A satellite apparatus, a satellite assembly, and a method of deploying a satellite from a launch vehicle are disclosed, the satellite apparatus including a housing having a first wall and a second wall opposite each other, and a support structure spanning the first wall and the second wall within the housing. The support structure is structurally connected to the housing only at the first wall and the second wall, and an end portion of the support structure is configured to be connected to the launch vehicle by a disconnect system.
公开了一种卫星设备、卫星组件及从发射载具部署卫星的方法,卫星设备包括壳体和支撑结构,该壳体具有彼此相对的第一壁和第二壁,该支撑结构在壳体内横跨第一壁和第二壁。支撑结构仅在第一壁和第二壁处结构性地连接到壳体,并且支撑结构的端部部分配置成通过分离系统连接到发射载具。
Satellite equipment, satellite assembly and method for deploying satellites from launch vehicle
卫星设备、卫星组件及从发射载具部署卫星的方法
2022-06-21
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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