RESEARCH ON SATELLITE ATTITUDE CONTROL USING PLASMA PINCH ENGINES
Abstract
This report covers theoretical and experimental research of single axis attitude control systems using Pinch Plasma Engines as torquing devices; and describes the experimental apparatus and open and closed loop tests, as well as the analyses which corroborate the test results. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 31, 1964
- Accession Number
- AD0353288