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Electric thruster models for multimegawatt nuclear electric propulsion mission design

Conference · · AIP Conference Proceedings (American Institute of Physics); (United States)
DOI:https://doi.org/10.1063/1.40150· OSTI ID:5484702
; ;  [1]
  1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 911109 (US)
Three types of electric thrusters currently under development at JPL have potential to support future missions which utilize multimegawatt nuclear electric propulsion. These electric thrusters are the electron bombardment ion thruster, the magnetoplasmadynamic (MPD) thruster, and the electron-cyclotron-resonance (ECR) thruster. The electron bombardment ion thruster is a relatively mature technology which has been developed for operation at kilowatt power levels but will require new development for application in the multimegawatt regime. The MPD engine represents a technology which may be very well suited to steady-state multimegawatt applications but which has been limited to sub-scale (100's of kW) and pulsed (MW) testing thus far. The ECR plasma engine represents a class of very promising new concepts which are still in the basic research phase of development, but which may possess important fundamental advantages over other electric thruster technologies. In this paper, models of these thrusters are described and used to make projections of thruster specific mass, efficiency, and power handling capacity for operation in the multimegawatt regime.
OSTI ID:
5484702
Report Number(s):
CONF-910116--
Conference Information:
Journal Name: AIP Conference Proceedings (American Institute of Physics); (United States) Journal Volume: 217:2
Country of Publication:
United States
Language:
English