The invention discloses a propulsion system for a small high-orbit satellite public platform. The system comprises a plurality of thrusters arranged in the outer side of a satellite bottom plate cabin, and the thrusters comprise +Y and -Y direction electric thrusters respectively arranged in the outer side of the satellite bottom plate cabin and +X and -X direction chemical thrusters arranged in the outer side of the satellite bottom plate cabin.
本发明公开一种用于小型高轨卫星公用平台的推进系统,包括布置于卫星底板舱外侧的若干个推力器,其中,所述推力器包括分别设置于卫星底板舱外侧的+Y及‑Y向的电推力器以及设置于卫星底板舱外侧的+X及‑X向化学推力器。
Propulsion system for small high-orbit satellite public platform
一种用于小型高轨卫星公用平台的推进系统
2021-08-27
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
Main framework of small high-orbit satellite public platform
European Patent Office | 2020
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