The invention relates to a non-throwing type aircraft separation launching device which comprises a carrier, two separation supports are rotationally installed on the carrier, notches are formed in the separation supports, the two separation supports are locked in a closed state through separation bolts, a cavity is formed between the two separation supports, and the two separation supports are arranged in the cavity. A mounting opening is defined by the two notches, an elastic piece is connected between the separation supports and the carrier, and the elastic piece tends to open the two separation supports; a first aircraft is installed in the installation opening, and a second aircraft is installed in the cavity. The separation bolt explodes for separation, limiting and fixing of the separation support are relieved, the separation support is opened under the elastic force of the elastic piece, the first aircraft in the mounting opening is released, and meanwhile preparation work is made for subsequent separation of the second aircraft; the separation support is connected with the carrier, the rotating function is reserved, the separation support is not thrown away after rotating, and the requirement that space junk is not newly added to affect track safety in spaceflight launching activities is met.
本发明涉及一种非抛离式飞行器分离发射装置,其包括:运载器,所述运载器转动安装有两个分离支架,所述分离支架开设有缺口,两个所述分离支架通过分离螺栓锁止于关闭状态,且两个所述分离支架之间形成腔室,两个所述缺口围成安装口,所述分离支架与所述运载器之间连接有弹性件,所述弹性件趋于打开两个所述分离支架;所述安装口安装飞行器一,所述腔室安装飞行器二。分离螺栓爆炸分离,解除对分离支架的限位固定,在弹性件的弹力下,打开分离支架,释放安装口内的飞行器一,同时也为后续飞行器二的分离做好准备工作;分离支架与运载器相连,保留了转动功能,分离支架转动后不抛离,满足航天发射活动不新增太空垃圾影响轨道安全的要求。
Non-throwing type aircraft separation launching device
一种非抛离式飞行器分离发射装置
2023-08-11
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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