Nuclear powered spaceborne laser for orbital debris removal

A. Avdeev, A. Boreysho, S. Ivakin, B. Katorgin, Artem Metelnikov
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引用次数: 1

Abstract

Mid-term opportunities to launch a high-power spaceborne laser are highly restricted due to technical, economic and political issues of it`s design, satellite deployment and system performance. The key technologies, providing the midterm development of a preproduction prototype of a spaceborne laser for small scale debris removal from the low-Earth orbits, are analyzed. A novel approach of nuclear power supplying of the spaceborne laser is presented. It is claimed that nuclear power supplying and electric jet engine technologies implemented in a spacecraft with an onboard laser would provide not only all the energetic requirements, but also orbital maneuvering strong capabilities. The latter would ensure more consistent follow-on rendezvous conditions with space objects, and hence, more efficient low orbital debris removal scenarios.
轨道碎片清除核动力星载激光器
由于其设计、卫星部署和系统性能的技术、经济和政治问题,发射高功率星载激光器的中期机会受到高度限制。分析了用于近地轨道小型碎片清除的星载激光器预生产样机的中期开发的关键技术。提出了一种新的星载激光器核动力供电方法。据称,在具有机载激光的航天器上实施核动力供应和电动喷气发动机技术,不仅可以提供所有的能量需求,而且还可以提供强大的轨道机动能力。后者将确保与空间物体更一致的后续交会条件,从而更有效地清除低轨道碎片。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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