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surface to air missile

机译:地空导弹

摘要

the utility model relates to missile technology, in particular to зенитным controlled missiles.;air defense missile, in the form of конусообразного corps, included in обтекателем, starting the motor installation, маршевой motor installation, the transitional section.production management and control, and the part edge and primed management different, fairing and transition bay met with a heat-resistant электропроводящего mat rial.on the surface of the conductive layer and the layer which is caused by the emission of electrons from materials with low work output of electrons with education through source and электроэнергand a closed circuit with a маршевой propulsion installed high-speed ramjet.;the technical result is to increase the efficiency of high-speed objectives by ensuring the maintenance of missiles with high speeds while maintaining its целостн guests in athanks to the high speed aerodynamic heating by installing a маршевого engine впврд and the electronic cooling in термоэлектронной emissions pst екателя zur.1 il.
机译:本实用新型涉及导弹技术,尤其涉及二等控制导弹。防空导弹,包括在三等兵中,形式为конусообразногоcorps,启动电动机安装,маршевой电动机安装,过渡部分,生产管理和控制,以及零件边缘和底漆处理的不同,整流罩和过渡槽在导电层和导电层的表面上遇到了耐热的электропроводящего材料,该材料是由电子的低功输出的材料发出的电子所致。通过信号源和электроэнерг以及带有маршевой推进装置的闭路驱动装置安装了高速冲压喷气机。技术结果是通过确保高速维护导弹,同时又要保证其целостн来宾保持高速飞行,从而提高了高速目标的效率。通过安装маршевого发动机вппврд和термоэле的电子冷却来加速空气动力学加热ктронной排放量pstекателяzur.1 il。

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