Increased capabilities of the 30-cm diameter Hg ion thruster

Author:

RAWLIN V.1,HAWKINS C.1

Affiliation:

1. NASA, Lewis Research Center, Cleveland, Ohio

Publisher

American Institute of Aeronautics and Astronautics

Reference21 articles.

1. Stearns, J. W. "Large-Payload Earth-Orbit Transportationwith Electric Propulsion, "Jet Propulsion Laboratory, Pasadens, Calif., TM33-793, Sep. 1976. (NASA CR-148973)

2. AIAA Paper 76-1006, Nov. 1976.

Cited by 6 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. Advanced ion propulsion for space exploration;Conference on Advanced SEI Technologies;1991-08-17

2. Ion propulsion system design and throttling strategies for planetarymissions;24th Joint Propulsion Conference;1988-07-11

3. Ion accelerator systems for high-power 30-cm thruster operation;Journal of Spacecraft and Rockets;1985-01

4. Augmenting the Space Shuttle with a space station and tug;Journal of Spacecraft and Rockets;1984-11

5. Improved ion containment using a ring-cusp ion thruster;Journal of Spacecraft and Rockets;1984-09

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