conventional propellant loading system 常规加注系统
propellant loading control system 推进剂装填控制系统
Propellant Loading and Transfer System 燃料装填与运输系统
According to the general design of the cryogenic propellant loading system, a centrifugal pump is used for loading liquid oxygen to launch vehicle.
根据低温加注系统总体设计，采用离心泵加注液氧。
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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