The embodiment of the invention discloses a pulley block type rocket projectile launching method and device, and the method comprises the steps of rope traction, distribution of a movable pulley block, preparation of a power-assisted source, data simulation, data substitution, arrangement of a device consisting of a launcher, a rope, the movable pulley block and a heavy object, accelerating of a carrier rocket to move through the dead weight of the heavy object, removing of the rope on the carrier rocket after the carrier rocket reaches the initial speed value, and ignition and launching. The carrier rocket is pre-accelerated to a certain initial speed through a traction mode before ignition of the rocket, so rocket fuel is saved, and then the effective load of the rocket is improved.

    本发明实施例公开了一种滑轮组式火箭弹射发射方法及装置,包括绳索牵引、分配动滑轮组、配备助力源、数据模拟、数据代入等,并设置由发射架、绳索、动滑轮组以及重物等构成的装置,通过重物的自重使运载火箭加速运动,并在运载火箭达到初速度值后,解除运载火箭上的绳索,并点火发射。本发明将运载火箭通过牵引的方式,在火箭点火前预加速至一定的初速度,以实现节约火箭燃料进而提升火箭的有效载荷。


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    Title :

    Pulley block type rocket projectile launching method and device


    Additional title:

    一种滑轮组式火箭弹射发射方法及装置


    Contributors:
    CAO RUI (author)

    Publication date :

    2021-06-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F41F APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS , Vorrichtungen zum Abschießen von Geschossen oder Flugkörpern aus Rohren, z.B. Geschütze





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