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The NASA Electric Propulsion programIt is pointed out that the NASA Electric Propulsion program is aimed at providing technology for auxiliary and primary propulsion functions for earth-orbital and planetary space missions. Efforts in electrostatic propulsion include analyses of ion propulsion for Geosynchronous (GEO) and planetary spacecraft, continued preflight efforts associated with the Ion Auxiliary Propulsion System (IAPS), and research and technology for advanced and simplified ion thruster systems. In the area of electromagnetic propulsion, studies were conducted regarding the feasibility and impacts of the use of electromagnetic launchers. Research on magnetoplasmadynamic (MPD) thrusters, electromagnetic launchers, and Hall current thrusters was also performed. Studies in the electrothermal sector included an evaluation of electric propulsion options for the Space Station, taking into account also resistojets, a pulsed electrothermal thruster, and arc jets.
Document ID
19850034226
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Byers, D. C.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Tokyo
Country: Japan
Start Date: May 28, 1984
End Date: May 31, 1984
Sponsors: Japan Society for Areonautical and Space Sciences, AIAA, and DGLR
Accession Number
85A16377
Distribution Limits
Public
Copyright
Other

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