The invention provides an ejection system of a spacecraft and a method for helping the spacecraft to operate by using the ejection system, and the system consists of a base on the spacecraft flying near a small space celestial body, an ejection driver on the base, a touch device capable of being pushed by the ejection driver, a tether connected with the spacecraft and a tether winding device, the ejection driver comprises a motor and an ejection mechanism or a curved bar or a mechanical arm device driven by the motor through a transmission device, a touch device can be directly pushed or pulled to eject or stretch out, and the touch device can touch or fall to the surface of a nearby small celestial body. The touch device connected with the tether is dragged or collided with the surface of the small celestial body at the rear lower part or the lower part or the front lower part of the spacecraft, and the touch device is subjected to counter-acting force of the surface of the small celestial body towards the rear part or the front upper part or the upper part or the rear upper part, so that the flying mechanical energy or speed or orbit height or flying direction of the spacecraft is changed; and meanwhile, the fuel consumption of the jet engine is avoided or reduced.
本技术提出一种航天器的弹射系统和利用其帮助航天器运行的方法,该系统由位于空间小型天体附近飞行的航天器上的底座、底座上的弹射驱动器、可以由它推动的触碰器、与其及航天器连接的系绳、系绳卷扬装置构成,其中弹射驱动器包括:电动机、由电动机通过传动装置带动的弹射机构或曲杆或机械臂装置,可直接推动或拉动触碰器射出或伸出,触碰器可以触碰或降落到附近小型天体表面,令连接系绳的触碰器在航天器的后下方或下方或前下方与小型天体表面拖曳或碰撞,其会受到小型天体表面朝后方或前上方或上方或后上方的反作用力,以改变航天器飞行的机械能或速度或轨道高度或飞行方向,同时避免或减少对喷气发动机燃料的消耗。
System and method for assisting operation of spacecraft by using small celestial body
利用小型天体帮助航天器运行的系统和方法
2024-10-22
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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