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Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0

机译:基于加热和火箭铰链力矩的实验研究,模拟导弹的马赫数范围为0.8至2.0

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Jet-stream interaction effects on rocket engine studied with simulated ballistic missile using liquid oxygen and JP-4 fuel mixture

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