The invention provides a hidden type child-mother satellite structure and a child-satellite separation control method, the child-mother satellite structure comprises a mother satellite and a child-satellite assembly (200), the mother satellite comprises a platform cabin (100) and a load cabin (300), the upper part of the platform cabin (100) is connected with the load cabin (300), and the child-satellite assembly (200) is arranged in the load cabin (300); the load cabin (300) has a closed state and an unclosed state, and when the load cabin top plate (302) is in an unfolded state, the sub-star assembly (200) arranged in the load cabin (300) can be exposed; the child satellite assembly (200) comprises a child satellite (201) and a separation mechanism (202), and the child satellite (201) is arranged in the load cabin (300) through the separation mechanism (202). According to the invention, a good temperature environment and an anti-radiation environment can be provided for the child satellite (201) before separation, and the child satellite (201) is hidden in the load cabin (300) before separation, so that the actual use of the child satellite (201) is not easy to observe and discover.
本发明提供了一种隐蔽式子母星结构和子星分离控制方法,其中子母星结构包括:母星和子星组件(200),其中,母星包括平台舱(100)和载荷舱(300),平台舱(100)上方连接载荷舱(300),载荷舱(300)内设置有子星组件(200);载荷舱(300)具有封闭和不封闭两种状态,当载荷舱顶板(302)处于展开状态时能够露出置于载荷舱(300)内的子星组件(200);子星组件(200)包括子星(201)和分离机构(202),子星(201)通过分离机构(202)设置在载荷舱(300)内。本发明能够为子星(201)分离前提供良好的温度环境及抗辐照环境,且子星(201)分离前隐藏在载荷舱(300)内,其实际用途不容易被观测和发现。
Hidden type child-mother satellite structure and child-satellite separation control method
隐蔽式子母星结构和子星分离控制方法
2023-05-05
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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