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Helicon Wave Physics Impacts on Electrodeless Thruster DesignEffective generation of helicon waves for high density plasma sources is determined by the dispersion relation and plasma power balance. Helicon wave plasma sources inherently require an applied magnetic field of .01-0.1 T, an antenna properly designed to couple to the helicon wave in the plasma, and an rf power source in the 10-100 s of MHz, depending on propellant choice. For a plasma thruster, particularly one with a high specific impulse (>2000 s), the physics of the discharge would also have to address the use of electron cyclotron resonance (ECR) heating and magnetic expansion. In all cases the system design includes an optimized magnetic field coil, plasma source chamber, and antenna. A preliminary analysis of such a system, calling on experimental data where applicable and calculations where required, has been initiated at Glenn Research Center. Analysis results showing the mass scaling of various components as well as thruster performance projections and their impact on thruster size are discussed.
Document ID
20070032049
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Gilland, James
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
August 23, 2013
Publication Date
March 17, 2003
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
IEPC-0150
Report Number: IEPC-0150
Meeting Information
Meeting: International Electric Propulsion Conference ERPS
Location: Toulouse
Country: France
Start Date: March 17, 2003
End Date: March 21, 2003
Funding Number(s)
CONTRACT_GRANT: NCC3-860
WBS: WBS 22-755-70-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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