile Azimuth Alignment System
Abstract
This patent discloses continuous alignment system for preventing rotation of a missile during on-loading in a launching tube, while permitting a controlled translation of the missile in the launching tube when subjected to external seismic shocks.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 21, 1987
- Accession Number
- ADD013361
Entities
People
- Bettadapur N. Stridhar
- Richard D. Gassler
Organizations
- United States Department of the Air Force