火箭推进2012，Vol.38Issue(5)：65-69,5.
提高低温压力测量准确度的方法初探
Discussion on method of improving accuracy of pressure measurement in low temperature
王军钢 1赵万明 1唐丽萍1
作者信息
- 1. 西安航天动力试验技术研究所,陕西西安710100
- 折叠
摘要
Abstract
Pressure is one of the key parameters in the ground test of rocket engines and must be measured accurately. The principle of low-temperature pressure parameter measurement, calibration method and problems existing in the LOX/kerosene rocket engine test are introduced in this paper.The zero drift and slope change of pressure sensors in low temperature are discussed and researched emphatically in the paper. Solutions of the problems and data modification methods are proposed on the basis of problem analysis. This has laid the foundation for improving accuracy of pressure measurement in low temperature.关键词
发动机试验/零位漂移/数据修正Key words
rocket engine test/zero drift/data modification分类
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王军钢,赵万明,唐丽萍..提高低温压力测量准确度的方法初探[J].火箭推进,2012,38(5):65-69,5.
