Current status of electric propulsion technology-Reference-Cited by-同舟云学术

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Current status of electric propulsion technology

Published:1969-08-16 Issue: Volume: Page:
ISSN:
Container-title:6th Annual Meeting and Technical Display
language:
Short-container-title:

Author:

LAZAR J.¹

Affiliation:

1. NASA, OFFICE OF ADVANCED RESEARCH AND TECHNOLOGY, WASHINGTON, D.C.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1969-1107

Reference29 articles.

1. Jackson, F. A. , etal; "An Operational Electrothermal PropulsionSystem for Spacecraft Reaction Control, 'AIAA Paper 66-213, March 1966.

2. Hunter, R. E. , etal; "Cesium Contact Ion Microthruster Ekperiment Aboard Applications Technology Satellite (ATSbN, '' AIAA Paper 69-297, March 1969.

3. Guman, W.J. , and Nathanson, D.M,"Pulsed Plasma Microthruster Propulsion System for Synchronous Orbit Satellite, AIAA Papr 69-298, March 1969.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Characteristics, capabilities, and costs of solar electric spacecraft for planetary missions;Journal of Spacecraft and Rockets;1970-12

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