Space debris removal system using a small satellite

被引:143
|
作者
Nishida, Shin-Ichiro [1 ]
Kawamoto, Satomi [1 ]
Okawa, Yasushi [1 ]
Terui, Fuyuto [1 ]
Kitamura, Shoji [1 ]
机构
[1] Japan Aerosp Explorat Agcy, Inst Aerosp Technol, Tokyo, Japan
关键词
Space debris;
D O I
10.1016/j.actaastro.2009.01.041
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Since the number of satellites in Earth orbit is steadily increasing, space debris will eventually pose a serious problem to near-Earth space activities if left unchecked, and so effective measures to mitigate it are becoming urgent. Equipping new satellites with an end-of-life de-orbit or orbital lifetime reduction capability could be an effective means of reducing the amount of debris by reducing the probability of the collisions between objects. On the other hand, the active removal of space debris and the retrieval of failed satellites by spacecraft are other possible measures. The Institute of Aerospace Technology, Japan Aerospace Exploration Agency (JAXA), is studying a micro-satellite system for active space debris removal, and is examining the applicability of electro-dynamic tether (EDT) technology as its high efficiency orbital transfer system. A small EDT package provides a possible means for lowering the orbits of objects without the need for propellant. Capture is indispensable for the retrieval of large space debris objects, and we propose a flexible robot arm for this purpose. This paper discusses a space debris removal satellite system and describes the development status of prototypes of the EDT package and a new robot arm for capturing non-cooperative targets. (c) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码:95 / 102
页数:8
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