The constrain-analyzed results and the mission-analyzed results of some maneuverable missiles indicate that the model of maneuverable missile and turbofan integrated constrain analysis and mission analysis is feasible and available.

• 对飞航导弹的约束分析计算结果和任务分析计算结果表明，建立的飞航导弹/涡扇发动机一体化约束分析与任务分析模型是合理可行的，具有很好的工程实用价值。