摘要: The surface-to-air engagement scenario is analyzed to illustrate the operation of an IR missile. The function of a guided missile is defined and the basic aerodynamic characteristics of a missile are discussed. The implications of... 展开
作者 | Allan, R. I. | ||
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原报告号 | N8810822 | 总页数 | 104 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Electronic countermeasures Infrared detectors Surface to air missiles Aerodynamic characteristics Homing Infrared signatures Missile control |