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A review of the multimegawatt MPD thruster and current mission applications

Authors :
King, D. Q
Sercel, J. C
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

Subjects :
Spacecraft Propulsion And Power

Details

Language :
English
Database :
NASA Technical Reports
Publication Type :
Report
Accession number :
edsnas.19860057904
Document Type :
Report