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Hyper-X Flight Engine Ground Testing for X-43 Flight Risk Reduction

机译:用于降低X-43飞行风险的Hyper-X飞行引擎地面测试

摘要

Airframe-integrated scramjet engine testing has been completed at Mach 7 flight conditions in the NASA Langley 8-Foot High Temperature Tunnel as part of the NASA Hyper-X program. This test provided engine performance and operability data, as well as design and database verification, for the Mach 7 flight tests of the Hyper-X research vehicle (X-43), which will provide the first-ever airframe-integrated scramjet data in flight. The Hyper-X Flight Engine, a duplicate Mach 7 X-43 scramjet engine, was mounted on an airframe structure that duplicated the entire three-dimensional propulsion flowpath from the vehicle leading edge to the vehicle trailing edge. This model was also tested to verify and validate the complete flight-like engine system. This paper describes the subsystems that were subjected to flight-like conditions and presents supporting data. The results from this test help to reduce risk for the Mach 7 flights of the X-43.
机译:作为NASA Hyper-X计划的一部分,已经在NASA Langley 8英尺高温隧道的7马赫飞行条件下完成了与飞机一体的超燃冲压发动机的测试。该测试为Hyper-X研究飞行器(X-43)的Mach 7飞行测试提供了发动机性能和可操作性数据,以及设计和数据库验证,这将提供有史以来首架在飞机上集成的超燃冲压发动机数据。 Hyper-X飞行引擎是Mach 7 X-43超​​燃冲压发动机的复制品,安装在机身结构上,该结构复制了从车辆前缘到车辆后缘的整个三维推进流路。还对该模型进行了测试,以验证和验证完整的类似飞行的发动机系统。本文描述了遭受类似飞行条件的子系统并提供了支持数据。该测试的结果有助于降低X-43的7马赫飞行风险。

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