Layout cooling channels around cavities evenly.
在型腔周围均衡的配置冷却孔道。
A sample of rocket engine thrust chamber with cooling channels was successfully manufactured by APEF.
成功制造出带冷却通道的火箭发动机推力室身部样件。
The cooling channels are sealed most effectively against the smooth inner jacket by elastic elements.
冷却通道与光滑的内护套之间用弹性元件紧紧地密封起来。
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