A modularized electromagnetic power backpack applied to satellite auxiliary orbit injection comprises a backpack body and an electric propulsion module, the backpack body comprises a first connecting part and a second connecting part, the backpack body is connected with the electric propulsion module through the first connecting part and connected with a satellite platform through the second connecting part, and the satellite platform comprises a third connecting part. The satellite platform and the modularized electromagnetic power backpack applied to satellite auxiliary injection are jointly connected to the carrier through a third connecting part, and after the satellite platform and the modularized electromagnetic power backpack applied to satellite auxiliary injection are carried and launched to a relatively low orbit height by the carrier, the satellite platform and the modularized electromagnetic power backpack applied to satellite auxiliary injection are connected to the carrier through a second connecting part. The satellite platform is separated from the modularized electromagnetic power backpack applied to satellite auxiliary orbit injection from the carrier, and the satellite platform is launched to the orbit height of a preset target orbit of the satellite platform under the electric propulsion effect of the modularized electromagnetic power backpack applied to satellite auxiliary orbit injection.
一种应用于卫星辅助入轨的模块化电磁动力背包包括背包本体以及电推进模块,背包本体包括第一连接部以及第二连接部,背包本体通过第一连接部与电推进模块连接,通过第二连接部与卫星平台连接,卫星平台包括第三连接部,卫星平台与应用于卫星辅助入轨的模块化电磁动力背包通过第三连接部共同连接在运载器上,其中,卫星平台与应用于卫星辅助入轨的模块化电磁动力背包由运载器运载发射至相对较低的轨道高度后,卫星平台与应用于卫星辅助入轨的模块化电磁动力背包自运载器分离,卫星平台在应用于卫星辅助入轨的模块化电磁动力背包的电推进作用下发射至卫星平台的预定目标轨道的轨道高度。
Modularized electromagnetic power backpack applied to satellite auxiliary orbit injection and satellite orbit injection method
一种应用于卫星辅助入轨的模块化电磁动力背包及卫星入轨方法
2023-07-21
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
Near-circular orbit satellite electric propulsion orbit injection method
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|NTIS | 1983
|NTRS | 1973
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