The embodiment of the invention provides an intercontinental quick arrival transportation system based on rocket power, which is characterized in that the intercontinental quick arrival transportation system adopts a two-stage wing lift type structure and comprises a boosting-stage aircraft and a load-stage aircraft, the booster-level aircraft and the load-level aircraft are powered by liquid rocket engines, and the intercontinental quick arrival transportation system adopts a mode of horizontal takeoff and landing on an airport runway. The boosting-stage aircraft is used for sending the load-stage aircraft to a preset height at a certain speed; the load-level aircraft is loaded with an effective load to carry out intercontinental flight tasks; and the boosting-stage aircraft and the load-stage aircraft independently execute tasks.

    本发明实施例提供了一种基于火箭动力的洲际快速抵达运输系统,其特征在于,所述洲际快速抵达运输系统采用两级带翼升力式构型,分别包括助推级飞行器和载荷级飞行器,其中,所述助推级飞行器和载荷级飞行器均采用液体火箭发动机提供动力,所述洲际快速抵达运输系统采用在机场跑道水平起飞和降落的模式;所述助推级飞行器用于将载荷级飞行器以一定的速度送入预定高度;所述载荷级飞行器装载有效载荷进行洲际飞行任务;所述助推级飞行器和载荷级飞行器独立执行任务。


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    Title :

    Intercontinental quick arrival transportation system based on rocket power


    Additional title:

    一种基于火箭动力的洲际快速抵达运输系统


    Contributors:
    XU DAFU (author) / QU SHUIQUN (author) / LI YUNFEI (author) / LIU LUJIANG (author) / TANG SHENGYONG (author) / GOU YONGJIE (author) / ZENG ZHANKUI (author)

    Publication date :

    2021-09-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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