Electrospray Plume Modeling for Rapid Life and Performance Analysis-Reference-Cited by-同舟云学术

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Electrospray Plume Modeling for Rapid Life and Performance Analysis

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
language:
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Author:

Parmar Shehan M.¹,Collins Adam L.¹,Wirz Richard E.¹

Affiliation:

1. University of California Los Angeles

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1357

Reference38 articles.

1. ST7-DRS Colloid Thruster System Development and Performance Summary

2. The LISA Pathfinder Mission

3. Electrospray Thruster Propellant Feedsystem for a Gravity Wave Observatory Mission

Cited by 2 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. High angle mass flux of an electrospray plume;Journal of Electric Propulsion;2022-12-19

2. Molecular Dynamics Simulations of Ion Extraction from Nanodroplets for Ionic Liquid Electrospray Thrusters;Journal of Electric Propulsion;2022-09-26

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