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研究了空气涡轮冲压发动机的高推力小型化结构要素 ,明确了各要素的性能。对该发动机进行了地面静止试验。确认了作为推进系统设计的可行性。介绍了试验用发动机概况、试验方法与试验结果
The components of high thrust miniaturization of air turbine ramjet engine are studied, and the performance of each element is clarified. The engine was ground static test. Confirmed as a propulsion system design feasibility. Introduced the test engine overview, test methods and test results