Modeling to Evaluate a Spacecraft Propellant Gauging System
Author:
Affiliation:
1. Lockheed Martin, Palo Alto, California 94304-1191
2. Lockheed Martin Technical Operations, Sunnyvale, California 94089
3. Purdue University, West Lafayette, Indiana 47907-1282
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3642
Reference6 articles.
1. Transient lumped capacity thermodynamic model of satellite propellant tanks in micro-gravity
2. The Surface Evolver
3. A vane type propellant management device
Cited by 22 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. Study of the thermal characteristics of propellant tanks in microgravity and its application to propellant gauging;Journal of Physics D: Applied Physics;2024-07-19
2. Mathematical Modelling of a Propellent Gauging System: A Case Study on PRISMA;Aerospace;2023-06-18
3. Flexible Assemblies of Electrocapacitive Volume Tomographic Sensors for Gauging Fuel of Spacecraft;Journal of Spacecraft and Rockets;2021-03
4. Measuring Techniques;Heat Transfer in Aerospace Applications;2017
5. Hydrazine decomposition on a small platinum cluster: the role of N2H5 intermediate;Theoretical Chemistry Accounts;2016-02-19
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
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3