无传统推进系统的低轨道小卫星脱轨

SoutheastCon 2017 Pub Date : 2017-03-01 DOI:10.1109/SECON.2017.7925386

C. Ham, Diane Ngo

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引用次数: 2

摘要

介绍了一种有效的低地球轨道卫星无推进剂空间碎片缓减方案。机械化气动帆和电动力系索系统为低轨道小卫星提供了脱离轨道的能力，满足了美国政府和欧洲航天局(ESA)要求的25年的时间限制。仿真结果验证了所提技术方法的有效性。

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Deorbiting of LEO small satellites without a conventional propulsion system

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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来源期刊

SoutheastCon 2017

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