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1)  hypersonic boost-flight experiment
高超声速助推飞行试验
1.
Overall plan for hypersonic boost-flight experiment technology is investigated in detail for the free-flight test of hypersonic vehicle under nominal design conditions.
以高超声速飞行器为有效载荷,进行了高超声速助推飞行试验技术方案研究,并通过分析气动力参数、设计变量参数的范围及约束条件,进行了助推弹道设计,确定了二级助推发动机设计要求,并利用调整发射俯仰角、滑行时间和配重物质量来调整助推弹道参数,将高超声速飞行器送入试验弹道。
2)  hypersonic flight test
高超声速飞行试验
1.
Based on some actual high altitude range in hypersonic flight test,the characters of wind such as mean wind,gust,turbulence and random wind are analyzed,and then the mathematic models of ground wind,low/middle-altitude and high-altitude have been established.
从高超声速飞行试验的飞行高度范围出发,对平均风、阵风/突风、大气紊流及随机风场进行了分析与研究。
3)  boost-glide vehicle
高超声速助推-滑翔飞行器
1.
Based on rocket-boost launching mode,the analytical expressions between takeoff mass and range as well as propellant specific impulse and payload were deduced for three kinds of hypersonic vehicles,including ballistic vehicles,boost-glide vehicles and boost-cruise vehicles.
基于火箭助推的发射方式,推导出弹道式飞行器、高超声速助推-滑翔飞行器及高超声速助推-巡航飞行器的起飞质量与航程、燃料比冲和载荷之间的解析关系,为总体设计初期快速估算飞行器起飞质量提供了方法。
4)  boost-cruise vehicle
高超声速助推-巡航飞行器
1.
Based on rocket-boost launching mode,the analytical expressions between takeoff mass and range as well as propellant specific impulse and payload were deduced for three kinds of hypersonic vehicles,including ballistic vehicles,boost-glide vehicles and boost-cruise vehicles.
基于火箭助推的发射方式,推导出弹道式飞行器、高超声速助推-滑翔飞行器及高超声速助推-巡航飞行器的起飞质量与航程、燃料比冲和载荷之间的解析关系,为总体设计初期快速估算飞行器起飞质量提供了方法。
5)  hypersonic test vehicle
高超音速试验飞行器
6)  supersonic/hypersonic flight
超声速/高超声速飞行
补充资料:高超
好得超过一般水平:见解~丨技术~。
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