Plume Study of a 1.35-kW SPT-100 Using an ExB Probe-Reference-Cited by-同舟云学术

Plume Study of a 1.35-kW SPT-100 Using an ExB Probe

Published:2002-11 Issue:6 Volume:39 Page:904-909
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Kim Sang-Wook¹,Gallimore Alec D.¹

Affiliation:

1. University of Michigan, Ann Arbor, Michigan 48109-2118

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/2.3897

Reference20 articles.

1. Measurement of double charged ions in the beam of a 30-cm mercury bombardment thruster

2. Hutchinson, I., Principles of Plasma Diagnostics, 1st ed.Cambridge Univ. Press, New York, 1987, pp.79-84.

3. King, L. B. “Transport-Property and Mass Spectral Measurements in the Plasma Exhaust Plume of a Hall-Effect Space Propulsion System,” Ph.D. Dissertation, Dept. of Aerospace Engineering,Univ. of Michigan, Ann Arbor, MI,Aug. 1998.

4. Improved ion containment using a ring-cusp ion thruster

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