介绍了卫星推进系统气体流量探头设计中的几个问题。
This paper discusses some problems in the design of the gas flow probe on the satellite propulsion system.
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。
A kind of multi channel micro gas flowmeter used for satellite propulsion system is introduced.
根据弹塑性有限变形理论，用有限元法建立了卫星推进系统贮箱金属膜片变形的有限元分析模型。
According to the deformation of elastic-plastic theory, the finite element analysis model of metal diaphragm for tank of propulsion system in satellite was established in this paper.
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