By using the method of aircraft and turbofan engine integrated analysis, a model of maneuverable missile and turbofan engine integrated constrain analysis and mission analysis was developed and the computative examples and the analysis were given.

• 摘要利用飞机/涡扇发动机一体化设计的思路，建立了飞航导弹/涡扇发动机一体化设计的约束分析和任务分析模型并给出了算例和分析。