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综合导弹和整体式冲压发动机的相互影响，从导弹总体设计的观点出发，对整体式液体冲压发动机的性能进行了研究，分析讨论了设计参数对发动机性能的影响及发动机设计的特殊问题。本方法可用于导弹总体方案设计阶段参数的选择和性能分析。
Based on the interaction between the integrated missile and the integrated ramjet engine, the performance of the integral ramjet engine is studied from the viewpoint of missile overall design. The influence of design parameters on engine performance and special problems of engine design are analyzed and discussed. The method can be used for the parameter selection and performance analysis in the design stage of missile overall scheme.