Separable satellite propulsion system configuration
Separable satellite propulsion system configuration
- Neue Suche nach: WANG MIN
- Neue Suche nach: WANG WEI
- Neue Suche nach: LIU ZHENGSHAN
- Neue Suche nach: HU ZHAO
- Neue Suche nach: PENG ZHEN
- Neue Suche nach: HAN SHAOHUAN
- Neue Suche nach: PI XIAOLI
- Neue Suche nach: WANG MIN
- Neue Suche nach: WANG WEI
- Neue Suche nach: LIU ZHENGSHAN
- Neue Suche nach: HU ZHAO
- Neue Suche nach: PENG ZHEN
- Neue Suche nach: HAN SHAOHUAN
- Neue Suche nach: PI XIAOLI
The invention discloses a separable satellite propulsion system configuration. A propulsion system sends a satellite into a higher orbit and is separable from the satellite after the satellite entersan orbit, so that the problems of 'dead weight' of the satellite, reduction of the in-orbit position guarantee efficiency of the satellite and consumption of precious fuel resources of the satellite are solved. The invention provides the separable satellite propulsion system configuration which can be used for sending a satellite to a specified orbit. The separable satellite propulsion system configuration comprises a force bearing cylinder, a connecting and separating device and a boosting control structure; the force bearing cylinder is used for bearing the satellite; the connecting and separating device is arranged at the top end of the force bearing cylinder for connecting the satellite; and the boosting control structure is connected with the connecting and separating device and is used for propelling the satellite borne by the force bearing cylinder to a specified orbit and separating from the connecting and separating device to separate from the satellite after propelling the satellite to the specified orbit.
本发明公开了一种可分离卫星推进系统构型，该推进系统将卫星送入较高轨道以及卫星入轨后，与卫星可分离，从而解决卫星“呆重”，降低卫星在轨位保效率，耗费卫星宝贵的燃料资源的问题。本发明提供了一种可分离的卫星推进系统构型，该推进系统可用于将卫星送到指定轨道，包括承力筒、连接分离装置和助推控制结构，其中，承力筒用于承载卫星；连接分离装置设置在承力筒顶端，用于连接卫星；助推控制结构，与连接分离装置连接，用于将承力筒所承载的卫星推进到指定轨道，在将卫星推进到指定轨道后，与连接分离装置分离，脱离卫星。
Dokumentinformationen
Separable satellite propulsion system configuration
一种可分离卫星推进系统构型
2021-02-19
Patent
Elektronische Ressource
Chinesisch
| IPC: | B64G Raumfahrt , COSMONAUTICS |
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