Implementation Scheme of Orbital Refueling Using Microsate IIite

Li Yuan-dong, Wang Na-na
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Abstract

The orbital refueling in space can prolong the lifetime of spacecraft and reduce the cost of space applications. Therefore, it is an important direction for the development of space technology in the future. In this paper, a scheme using microsatellite to operate orbital refueling for the GEO spacecraft is designed. The process of rendezvous and refueling are emphatically described. In addition, the key technologies of microsatellite propulsion, control, observation are analyzed and prospected. At last, the commercial prospect of this scheme is analyzed.
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微卫星轨道加注实现方案
空间轨道加油可以延长航天器的使用寿命,降低空间应用的成本。因此,它是未来空间技术发展的重要方向。本文设计了一种利用微卫星对地球同步轨道航天器进行轨道加油的方案。重点描述了交会和加油过程。此外,对微卫星推进、控制、观测等关键技术进行了分析和展望。最后,对该方案的商业前景进行了分析。
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Copyright Information Ferrofluid Levitated Micro/Milli-Robots Implementation Scheme of Orbital Refueling Using Microsate IIite Assembly of Cellular Microstructures into Lobule-Like 3D Microtissues Based on Microrobotic Manipulation* Research supported by the Beijing Natural Science Foundation under Grant 4164099and the National Natural Science Foundation of China under grants 61603044and 61520106011. Three Dimensional Microfabrication Using Local Electrophoretic Deposition Assisted with Laser Trapping Controlled by a Spatial Light Modulator
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