Operating characteristics of the Russian D-55 thruster with anode layer-Reference-Cited by-同舟云学术

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Operating characteristics of the Russian D-55 thruster with anode layer

Published:1994-06-27 Issue: Volume: Page:
ISSN:
Container-title:30th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Sankovic John¹,Haag Thomas¹,Manzella David²

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. NYMA, Inc., Brook Park, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-3011

Reference24 articles.

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2. Effect of vacuum backpressure on discharge characteristics of hollow cathode;Plasma Science and Technology;2019-10-01

3. Preliminary Design of a Single Stage Bismuth SPT Hall Thruster for Small Spacecraft Applications;AIAA Propulsion and Energy 2019 Forum;2019-08-16

4. Laser Induced Fluorescence Measurements in a Hall Thruster as a Function of Background Pressure;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22

5. History of Electric Propulsion at NASA Glenn Research Center: 1956 to Present;Journal of Aerospace Engineering;2013-04

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