火箭推进
火箭推進
화전추진
JOURNAL OF ROCKET PROPULSION
2012年
2期
75-78
,共4页
低温热敏电阻温度计%不确定度评定%校准装置
低溫熱敏電阻溫度計%不確定度評定%校準裝置
저온열민전조온도계%불학정도평정%교준장치
cryogenic thermistor thermometers%uncertainty evaluation%calibration system
根据测量不确定度的评定方法,分析和计算低温热敏电阻温度计校准装置的测量不确定度。通过校准结果的不确定度评定,掌握校准装置的计量性能及误差来源,为国防计量标准的建立、实行与考核提供不确定度评定的依据。
根據測量不確定度的評定方法,分析和計算低溫熱敏電阻溫度計校準裝置的測量不確定度。通過校準結果的不確定度評定,掌握校準裝置的計量性能及誤差來源,為國防計量標準的建立、實行與攷覈提供不確定度評定的依據。
근거측량불학정도적평정방법,분석화계산저온열민전조온도계교준장치적측량불학정도。통과교준결과적불학정도평정,장악교준장치적계량성능급오차래원,위국방계량표준적건립、실행여고핵제공불학정도평정적의거。
The measurement uncertainty of a calibration system for cryogenic thermistor thermometers applied to rocket engines is analyzed and computed according to the evaluation method of measurement uncertainty.Through the uncertainty evaluation of calibration results,the performance and error of the calibration system for cryogenic thermistor thermometers applied to rocket engines were mastered,and the gist of uncertainty evaluation was provided for the establishment,effectuation and exmaination of the metrological standard in national defense.