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MPD thruster technologyMPD (MagnetoPlasmaDynamic) thrusters demonstrated between 2000 and 7000 seconds specific impulse at efficiencies approaching 40 percent, and were operated continuously at power levels over 500 kW. These demonstrated capabilities, combined with the simplicity and robustness of the thruster, make them attractive candidates for application to both unmanned and manned orbit raising, lunar, and planetary missions. To date, however, only a limited number of thruster configurations, propellants, and operating conditions were studied. The present status of MPD research is reviewed, including developments in the measured performance levels and electrode erosion rates. Theoretical studies of the thruster dynamics are also described. Significant progress was made in establishing empirical scaling laws, performance and lifetime limitations and in the development of numerical codes to simulate the flow field and electrode processes.
Document ID
19910022848
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Myers, Roger M.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Mantenieks, Maris A.
(NASA Lewis Research Center Cleveland, OH., United States)
Lapointe, Michael R.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-105242
E-6569
NAS 1.15:105242
AIAA PAPER 91-3568
Report Number: NASA-TM-105242
Report Number: E-6569
Report Number: NAS 1.15:105242
Report Number: AIAA PAPER 91-3568
Meeting Information
Meeting: Conference on Advanced Space Exploration Initiative Technologies
Location: Cleveland OH
Country: United States
Start Date: September 4, 1991
End Date: September 6, 1991
Sponsors: OAI, AIAA, NASA
Accession Number
91N32162
Funding Number(s)
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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