| 卫星推进系统气体流量探头的研制 |
| Development of Gas Flow Probe on Satellite Propulsion System |
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| 中文摘要: |
| 介绍了卫星推进系统气体流量探头设计中的几个问题，该探头适用微波量气体流量的测量，采用了差压式孔板流量计的原理，设计轻巧，使用方便，能够进行远距离无失真传输，方便了现场测试。 |
| 英文摘要: |
| This paper discusses some problems in the design of the gas flow probe on the satellite propulsion system.This probe suits the measurement of micro gas flow,which conforms with the theory of the differential\|pressure orifice flow meter,and it is designed light and handy and used conveniently.This probe can export current be transferred distorionlessly with long distance and this brings great convenience for measurement on the spot. |
| 李玉涛 吕俊芳 |
| 北京航空航天大学自动控制系,北京市,100083 |
| 中文关键词: 气体流量 孔板流量计 探头 调理电路 卫星推进系统 |
| 英文关键词:Gas flow,Orifice meter,Probe,Condition circuit,Propulsion system |
| 基金项目: |
| DOI： |
| 引用本文：李玉涛,吕俊芳.卫星推进系统气体流量探头的研制[J].计测技术,2000,(3):5~7,14. |
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