高能推进系统试验操作风险及处置措施  

Risk analysis and disposal measures for high energy propelled system test

作　　者：尹怀志 徐松林[1] 王军延[1] YIN Huaizhi;XU Songlin;WANG Junyan(91550 Unit of People's Liberation Army of China, Dalian 116023, China)

机构地区：[1]中国人民解放军91550部队

出　　处：《科技导报》2019年第13期104-108,共5页Science & Technology Review

摘　　要：高能推进系统的高能量特性使得飞行器射程更远,但同时也增大了推进系统及其飞行器的操作使用风险。通过综述目前被国内外导弹、火箭广泛使用的硝酸酯增塑聚醚推进剂及其高能推进系统特性,梳理了近年来与推进系统相关的安全事故及原因,基于某型高能推进系统火箭在试验场的试验操作内容,采用使用和保障危险分析方法对其试验过程进行了风险分析,并提出了改进措施建议。The high energy characteristic of high energy propelled system makes the fighting efficiency of missile weapons stronger but also more dangerous to use and sustain. The nitrate ester poly-ether propellant and propelled systems of missiles and rockets using NEPE are generalized. Safety accidents of missiles and rockets in recent years are reviewed briefly. Technique preparation of certain rocket with high energy propelled system is introduced. Hazard source identification on technical preparation of high energy propelled vehicle is studied by PHA method, and the disposal measures are suggested a. The research can provide a technical support for the test of high energy propelled vehicle test in test range.

关 键 词：高能推进系统 技术准备 风险分析 处置措施 

分 类 号：TJ7[兵器科学与技术—武器系统与运用工程] V43[航空宇航科学与技术—航空宇航推进理论与工程]