NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
High frequency plasma generator for ion thrustersThe results of a program to experimentally develop two new types of plasma generators for 30 cm electrostatic argon ion thrusters are presented. The two plasma generating methods selected for this study were by radio frequency induction (RFI), operating at an input power frequency of 1 MHz, and by electron cyclotron heating (ECH) at an operating frequency of 5.0 GHz. Both of these generators utilize multiline cusp permanent magnet configurations for plasma confinement and beam profile optimization. The program goals were to develop a plasma generator possessing the characteristics of high electrical efficiency (low eV/ion) and simplicity of operation while maintaining the reliability and durability of the conventional hollow cathode plasma sources. The RFI plasma generator has achieved minimum discharge losses of 120 eV/ion while the ECH generator has obtained 145 eV/ion, assuming a 90% ion optical transparency of the electrostatic acceleration system. Details of experimental tests with a variety of magnet configurations are presented.
Document ID
19850008714
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Goede, H.
(TRW Space Technology Labs. Redondo Beach, CA, United States)
Divergilio, W. F.
(TRW Space Technology Labs. Redondo Beach, CA, United States)
Fosnight, V. V.
(TRW Space Technology Labs. Redondo Beach, CA, United States)
Komatsu, G.
(TRW Space Technology Labs. Redondo Beach, CA, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1984
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-174772
NAS 1.26:174772
Report Number: NASA-CR-174772
Report Number: NAS 1.26:174772
Accession Number
85N17023
Funding Number(s)
CONTRACT_GRANT: NAS3-22473
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available