The objective of this program is to identify, validate and assess advantages to the Air Force of using high performance pulsed plasma electric propulsion technology for satellite stationkeeping, attitude control, drag make-up, and solar pressure compensation and to develop pulsed plasma propulsion system/spacecraft integration and design criteria.
Mission Integration Study for Solid Teflon Pulsed Plasma Millipound Propulsion System
1980
183 pages
Report
Keine Angabe
Englisch
Electric & Ion Propulsion , Unmanned Spacecraft , Electric propulsion , Plasma engines , Space propulsion , Stationkeeping , Attitude control systems , Thrusters , Drag , Artificial satellites , Communication satellites , Spacecraft , Auxiliary power plants , Electric power , Pulses , Monopropellants , Tetrafluoroethylene resins , Global positioning system , Missions , Cost analysis , Pulsed plasma propulsion , Defense Satellite Communication System 3 Satellite , Defense Support Program Satellite
One millipound pulsed plasma thruster development
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