SAM-D Trade-Off Study, Electromechanical Control Actuation System (EM/CAS).
Abstract
This report presents a discussion of the application of an electromechanical type actuator to the SAM-D missile. An actuator was not designed, but the preliminary design parameters and component sizes were estimated. The basic conclusion is that a conventional electromechanical actuator using magnetic particle clutches will not fit into the available volume on the SAM-D vehicle. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 02, 1976
- Accession Number
- ADA025232
Entities
People
- Joe L. Byrd