The priming process of feed lines of cryogenic propellant liquid rocket engines was studied.
研究了低温推进剂液体火箭发动机供应管道系统充填过程的建模问题。
A zero-gravity thermodynamic vent system which is desirable to be used in a cryogenic propellant tank is briefly presented.
简要介绍一种可供选择使用的低温燃料贮箱零重力排气系统。
The two level distributed control system for cryogenic propellant loading is introduced, taking the Lox loading control system for example.
以液氧加注控制系统为例，介绍液体运载火箭低温推进剂加注控制所采用的两级分布式系统。
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