A 10,000 hour life multipropellant engine for Space Station applications

Author:

PUGMIRE T.1,CANN G.1,HECKERT B.2,SOVEY J.3

Affiliation:

1. Technion, Inc., Irvine, CA

2. Rockwell International Corp., Canoga Park, CA

3. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Reference28 articles.

Cited by 7 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. Performance measurements of a water fed microwave electrothermal thruster;37th Joint Propulsion Conference and Exhibit;2001-07-08

2. Electric propulsion for International Space Station reboost - A fresh look;37th Joint Propulsion Conference and Exhibit;2001-07-08

3. Preliminary characterizations of a water vaporizer for resistojet applications;28th Joint Propulsion Conference and Exhibit;1992-07-06

4. The effect of test-cell pressure on resistojet nozzle flow;25th Joint Propulsion Conference;1989-07-12

5. Recent advances in low-thrust propulsion technology;24th Joint Propulsion Conference;1988-07-11

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