摘要
通过分析进行多目标攻击对导弹"同时"发射的要求,考虑多枚红外导弹连续发射的影响因素,建立了红外寻的制导空-空导弹红外辐射模型,并以此计算了导弹发动机喷管的红外辐射、尾喷焰辐射、蒙皮辐射和反射的环境辐射,将结果与目标飞机红外辐射进行对比,研究使用红外导弹进行多目标攻击的可行性问题,并给出了分析结果。
In order to investigate into the service feasibility of infrared missile for single-to-multiple attack, the infrared radiation model of air-to-air missile is established; and the three aspects, i.e. jet nozzle radiation, feather flow radiation and airflow heating radiation of the solid rocket motor are calculated. Finally the calculated results are compared with the numerical value of target infrared radiation to lead to the analysis conclusion.
出处
《飞机设计》
2010年第1期72-76,共5页
Aircraft Design
关键词
空-空导弹
发动机
红外辐射
多目标攻击
air-to-air missile
engine
infrared radiation
multi-target attack
