Space rope net capturing system based on recombining rope system formation flying
A technology of rope formation and rope net, which is applied in the direction of aircraft, space navigation equipment, space flight vehicles, etc., can solve the problems of poor maneuverability, short capture distance, high launch requirements, etc., to achieve improved reliability, long operation distance, good fault tolerance
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2017-02-15
Smart Images

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Abstract
Description
technical field
[0001] The invention relates to a space rope net capture system, in particular to a space rope net capture system based on recombinable rope formation flight. Background technique
[0002] In order to meet the needs of non-cooperative target acquisition tasks such as malfunctioning spacecraft and space debris in the future, the concept of flexible acquisition has gradually entered people's field of vision, and has become one of the research hotspots in recent years. The concept of flexible capture is a new capture method proposed in recent years. It covers and wraps the target with flexible structures such as nets or cloth, and forms a reliable connection with the mission spacecraft through flexible connectors (such as ropes). The traditional rope net capture system is mostly based on the structure of "task platform + connecting tether + rope net + passive mass block". The traction mass block is launched through the task platform and then pulled to expand t...
Examples
Embodiment Construction
[0024] The present invention will be further described below in conjunction with drawings and embodiments.
[0025] like figure 1 , image 3 As shown, the space rope net capture system of the present invention includes a reconfigurable mechanism 1, a flexible plane rope net 2 and a closing rope 3. The reorganizable mechanism 1 is composed of four sub-mechanisms a, b, c, and d with the same structure, each Each sub-mechanism includes an ejection-docking part and a tether control part.
[0026] like figure 2 As shown, the ejection-docking part includes: a cone 1.1, four springs 1.2, four guide rails 1.3, a cone rod 1.4 and a shell 1.5; in the shell 1.5, the large end of the cone 1.1 is installed on the left side of the shell 1.5 On the outside of the plate, four guide rails 1.3 are vertically evenly distributed on the side of the middle plate of the housing 1.5, and each spring 1.2 is set on the guide rail rod of each guide rail 1.3, and the end of the guide rail rod is conn...