Hits:
First Author:tanshujun
Disigner of the Invention:范军朋,Wu ZhiGang,杨云飞,于子文
Authorization Date:2014-05-13
Authorization number:2014SR089957
Pre One:运载火箭先进姿态控制系统设计软件
Next One:液体火箭推进-结构-控制动力学耦合分析软件[简称: LRPSC]1.0