Deorbiting of LEO Small Satellites Without A Conventional Propulsion System

被引：0
|
作者：
Ham, Chan [1 ]
Ngo, Diane [1 ]
机构：
[1] Kennesaw State Univ, Mechatron Engn Dept, Kennesaw, GA 30144 USA
来源：
SOUTHEASTCON 2017 | 2017年
关键词：
space debris mitigation; aerodynamic sail; electrodynamic tether; simulations;
D O I：
暂无
中图分类号：
TP301 [理论、方法];
学科分类号：
081202 ;
摘要：
This study introduces an effective propellantless space debris mitigation scheme for Low Earth Orbit (LEO) satellites. Mechanizing an aerodynamic sail and electrodynamic tether system provides LEO small satellites a deorbiting capability that meets the time limit of 25 years required by the U.S. Government and European Space Agency (ESA). Simulation results confirm the effectiveness of the proposed technical approach.
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页数：2
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