... 火箭炮构件 multibarrel rocket gun component; 火箭喷管 rocket nozzle; 火箭喷管盖 rocket nozzle closure; ...
基于6个网页-相关网页
self-cooled rocket nozzle 自冷式火箭发动机喷管
rocket nozzle closure 火箭喷管盖
Solid rocket nozzle 固体火箭喷管
electroformed rocket nozzle 电成型火箭发动机喷管
Solid rocket nozzle flow 固体火箭发动机燃气流动
entry of a rocket nozzle 火箭喷管进气部分
multi nozzle rocket 多喷管火箭发动机
double nozzle rocket 双喷管火箭发动机
The plume temperature of the rocket nozzle should be taken into consideration in the vector control of various missile weapons.
在各种导弹武器的矢量控制技术中需要考虑火箭喷管羽焰的温度。
参考来源 - 喷管羽流温度场测量系统的研制·2,447,543篇论文数据，部分数据来源于NoteExpress
A new method of the solid propellant rocket nozzle design is presented.
本文介绍一种设计固体火箭喷管的新方法。
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。
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