A kind of multi channel micro gas flowmeter used for satellitepropulsionsystem is introduced.
介绍了一种多通道气体微流量测试仪,用于卫星推进系统气体流量测量。
2
This paper discusses some problems in the design of the gas flow probe on the satellitepropulsionsystem.
介绍了卫星推进系统气体流量探头设计中的几个问题。
3
According to the deformation of elastic-plastic theory, the finite element analysis model of metal diaphragm for tank of propulsionsystem in satellite was established in this paper.