电能分配航天器及相关方法

By combining modular spacecraft with electric thrusters, chemical thrusters, and deformable solar generators, the limitations of existing power distribution technologies have been solved, enabling flexible and efficient multi-point power distribution and reducing costs and launcher requirements.

CN117337259BActive Publication Date: 2026-07-17SAFRAN SPACECRAFT PROPULSION

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
SAFRAN SPACECRAFT PROPULSION
Filing Date
2022-05-11
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In existing technologies, the use of solar generators is limited to a single mission, making it impossible to distribute electrical energy at multiple points in free space, orbit, and celestial bodies. Furthermore, the launch systems are complex and costly, increasing the demand for fuel containers.

Method used

Design a modular spacecraft that combines electric thrusters, chemical thrusters, and variable geometry solar generators to achieve multi-mission power distribution through a modular structure, including flexible combinations of power distribution, relocation, and landing phases.

Benefits of technology

It enables continuous power distribution across multiple points in free space, orbits, and celestial bodies, reducing mission costs, minimizing launcher requirements, and improving the flexibility and efficiency of power distribution.

✦ Generated by Eureka AI based on patent content.

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Abstract

本发明涉及一种用于在位于自由空间、轨道上和 / 或天体上的点处向客户飞行器(2)分配电能的航天器(1),该航天器(1)包括主结构(10),其配备有电推进器(10A)、化学推进器(10B)和太阳能发电机(10C)、用于电推进器(10A)的燃料的第一燃料容器(11)、以及用于化学推进器(10B)的燃料的第二燃料容器(12),该航天器(1)被配置成使得:主结构(10)可以可替代地与第一容器(11)或第二容器(12)联接 / 分离,第一容器(11)和第二容器(12)能够彼此联接 / 分离,太阳能发电机(10C)用于展开或收回。
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