The solid rocket ramjet , which combines the techniques of ramjet propulsion and solid rocket propulsion , offers the following advantages for missile propulsion : high specific impulse , simple configuration , high credibility , convenient using and high maneuverability 固体火箭冲压发动机结合了冲压技术和固体火箭技术,具有比冲高、结构紧凑、工作可靠、使用方便、机动性好等优点,是新一代超声速战术导弹的优选动力装置。
According to the definition and expression of the thrust , as well as the condition derived from them , a method of solid rocket ramjet thrust determination and its program are provided on the basis of engine ground simulation test 本文以西北工业大学固体火箭冲压发动机直连式试车台为研究对象，探讨固体火箭冲压发动机地面试验技术。首先，从推力的定义出发，建立了试验中来流空气流量、燃料流量与固体火箭冲压发动机推力之关系。
Design of two propulsion systems is studied - solid rocket ramjet and liquid ramjet . the performance analysis models and design methods are set up for these two kinds of engines . the different characteristics are analyzed and compared , which provide basis for farther trajectory computation and conceptual optimization design ( 4 )研究了两种动力装置? ?固体火箭冲压发动机和液体燃料冲压发动机的设计问题，建立了两种发动机的性能分析模型和计算方法，对固体火箭冲压发动机和液体燃料冲压发动机的特性进行计算分析及比较，为弹道计算及总体优化设计提供依据。
