One embodiment of the invention discloses an open type satellite configuration which comprises a satellite body, an expandable solar wing and a solar wing pressing device, and the satellite body is of an open type box body structure; the expandable solar wing is arranged in the satellite body and is fixedly connected with the satellite body through a solar wing driving mechanism; the solar wing pressing device is arranged in the satellite body and penetrates through the expandable solar wing pressing hole, one end of the solar wing pressing device is fixed to the satellite body through screw joint, and the other end of the solar wing pressing device presses and fixes the foldable solar wing in a folded state through a pressing nut. The volume utilization rate of the fairing during satellite launching is effectively improved, useless space in the satellite is reduced, the volume of the rocket fairing is fully utilized, and the launching efficiency of one rocket with multiple satellites is improved.
本发明的一个实施例公开了一种开放式卫星构型,包括:卫星本体、可展开太阳翼和太阳翼压紧装置,其中,所述卫星本体为开口式箱体结构;所述可展开太阳翼设置于所述卫星本体内部,通过太阳翼驱动机构与所述卫星本体连接固定;所述太阳翼压紧装置设置于所述卫星本体内部,穿过所述可展开太阳翼压紧孔,一端与所述卫星本体通过螺接固定,另一端通过压紧螺母将折叠状态的所述可展开太阳翼压紧固定。本发明有效提高了卫星发射时的整流罩容积利用率,减少卫星内部无用空间,充分利用火箭整流罩体积,提高一箭多星的发射效率。
Open type satellite configuration
一种开放式卫星构型
2022-10-25
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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European Patent Office | 2024
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