Alkali metal propellants for MPD thrusters-Reference-Cited by-同舟云学术

Alkali metal propellants for MPD thrusters

Published:1991-08-17 Issue: Volume: Page:
ISSN:
Container-title:Conference on Advanced SEI Technologies
language:
Short-container-title:

Author:

POLK J.¹,PIVIROTTO T.¹

Affiliation:

1. JPL, Pasadena, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-3572

Reference53 articles.

1. M. Auweter-Kurtz et al. High Power Steady State MPD Thruster. Technical Report IRS-90-P4, Institut fijr Raumfahrtsysteme, Universitat Stuttgart,Stuttgart,Germany,1990.

2. J.E. Polk, A. J. Kelly, and R. G. Jahn. Characterization of Cold Cathode Erosion Processes. In 20th International Electric Propulsion Conference, Garmisch-Partenkirchen,W. Germany, 1988. AIAA-88-075.

3. D.W. Esker, J.C. Kroutil, and R.J. Checkley. Radiation Cooled MPDArc Thruster. Technical Report MDC-H296 (NASA CR-7255'?), McDonne11 Douglas Corporation, St. Louis MO,1969.

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