Ion source with particular grid assembly

Electric lamp and discharge devices – With positive or negative ion acceleration – Plural apertured electrodes

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313268, 60202, H01J 2700, F02K 900

Patent

active

048734675

ABSTRACT:
An ion source has the typical chamber wherein ions are produced and caused to be propelled outwardly through at least a pair of grids which have a mutually-aligned respective plurality of apertures. Thus, there are the usual cathode, anode, magnet assembly, ionizable gas inlet and supporting power supplies as well as neutralizing means. First and second grids each have an integrally-formed peripheral marginal portion. A support element has a shape which matches and overlies the marginal portion of one grid, while a clamp has a shape which matches that of and overlies the other marginal portion. The support element and clamp are secured together. First and second mutually-aligned seats are successively spaced around the respective marginal portions. A plurality of insulators, each having of circular cross-section, are individually seated between the two different marginal portions in a manner to cause general alignment while enabling radial movement due to thermal expansion of the marginal portions relative to the support element and the clamp and each other.

REFERENCES:
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patent: 3864797 (1975-02-01), Banks
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Guide to Operations for the 38-cm Ion Source by Commonwealth Scientific Corp. 6/30/87.
"Low Specific Impulse Electric Thrusters" by Kaufman et al Jul. 1984.
"Design, Fabrication and Operation of Dished Accelerator Grids on a 30 cm Ion Thruster" by Rawlin et al, Apr. 1972.
"Dished Accelerator Gridson a 30 cm Ion thruster" by Rawlin et al Journal of Spacecraft and Rockets vol. 10, No. 1, Jan. 1973, pp. 29-35.
Characteristics of the Le RC/Hughes J-Series 30 cm Engineering Model Thruster by Collet t et al, 14 International Electric Propulsion COnference 10/30-11/1,1979.
Results of the Mission Profile Life Test by Bechtel et al, 16 International Electric Propulsion COnference 11/1982.

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