固体火箭发动机排气羽流对微波衰减的计算方法
Calculation method of microwave attenuation by exhaust plume of solid rocket motors
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摘要: 研究了弱电离的羽流等离子体对平面正弦微波的衰减机理,应用羽流等离子体电磁场标准Maxwell方程,结合颗粒相产物充放电的Shukla方程,给出有效用于微波衰减的预估方法;编制了(Radio fre-quency attenuation calculation,简称RFAC)羽流场微波衰减计算软件;分析了羽流场各特性参数对复电导率及微波衰减常数的影响规律,并结合ThermoCalc推进剂热力学评估系统计算了两种不同推进剂配方下,喷管出口羽流场对微波制导信号的衰减,计算结果与文献中的实验结果符合较好.Abstract: The attenuation mechanism of microwave was investigated according to the standard Maxwell equations of exhaust plume plasma.With a reference to the Shukla charging equation of particle components,the prediction method of microwave attenuation by weakly ionized exhaust plume plasma was presented.Radio frequency attenuation calculation(RFAC) software was designed and used to calculate the rules of complex conductivity and microwave attenuation constant that are influenced by some special exhaust plume field parameters.The RFAC and ThermoCalc propellant thermo evaluation system was used comprehensively to calculate the microwave attenuation by nozzle exhaust plume field that comes from two different kinds of propellant.The calculation consequences are in well agreement with the experimental results in citation.
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Key words:
- microwave attenuation /
- exhaust plume /
- solid rocket motor /
- conductivity /
- attenuation constant
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