A one-time micro-nano satellite system with harassment function

CN118833411BActive Publication Date: 2026-08-28HARBIN INST OF TECH +1
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Patent Information

Application Number
CN202411072156.0
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-08-06
Publication Date
2026-08-28
Estimated Expiration
2044-08-06

AI Technical Summary

Technical Problem

化学物质喷射是一种利用腐蚀性或者遮光性等化学性质使用一种干扰、破坏手段,可造成敌方卫星的破坏,或者影响太样帆的受光面积,造成供电不足

Benefits of technology

[0014]因此,本发明采用上述结构的一种具备袭扰功能的一次性微纳卫星系统,能够满足低成本高效打击在轨目标的任务需求,所提出的一次性微纳卫星系统结构紧凑,内部所含元器件种类少,体积小,且安装在卫星内结构紧凑,质量轻。整体的动力来源为尾部运动控制喷嘴和前姿态控制喷嘴,能够实现高效的轨道调整和目标追击;相机模块与微型电磁发射器的组合可以实现高效低能耗的袭扰;整体又可以通过撞击与内部炸药爆破的形式对大型目标进行高效摧毁。满足在轨武器装备对小体积、轻质量、低能耗、高效率作战的在轨任务需求。

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Abstract

The application discloses a one-time micro-nano satellite system with a harassment function, and belongs to the technical field of on-orbit weapon equipment, which comprises a goose egg type satellite shell component and a satellite-borne power module, a satellite-borne computer module, a gas cylinder module, a camera module, a miniature electromagnetic emitter, a front attitude control nozzle and a tail motion control nozzle which are arranged in the goose egg type satellite shell component; a middle-through hole is arranged in the center of the goose egg type satellite shell component; six hole positions are uniformly arranged at the head of the goose egg type satellite shell component; the camera module, the miniature electromagnetic emitter and the front attitude control nozzle are correspondingly arranged at the hole positions, and the gas cylinder module is connected with the front attitude control nozzle and the tail motion control nozzle through gas supply pipelines. The one-time micro-nano satellite system with the harassment function has the advantages that the task demand of low-cost and high-efficiency attack on an on-orbit target can be met, and the on-orbit task demand of small size, light weight, low energy consumption and high efficiency can be met.
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Citation Information

Patent Citations

  • High pressure gas propelling system used for microsatellite

    CN204173166U

  • Space based orbital kinetic energy weapon system

    US20090321579A1