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Application of Aerospike to Hypersonic Vehicle: The Scientific Flight Test of China's First Commercial Rocket

机译:Aerospike Aerospike在超音速车辆中的应用:中国第一个商用火箭的科学飞行试验

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The first commercial rocket OS-XO was launched in May 17, 2018. The main goal of the OS-X series rockets is to provide a low-cost and high-efficiency platform for the performance testing of hypersonic vehicle to gather fundamental scientific data which is difficult or impossible to obtain via ground testing alone. A solid rocket engine named XGF-01 was independently designed, and successfully tested in December 22, 2017. The payload is composed of a universal hypersonic vehicle head with an aerospike. The purpose is to investigate the performance of passive flow-control of the aerospike in hypersonic flow. The geometric shape of the aerospike determines the size of the low pressure recirculation zone of the head. As the drag reduction effect of aerospike in the supersonic flow has been verified in flight tests abroad, the aerospike could achieve maximum drag reduction of 35% for the head in hypersonic flow. The scientific research of OS-XO focuses on heat flux reduction and sonic-boom mitigation. The flight test results show that the aerospike could achieve a maximum reduction of 42% for the heat flux of head in hypersonic flow, which will greatly improve the flight performance of hypersonic vehicle because of a good thermal environment. When the rocket flies in the near space with a hypersonic speed, the sonic boom intensity is between 136-120 decibels. During the burning stage, the sonic boom characteristics of the supersonic vehicle can be predicted by the numerical simulations of two states which include engine power on and power off, covering the sonic boom value of the flight test. The flight test results can be helpful to support the engineering application of hypersonic vehicles in the future, breaking through the key technologies, improving commercialization and developing core technology for long-range high-speed aircraft.
机译:第一个商业火箭OS-XO于2018年5月17日推出。OS-X系列火箭的主要目标是为高超声音车辆进行性能测试提供低成本和高效的平台,以收集基本的科学数据难以单独地通过地面测试获得困难或不可能获得。一个名为XGF-01的固体火箭发动机独立设计,并于2017年12月22日成功进行了测试。有效载荷由具有Aerospike的通用超音车车头组成。目的是探讨超声波流量的无源流量控制的性能。 Aerospike的几何形状决定了头部的低压再循环区的尺寸。由于在国内航空公司飞行试验中验证了Aerospike的减阻效果,Aerospike可以在超声波流动中实现35%的最大阻力减少35%。 OS-XO的科学研究侧重于热通量减少和Sonic-Boom缓解。飞行试验结果表明,由于热环境良好,空气运输司适用于高超声速流动的热通量最大减少42%,这将大大提高超音速车辆的飞行性能。当火箭在具有超声速度的近空间中飞行时,声波臂强度在136-120分贝之间。在燃烧阶段,可以通过两个状态的数值模拟来预测超音速车辆的声波臂特性,包括发动机电源接通和断电,覆盖飞行试验的声波臂值。飞行试验结果可以有助于支持未来超音速车辆的工程应用,突破关键技术,改善远程高速飞机的商业化和开发核心技术。

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