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。
Intercontinental quick arrival transportation system based on rocket power
一种基于火箭动力的洲际快速抵达运输系统
2021-09-03
Patent
Electronic Resource
Chinese
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