The invention discloses a satellite launching aviation aircraft and relates to the technical field of spaceflight. The aviation aircraft comprises an aircraft body; the upper end of the cabin communicates with a launching cabin; the launching cabin comprises cabin plates folded on the front side and the rear side, and a launching opening is formed between the cabin plates. An openable cabin door is arranged at the upper end of the launching opening; a supporting platform capable of being obliquely lifted is mounted in the launching cabin; telescopic clamping blocks are arranged on the front side and the rear side of the supporting platform in the launching cabin; a carrier rocket is arranged at the upper end of the supporting platform; a vertical baffle is arranged at the tail end, located on one side of the tail of the carrier rocket, of the upper end of the supporting platform, and boosting equipment is arranged between the baffle and the heat insulation box. A cavity is formed in one end, close to the tail of the carrier rocket, of the supporting platform; a hollow cylinder is mounted in the cavity; a piston is slidably arranged in the hollow cylinder; cooling liquid is arranged inside the piston in the hollow cylinder, and the outer side of the piston is connected with a piston rod; the piston rod is fixedly connected with the heat insulation box; an elastic guide pipe is connected between the empty cylinder and the cooling pipe. The invention can solve the problem of high fuel loss caused by high resistance in satellite launching in the prior art.

    一种卫星发射航空飞机,涉及航天技术领域;包括机体,机舱上端连通设置发射舱,发射舱包括前后侧折叠设置的舱板,舱板之间设有发射口,发射口上端设有可开合的舱门,发射舱内安装有可倾斜抬起的支撑平台,发射舱内部位于支撑平台前后侧设有可伸缩的夹持块,支撑平台上端设有运载火箭,支撑平台上端位于运载火箭尾部一侧的末端设有竖直的挡板,挡板与隔热箱之间设置助推设备,支撑平台靠近运载火箭尾部一端的内部设为空腔,空腔内安装有空筒,空筒内滑动设置活塞,空筒内位于活塞内侧设有冷却液,活塞外侧连接活塞杆,活塞杆与隔热箱之间固定连接,空筒与冷却管之间连接弹性导管。解决现有技术中卫星发射存在阻力大导致燃料损耗大的问题。


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    Title :

    Satellite launching aviation aircraft


    Additional title:

    一种卫星发射航空飞机


    Contributors:
    KANG GUOJUN (author)

    Publication date :

    2021-12-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS




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