Current position: Home >> Scientific Research >> Patents

一种大推力固体火箭发动机推力测试装置

Hits:

First Author:zhangjun

Disigner of the Invention:jia zhenyuan,李明昱,renzongjin,liuwei

Affilication of Author(s):机械工程学院

Application Number:ZL201710999601.1

Pre One:一种基于双尾支撑和张线支撑的模型支撑装置及方法

Next One:一种电火花微小孔加工控制方法