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    JPL nuclear electric propulsion task (1993)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The development of lithium magnetoplasmadynamic (MPD) thrusters at JPL is discussed. The following topics are presented in vugraph form: mercury vapor mass flow control; porous tungsten vaporizer and housing; the lithium vaporizer experiment; a dry box for handling solid lithium; MPD thruster electrode modeling; engine lifetime definitions; cathode failure modeling; cathode erosion modeling; cathode thermal modeling; near cathode plasma model regions; cathode work function modeling; anode work function modeling; and radiation-cooled anodes.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: NASA. Lewis Research Center, Nuclear Propulsion Technical Interchange Meeting, Volume 2; p 1027-1040
    Format: application/pdf
    Location Call Number Expected Availability
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