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.
针对卫星推进系统管路中经常使用的球面密封结构，分析了其密封的机理，讨论了塑性变形对金属密封的重要作用。
The orbicular seal joint was widely used in the propulsion system of satellites. Its sealing mechanism was studied, and the important effect of the plasticity for metal seal was discussed.
在把MUOS卫星变轨到最终位置以及执行任务寿命期内的在轨机动性重新配置上，该推进系统是很关键的。
The propulsion subsystem is essential for maneuvering the MUOS satellite during transfer orbit to its final location as well as conducting on-orbit repositioning maneuvers throughout its mission life.
“你们可能不会在这些非常小的卫星上面使用任何其他的已经存在任何的电力推进系统，”Khayms说到Lozano的设计。
"You probably couldn't use any other existing electric propulsion [systems] on these very small satellites," Khayms said of Lozano's design.
但是这些系统都要求许多推进剂或推进燃料，并且没有缩小到立方体卫星合适的大小。
But the systems require a lot of propellant, or fuel, and haven't been miniaturized to the scale appropriate for a CubeSat.
他并不熟悉另一项为立方体卫星设计的电力推进系统。
He is not aware of another electric propulsion system designed for CubeSats.
这个推进器设计规定了推进器系统的总体积不超过立方体卫星的10%。
The thruster design requires that the total volume of the propulsion system be less than 10 percent of the CubeSat.
将微波等离子推力器(MPT)应用于“东方红三号”(DFH3)卫星的推进子系统，完成其轨道转移和南北位置保持任务。
Microwave plasma thruster (MPT) was applied to the sub system of DFH 3 satellite to complete its orbit transfer (OT) and north south station keeping (NSSK).
将微波等离子推力器(MPT)应用于“东方红三号”(DFH3)卫星的推进子系统，完成其轨道转移和南北位置保持任务。
Microwave plasma thruster (MPT) was applied to the sub system of DFH 3 satellite to complete its orbit transfer (OT) and north south station keeping (NSSK).
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