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Design and research russian program of experimental hydrogen fueled dual mode scramjet: choice of conception and results of pre-flight tests

机译:设计和研究俄罗斯实验性氢燃料双模超燃冲压发动机程序:概念选择和飞行前测试结果

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The experience of model dual mode Scramjet (DMSCRAM) creation and the main results of ground and pre-flight tests are analyzed in this paper beginning from the conception choice, goals and working program implemented for about 15 years, preceding to the first flight test of hypersonic flight laboratory. Design schemes for plane and axisymetrical engine concept are examined.
机译:本文从模型选择,目标和实施的工作方案(从大约15年开始实施)开始,对双模Scramjet(DMSCRAM)的创建经验以及地面和飞行前测试的主要结果进行了分析,然后进行了首次飞行测试。高超音速飞行实验室。审查了平面和轴对称发动机概念的设计方案。

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