The invention provides a rocket recovery method. The rocket recovery method comprises the steps that a rocket recovery device is provided, wherein the rocket recovery device comprises a fixing seat, asupporting structure and a hanging frame structure, one end of the supporting structure is fixedly arranged on the fixing seat, and the other end of the supporting structure is used for being connected with the hanging frame structure; the posture and the speed of a rocket to be recovered are adjusted through a posture adjusting system and a reverse thrust system, so that the rocket to be recovered is moved to a preset height above the rocket recovery device; a padlock mechanism of the rocket to be recovered is opened, so that the rocket to be recovered is hung to the hanging frame structure;and the hanging frame mechanism is matched with the padlock mechanism to move in the descending direction of the rocket to be recovered, the acting force of the rocket to be recovered in the landingprocess is buffered, the rocket to be recovered is fixed, and rocket recovery is realized. According to the rocket recovery method, the recovery can be facilitated under the condition that an originalrecovery track and a power system are not changed, the stability during landing is improved, the requirements for the posture and the speed of rocket recovery can be reduced, and the success rate ofrocket recovery is improved.
本发明提供一种火箭回收方法,包括提供火箭回收装置,其中所述火箭回收装置包括固定座、支撑结构及挂架结构,所述支撑结构的一端固设在所述固定座,另一端用于连接所述挂架结构;通过调姿系统及反推系统调整待回收火箭的姿态和速度,使待回收火箭移动到所述火箭回收装置的上方预设高度处;打开待回收火箭的挂锁机构,使其挂接至所述挂架结构;所述挂架机构沿所述待回收火箭的下降方向配合所述挂锁机构运动,缓冲待回收火箭在降落过程的作用力,并固定待回收火箭,实现火箭回收。本发明可以在原有回收轨道、动力系统不变情况下,方便回收,提高着陆时的稳定性,可以降低对火箭回收的姿态和速度要求,提高火箭回收的成功率。
Rocket recovery method
一种火箭回收方法
2020-08-11
Patent
Electronic Resource
Chinese
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