The invention provides a one-rocket multi-satellite self-series launching structure of a small high-orbit satellite. The structure comprises a plurality of series modules, wherein each series module comprises a force bearing cylinder and a cabin body, and the series modules are directly connected with the first end face of the force bearing cylinder of the next series module through the second endface of the force bearing cylinder of the previous series module to form a multi-satellite self-series combination body; and multiple force bearing cylinders, wherein the column sections of the forcebearing cylinders have the same diameter, the column section of at least one force bearing cylinder protrudes out of the-Z direction of the cabin body, and the column section of at least one force bearing cylinder protrudes out of the + Z direction of the cabin body.
本发明提供了一种小型高轨卫星的一箭多星自串联发射结构,包括:多个串联模块,每个串联模块均包括承力筒和舱体,其中多个所述串联模块通过上一串联模块的承力筒的第二端面与下一串联模块的承力筒的第一端面直接连接,组成多星自串联组合体;以及多个承力筒,其柱段具有相同的直径,至少一个所述承力筒的柱段突出于所述舱体的‑Z向,至少一个所述承力筒的柱段突出于所述舱体的+Z向。
One-rocket multi-satellite self-series launching structure of small high-orbit satellite
小型高轨卫星的一箭多星自串联发射结构
2020-11-06
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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