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IRS organigramCharts and graphs relative to magnetoplasmadynamic (MPD) thruster technology are given. The research activities at the Institute of Space Transportation, University of Stuttgart, are summarized. Information is given on the Institute's Electric Propulsion and Plasma Wind Tunnel; thermal arcjet research; the nozzle-type thruster, DT-IRS; nozzle-type MPD thrusters; a hot anode thruster; the DT6 thruster; the ZT-1 thruster; the cylindrical MPD thruster; and a comparison of continuous and quasi-steady MPD.
Document ID
19920000835
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Messerschmid, Ernst
(Stuttgart Univ.)
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
92N10053
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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