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 polyether 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.
[1] 周晓杨, 石俊涛, 庞爱民, 等. 含CL-20固体推进剂研究现状[J]. 固体火箭技术, 2017, 40(4):443-447. Zhou Xiaoyang, Shi Juntao, Pang Aimin, et al. Research status of solid propellant containing CL-20[J]. Journal of Solid Rocket Technology, 2017, 40(4):443-447.
[2] 赵孝彬, 李军, 程立国, 等. NEPE推进剂组成与安全特性的相关性研究[C]//第二届固体推进剂安全技术研讨会. 襄樊:航天科技集团42所, 2009:71-75. Zhao Xiaobin, Li Jun, Cheng Liguo, et al. The relation research of composition and safety characteristic for NEPE propellant[C]//The 2nd Solid Propellant Safety Technology Conference. Xiangfan:42 Aerospace Science and Technology Group, 2009:71-75.
[3] 周光巍, 王丽丽. 预先危险分析在空空导弹固体火箭发动机中的应用[J]. 四川兵工学报, 2012, 33(4):30-33. Zhou Guangwei, Wang Lili. The application of preliminary hazard analysis in air-to-air missile solid rocket motor[J]. Journal of Sichuan Ordnance, 2012, 33(4):30-33.
[4] Chassagne F, Bordachar S. Large Solid Rocket Motor safety analyses:Thermal effects issues[C]//34th Department of Defense Explosives Safety Board Seminar. Portland:Oregon, 2010:ADM002313.
[5] Milner G. Trident D-5 missile explosive propellant hazards[R/OL].[2019-01-31]. www.gzcenter.org/D5rockethazards.pdf.
[6] 徐松林, 刘文一. 某型高能固体火箭发动机热烤燃性能研究[J]. 导弹与航天运载技术, 2017(6):27-27. Xu Songlin, Liu Wenyi. Research on the cook-off performance of high energy solid rocket motor[J]. Missiles and Space Vehicles, 2017(6):27-27.
[7] 吴勋, 任宁莉, 冯翔, 等. 固体发动机典型环境载荷分析[J]. 装备环境工程, 2010, 7(6):103-105. Wu Xun, Ren Ningli, Feng Xiang, et al. Analysis of typical environmental load of solid rocket motor[J]. Equipment Environmental Engineering, 2010, 7(6):103-105.
[8] 杨永忠, 陈国宏. 固体导弹靶场安全距离计算研究[J]. 导弹试验技术, 2004(3):19-21. Yang Yongzhong, Chen Guohong. The research of range safety distance calculation for solid missile[J]. Missile Test Technology, 2004(3):19-21.
[9] 胡保朝. 提高固体发动机设计质量和可靠性的措施[J]. 质量与可靠性, 1997(5):41-43. Hu Baochao. The measure to improve the design quality and reliability for solid motor[J]. Quality and Reliability, 1997(5):41-43.
[10] 陈广南, 张为华. 固体火箭发动机撞击与热击安全性分析[M]. 北京:国防工业出版社, 2008. Chen Guangnan, Zhang Weihua. Safety analysis for solid rocket motor under impact and heat[M]. Beijing:National Defence Industry Press, 2008.
[11] 方学谦, 王建灵, 杨建, 等. 固体推进剂安全性评价试验研究[J]. 火工品, 2017(3):49-52. Fang Xueqian, Wang Janling, Yang Jian, et al. The experimental study of hazard assessment on solid propellant[J]. Initiators & Pyrotechnics, 2017(3):49-52.