The design and operating characteristics of a 30-kW thermal arcjet engine for space propulsion-Reference-Cited by-同舟云学术

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The design and operating characteristics of a 30-kW thermal arcjet engine for space propulsion

Published:1986-06-16 Issue: Volume: Page:
ISSN:
Container-title:22nd Joint Propulsion Conference
language:
Short-container-title:

Author:

PIVIROTTO T.¹,KING D.¹,DEININGER W.¹,BROPHY J.¹

Affiliation:

1. California Institute of Technology, Jet Propulsion Laboratory, Pasadena

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1508

Reference3 articles.

1. Thirt Kilowatt Plasmajet Rocnet-Enqine &cezno-vear Development Proqraml - Summary Report, preparea for National AeronaufiyS a n d c e Administration by Research and Advanced Oevelooment Division. Avco Corporation, Wilmington, Massachusetts; NASA CR-54044, RAD-TR-64-6, 15 July 1964.

Cited by 11 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. Near and far-field plume studies of a 1 kW arcjet;30th Joint Propulsion Conference and Exhibit;1994-06-27

2. Extended life and performance test of a low-power arcjet;Journal of Spacecraft and Rockets;1992-07

3. Effect of nozzle and cathode configuration on arcjet performance;Journal of Propulsion and Power;1990-05

4. Electric propulsion for constellation deployment and spacecraft maneuvering;Journal of Spacecraft and Rockets;1989-09

5. Development of a hybrid (MPD plus thermal) arcjet engine with an applied magnetic field;25th Joint Propulsion Conference;1989-07-12

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