Micro Newton Colloid Thruster System Development for ST7-DRS Mission-Reference-Cited by-同舟云学术

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Micro Newton Colloid Thruster System Development for ST7-DRS Mission

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

Author:

Gamero-Castano Manuel¹,Hruby Vlad¹,Spence Douglas²,Demmons Nathaniel²,McCormick Ryan²,Gasdaska Charles²

Affiliation:

1. Busek Co Inc

2. Busek Co. Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4543

Reference13 articles.

1. Advanced High-Thrust Colloid Sources

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. Effects of the Wall Temperature on Rarefied Gas Flows and Heat Transfer in a Micro-Nozzle;Micromachines;2023-12-22

2. Direct Simulation Monte Carlo Simulation of the Effect of Needle Valve Structures on the Rarefied Flow of Cold Gas Thrusters;Micromachines;2023-08-11

3. Capillary ionic liquid electrospray: beam compositional analysis by orthogonal time-of-flight mass spectrometry;Journal of Fluid Mechanics;2021-10-05

4. Transient Behavior of Ion Extraction and Acceleration of Variable Thrust Ion Thruster;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2018

5. Effect of Aspect Ratio on the Wettability and Electrospray Properties of Porous Tungsten Emitters with the Ionic Liquid [Emim][Im];46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25

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