The invention discloses a satellite support and a carrier rocket. The satellite support comprises a mounting base plate, a fastening supporting assembly and an elastic separation assembly; the fastening supporting assembly comprises an explosion fastening piece and a first mounting connecting frame, the explosion fastening piece is sequentially connected with the first mounting connecting frame, the mounting base plate and a satellite, and the first mounting connecting frame is connected to a cabin body; the elastic separation assembly comprises an elastic piece and a second mounting connecting frame, the second mounting connecting frame is connected with the cabin body and the mounting base plate, and the elastic piece is fixedly arranged in the second mounting connecting frame and elastically abuts against the satellite; and the first mounting connecting frame and the second mounting connecting frame are arranged on the same side of the mounting base plate. By means of the mounting base plate, the fastening supporting assembly and the elastic separating assembly, the size of the satellite support is far smaller than that of a conical barrel adopted in the prior art, the weight of the satellite support is reduced so that the carrying capacity can be improved, and the occupied space of the satellite support is reduced so that waste of the space can be avoided.
本发明公开一种卫星支架和运载火箭,其中卫星支架包括:安装基板;紧固支撑组件,其包括爆炸紧固件和第一安装连接架,所述爆炸紧固件依次连接所述第一安装连接架、所述安装基板和所述卫星,所述第一安装连接架连接于舱体;弹性分离组件,其包括弹性件和第二安装连接架,所述第二安装连接件连接所述舱体和所述安装基板,所述弹性件固设于所述第二安装连接架内且弹性抵接于所述卫星;其中所述第一安装连接架和所述第二安装连接架同侧设置于所述安装基板上。通过设置安装基板、紧固支撑组件和弹性分离组件,其的体积远小于现有技术中采用的锥形筒的体积,减轻了卫星支架的重量以提高运载能力,以及减小了卫星支架的占用空间以避免空间的浪费。
Satellite support and carrier rocket
一种卫星支架和运载火箭
2021-07-09
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Satellite support, satellite support assembly and carrier rocket
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