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本文介绍CK-1M无人机是缩比为1/5的模拟无人机,安装在发射装置的短轨上,采用双发助推器进行发射起飞。以研究和分析双发助推器推力偏差对发射起飞过程中释放的选择、滑轨长度的确定、离轨安全和飞行姿态的影响。 发射起飞试验证明:有关双发助推器发射起飞模拟试验研究和分析方法是正确的,研究与试验结果具有良好的一致性。这些方法和结果均可作为无人机双发助推器发射起飞的设计依据。
This article describes the CK-1M drone is a 1/5 scale simulation drone, mounted on the launch of the short track, using dual launch booster launch. In order to study and analyze the influence of thrust bias of double-booster on the choice of launch, the determination of the length of the sliding rail, the safety of derailment and the flight attitude. Launch takeoff test proves that the research and analysis methods of launching takeoff of double booster are correct and the research and test results have good consistency. These methods and results can be used as a design basis for the launch of the UAV double booster.