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Increased capabilities of the 30-cm diameter Hg ion thruster

Authors :
C. E. Hawkins
V. K. Rawlin
Source :
Conference on Advanced Technology for Future Space Systems.
Publication Year :
1979
Publisher :
American Institute of Aeronautics and Astronautics, 1979.

Abstract

A 30-cm-diam mercury ion thruster, using two or three grid ion accelerating systems, is operated at increased values of beam current. Comparisons with the SEP (Solar Electric Propulsion) and EPSEP (Extended Performance SEP) baseline thrusters are made with respect to performance and lifetime. It is found that when a third, or decelerator, grid is added to the conventional two-grid optics of a SEP-like thruster, the ion beam focusing properties are improved, as expected from theoretical considerations. The total thruster efficiency as a function of specific impulse, is increased for values of specific impulse in the range 1200-2800 sec. Lifetime test results predict a thruster lifetime, under space conditions, not less than that of the baseline SEP thruster.

Details

Database :
OpenAIRE
Journal :
Conference on Advanced Technology for Future Space Systems
Accession number :
edsair.doi...........e6d53c836f241544637e06ca9910aa2c
Full Text :
https://doi.org/10.2514/6.1979-910