Thermal Effects on Inverted Pendulum Thrust Stands for Steady-state High-power Plasma Thrusters-Reference-Cited by-同舟云学术

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Thermal Effects on Inverted Pendulum Thrust Stands for Steady-state High-power Plasma Thrusters

Published:2003-06-26 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Kodys Andrea¹,Cassady Leonard¹,Choueiri Edgar¹

Affiliation:

1. Princeton University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4842

Reference4 articles.

1. Thrust stand for high‐power electric propulsion devices

2. A. Litvak, J. Lee, and E. Choueiri. Li-LFA Thrust Stand: Design, Fabrication and Calibration in open heat pipe lithium lorentz force accelerator: Final technical report for Thermacore’s Phase II SBIR. Technical Report EPPDyL-TRTC99, EPPDyL-Princeton University, Princeton, NJ, June 1999.

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. Development of a Metronome Thrust Stand for Miniature Electric Propulsion;2018 Joint Propulsion Conference;2018-07-08

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