The invention discloses a second rocket sublevel capable of releasing satellites and a working method.The second rocket sublevel capable of releasing satellites comprises a second rocket sublevel body with an effective load cabin arranged in the middle; the effective load cabin at least comprises a load cabin body provided with a cabin door opening, a left side cabin door, a right side cabin door, a cabin door driving system, a left side front radiant panel, a right side front radiant panel, an electromechanical actuation system, a left side rear radiant panel, a right side rear radiant panel, a remote control mechanical arm and an automatic locking mechanism. The two split cabin door structures are adopted on the effective load cabin, and the load bearing capacity of the second sub-stage of the rocket is improved.
本申请公开了一种可释放卫星的火箭二子级及工作方法,其中,可释放卫星的火箭二子级,包括:中部设置有有效载荷舱的火箭二子级;其中,有效载荷舱至少包括:开设有舱门口的载荷舱主体、左侧舱门、右侧舱门、舱门驱动系统、左侧前辐射板、右侧前辐射板、机电作动系统、左侧后辐射板、右侧后辐射板、遥控机械臂和自动锁紧机构。本申请在有效载荷舱上采用两扇对开式舱门结构,提高了火箭二子级的载荷承载能力。
Rocket second sublevel capable of releasing satellite and working method
一种可释放卫星的火箭二子级及工作方法
2024-02-23
Patent
Elektronische Ressource
Chinesisch
Europäisches Patentamt | 2024
|Vertical recovery method of liquid injection rocket under sublevel route and related equipment
Europäisches Patentamt | 2023
|Europäisches Patentamt | 2021
|