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A review of the multimegawatt MPD thruster and current mission applications
- Publication Year :
- 1986
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1986.
-
Abstract
- The magnetoplasmadynamic (MPD) thruster is potentially capable of providing 20-200 N of steady-state thrust, at 1000-20,000 s specific impulse while consuming a variety of propellants and megawatts of DC power. The specific impulse and power capacity put the MPD thruster in a class separate from other electric propulsion engines. Several types of missions are enhanced by the unique capabilities of a nuclear-electric driven MPD thruster and these include earth-orbit raising, cis-lunar transportation, and planetary exploration. This paper describes current MPD thruster technology, and several missions typical of the above cited categories.
- Subjects :
- Spacecraft Propulsion And Power
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Publication Type :
- Report
- Accession number :
- edsnas.19860057904
- Document Type :
- Report