Approximately 60 liters of water are then forced through a rocket nozzle under the seat.
然后大约60公升的水就会被压入座椅下方的火箭喷嘴。
The flow field and thermal environment of gap in solid rocket nozzle were simulated by finite element method.
用有限元素法数值模拟了固体火箭发动机喷管内缝隙的流场和热环境。
The calibration equipment is used to calibrate the visual testing system for rocket nozzle 3D motion, and supplies the standard position and motion parameters for static and dynamic calibration.
本校准装置是用来校准用于测试火箭喷管三维运动的视觉系统，为其提供标准的静态和动态运动参数。
The calibration equipment is used to calibrate the visual testing system for rocket nozzle 3D motion, and supplies the standard position and motion parameters for static and dynamic calibration.
本校准装置是用来校准用于测试火箭喷管三维运动的视觉系统，为其提供标准的静态和动态运动参数。
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