Turbopump is an important part in liquid rocket engine.

涡轮泵是液体火箭发动机的重要组成部份。

The engine-feed system interface is at the turbopump inlet flanges.

发动机与供应系统的交界是在涡轮泵的进口法兰盘处。

The engine-feed system interface is at the turbopump inlet flanges .

发动机与供应系统的交界是在涡轮泵的进口法兰盘处。

This has brought a lot of difficulties for the design of the turbopump.

这给涡轮泵的设计带来了很大的困难。

The drive for the turbopump units was actuated using hydrogen peroxide.

涡轮泵由过氧化氢分解产生的气体驱动。