同时介绍中国新的长征一号丁（CZ-1D）小型运载火箭的总体方案、主要系统、参数及运载能力。
The system concept, main sub systems, parameters and capacity of China′s new LM-1D(CZ-1D) small launch vehicle are also introduced.
针对控制系统采用侧喷流发动机和栅格舵的新型小型多级固体运载火箭开展六自由度弹道仿真研究。
This article studies the six-degree-of-freedom trajectory simulation of small multiple stage solid launch vehicles with control systems using lateral jet thrusters and grid fins.
针对控制系统采用侧喷流发动机和栅格舵的新型小型多级固体运载火箭开展六自由度弹道仿真研究。
This article studies the six-degree-of-freedom trajectory simulation of small multiple stage solid launch vehicles with control systems using lateral jet thrusters and grid fins.
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