Recent work on an RF ion thrusterPreliminary results of an RF ion thruster using an immersed coupler in an argon discharge are presented. Conventional ion accelerator optics are used to extract an ion beam. An account is given of the operation of an unoptimized thruster over a range of input powers, propellant flow rates, frequencies, and magnetic field strengths. It is noted that lifetime and overall efficiency factors have not yet been extensively investigated. The results obtained establish the feasibility of this approach and the potential for future improvements. The conical coil employed to couple RF power into the discharge is placed inside the discharge vessel. The discharge is self-sustained by 100-150 MHz RF power at low environmental pressures (approximately 0.00001 torr). The ion extraction is accomplished by conventional accelerator grid optics from an unoptimized 8 cm diameter ion thruster.
Document ID
19810051221
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lee, R. Q. (NASA Lewis Research Center Cleveland, OH, United States)
Nakanishi, S. (NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 81-0678Report Number: AIAA PAPER 81-0678
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Las Vegas, NV
Country: US
Start Date: April 21, 1981
End Date: April 23, 1981
Sponsors: Japan Society for Aeronautical and Space Sciences, AIAA, DGLR