固液火箭发动机 meaning in Chinese
solid-grain rocket engine
Examples
- The low frequency burning oscillation of the 85 % h202 - pe hybrid rocket motor is discussed
研究了85 hzoz ? pe固液火箭发动机的低频振荡燃烧现象。 - The combustion model of hybrid rocket propellant was established . the combustion flow in the hno3 + n2o4 - htpb hybrid rocket motor has been researched
研究了直径为706mm多孔分段装药全尺寸试验固液火箭发动机内部的燃烧与流动问题。 - Owing to the dissimilar combustion mode , their working process is different form that of solid rocket motors and the liquid rocket engines
由于氧化剂和燃料的燃烧方式不同,固液火箭发动机工作过程与液体及固体火箭发动机有很大的区别。 - Owing to the dissimilar combustion mode , their working process is different form that of solid rocket motors and the liquid rocket engines
由于氧化剂和燃料的燃烧方式不同，固液火箭发动机工作过程和液体火箭发动机及固体火箭发动机有很大的区别。 - Through the tests of the 85 % h2o2 - pe hybrid rocket motor , the operation process of the hybrid motor has been studied in the dissertation . the main aspects are as follows : 1
本文结合85 h _ 2o _ 2 ? pe固液火箭发动机试验，从以下几个方面比较系统地研究了固液火箭发动机的工作过程： 1