Accession Number:

AD0353288

Title:

RESEARCH ON SATELLITE ATTITUDE CONTROL USING PLASMA PINCH ENGINES

Descriptive Note:

Final summary status rept.

Corporate Author:

REPUBLIC AVIATION CORP FARMINGDALE NY

Personal Author(s):

Report Date:

1964-08-31

Pagination or Media Count:

64.0

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

Subject Categories:

  • Electric and Ion Propulsion
  • Rocket Engines
  • Unmanned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE