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红外高光谱大气探测仪星载固定点黑体辐射源的研制
引用本文:胡朝云,郝小鹏,宋健,文平,常稼强,顾明剑,丁雷.红外高光谱大气探测仪星载固定点黑体辐射源的研制[J].计量学报,2019,40(2):232-239.
作者姓名:胡朝云  郝小鹏  宋健  文平  常稼强  顾明剑  丁雷
作者单位:成都理工大学核技术与自动化工程学院,四川成都610059;中国计量科学研究院,北京100029;中国计量科学研究院,北京,100029;中国计量科学研究院,北京100029;中国科学院上海技术物理研究所,上海200083;中国科学院红外探测与成像技术重点实验室,上海200083;中国科学院上海技术物理研究所,上海200083;中国科学院红外探测与成像技术重点实验室,上海200083
基金项目:国家重点研发计划(2018YFB0504700,2018YFB0504702),国家自然科学基金(11475162)
摘    要:介绍了中国计量科学研究院为风云三号05星红外高光谱大气探测仪研制的微型镓固定点星载黑体辐射源。设计了黑体辐射源空腔,其有效发射率优于0.997。针对星载固定点黑体辐射源的结构设计和性能测试展开了研究:星载固定点黑体辐射源17 ℃的温度均匀性仿真结果优于0.01℃;黑体辐射源在真空下均匀性优于0.02 ℃,稳定性优于0.002 ℃(90 min内);在通过满足航天应用的力学冲击等实验后,镓固定点的复现性优于0.03 ℃;微型固定点相变温坪复现实验加热功率与拐点值之间存在较好的线性关系。

关 键 词:计量学  黑体辐射源  微型镓固定点  发射率  星载温度传感器
收稿时间:2018-11-08

Development of Blackbody Radiation Sources at Fixed Point on Satellite of Infrared Hyperspectral Atmospheric Detector
HU Chao-yun,HAO Xiao-peng,SONG Jian,WEN Ping,CHANG Jia-qiang,GU Ming-jian,DING Lei.Development of Blackbody Radiation Sources at Fixed Point on Satellite of Infrared Hyperspectral Atmospheric Detector[J].Acta Metrologica Sinica,2019,40(2):232-239.
Authors:HU Chao-yun  HAO Xiao-peng  SONG Jian  WEN Ping  CHANG Jia-qiang  GU Ming-jian  DING Lei
Affiliation:1. College of Applied Nuclear Technology and Automation Engineering, Chengdu University of Technology,Chengdu,Sichuan 610059, China
2. National Institute of Metrology, Beijing 100029, China
3. Shanghai Institute of Technical Physics, Chinese Academy of Sciences, Shanghai 200083, China
4. Key Laboratory of Infrared System Detection and Imaging Technology, Chinese Academy of Sciences, Shanghai 20083, China
Abstract:The miniature gallium fixed point onboard blackbody radiation source developed by National Institute of Metrology for the infrared hyperspectral atmospheric detector of Fengyun No.3 05 satellite is introduced. The black body radiation source cavity is designed, and the effective emissivity of the black body radiation source is better than 0.997. The structure design and performance test of blackbody radiation source with fixed point on satellite are studied. Blackbody radiation source uses double heating, one PID control output, one constant power output. Thermal simulation of spaceborne fixed point blackbody radiation source at 17 ℃, the temperature uniformity result is better than 0.01 ℃. The results of uniformity and stability of blackbody radiation source in vacuum are better than 0.02 ℃ and better than 0.002 ℃ (within 90 min), respectively. The reproducibility of the gallium fixed point is better than that of 0.03 ℃ by satisfying the mechanical impact test of aerospace application. There is a good linear relationship between the heating power and the inflection point value in the micro-fixed point phase transition temperature plateau reappearance experiment.
Keywords:metrology  blackbody radiation sources  micro gallium fixed points  emissivity  spaceborne temperature sensor  
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