涡轮泵是液体火箭发动机的重要组成部份。
得出了液体动静压滑动轴承可用于液体火箭发动机涡轮泵转子支撑的结论，同时提出了待解决的关键技术。
Comes to the conclusion that the hybrid bearing can be used to the liquid rocket engine turbopump, and then puts forward the key technique to be solved.
转子动力学问题是液体火箭发动机氢涡轮泵研制中最复杂的问题之一。
The problem of the rotor dynamics is one of the most complex problems in research of LOX/LH 2 engine LH 2 turbopump.
转子动力学问题是液体火箭发动机氢涡轮泵研制中最复杂的问题之一。
The problem of the rotor dynamics is one of the most complex problems in research of LOX/LH 2 engine LH 2 turbopump.
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