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The MPD thruster program at JPLThe main topics covered include: (1) the Space Exploration Initiative (SEI) context; (2) critical issues of MPD Thruster design; and (3) the Magnetoplasmadynamic (MPD) Thruster Program at JPL. Under the section on the SEI context the nuclear electric propulsion system and some electric thruster options are addressed. The critical issues of MPD Thruster development deal with the requirements, status, and approach taken. The following areas are covered with respect to the MPD Thruster Program at JPL: (1) the radiation-cooled MPD thruster; (2) the High-Current Cathode Test Facility; (3) thruster component thermal modeling; and (4) alkali metal propellant studies.
Document ID
19920000828
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barnett, John
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Goodfellow, Keith
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Polk, James
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Pivirotto, Thomas
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA. Lewis Research Center, Magnetoplasmadynamic Thruster Workshop
Subject Category
Spacecraft Propulsion And Power
Accession Number
92N10046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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