Background Flow Model Validation with a Six-Kilowatt Hall Effect Thruster-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Background Flow Model Validation with a Six-Kilowatt Hall Effect Thruster

Published:2020-03 Issue:2 Volume:36 Page:308-311
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Frieman Jason D.¹,Liu Thomas M.¹,Walker Mitchell L. R.¹

Affiliation:

1. Georgia Institute of Technology, Atlanta, Georgia 30332

Funder

Achievement Rewards for College Scientists Foundation

National Science Foundation

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.B37512

Reference12 articles.

1. Electrical Facility Effects on Hall Thruster Cathode Coupling: Performance and Plume Properties

2. Performance Characteristics of a Cluster of 5-kW Laboratory Hall Thrusters

3. Background Flow Model of Hall Thruster Neutral Ingestion

4. Free molecular background flow in a vacuum chamber equipped with two-sided pumps

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370

www.globalauthorid.com

TOP