The invention discloses a constellation satellite configuration, which is of a flat plate type cavity structure formed by N material plates with different specifications and sizes, and the ratio of the longest enveloping side length to the height of the bottom surface of the constellation satellite is not less than 3. No less than half weight or number of satellite single machines is arranged in the cavity. In addition, an upper lug structure and a lower lug structure, which are used for inter-satellite connection or satellite-rocket connection, are further arranged.
本发明公开一种星座卫星的构型,为N块不同规格尺寸的材料板形成的平板式腔体结构,且其底面最长的包络边长与的高度比不小于3。其腔体内布局安装有不少于一半重量或数目的卫星单机。此外,其还具有用于星间连接或星箭连接的上下凸耳结构。
Constellation satellite configuration
一种星座卫星的构型
2020-09-18
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
SATELLITE CONSTELLATION SYSTEM AND SATELLITE CONSTELLATION
European Patent Office | 2022
|European Patent Office | 2022
|European Patent Office | 2020
|European Patent Office | 2020
|European Patent Office | 2020
|