Development of a new fiber-optic multi-target multispectral pyrometer for achievable true temperature measurement of the solid rocket motor plume.

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Title: Development of a new fiber-optic multi-target multispectral pyrometer for achievable true temperature measurement of the solid rocket motor plume.
Authors: Liang, Mei1 mmglm@163.com, Sun, Bojun1, Sun, Xiaogang1 sxg@hit.edu.cn, Xie, Junyan2
Source: Measurement (02632241). Jan2017, Vol. 95, p239-245. 7p.
Subjects: Optical pyrometers, Temperature measuring instruments, Plumes (Fluid dynamics), Rocket engine exhaust, Photodiodes
Abstract: This paper describes the development of a novel multi-target multispectral pyrometer to remotely measure the true temperature of the plume of a solid fuel rocket engine in a harsh environment ground test. Using an optical fiber transmission technique, the core part of the instrument can be located 100 m away from the test site, so the influence of the harsh environment can be reduced and the instrument reliability improved. Optics are separated from prisms to accurately locate targets. Based on preamplifier circuits and parallelly adjacent pixels of the photodiode detectors, the measurement lower limit can reach 900 °C. The pyrometer is validated against experimental data from field measurements of a solid fuel rocket motor plume. The results demonstrate that the true temperature of the solid fuel rocket engine plume can be acceptably measured with the proposed pyrometer. [ABSTRACT FROM AUTHOR]
Copyright of Measurement (02632241) is the property of Elsevier B.V. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
Database: Engineering Source
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DbLabel: Engineering Source
An: 119776443
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  Data: Development of a new fiber-optic multi-target multispectral pyrometer for achievable true temperature measurement of the solid rocket motor plume.
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  Data: <searchLink fieldCode="JN" term="%22Measurement+%2802632241%29%22">Measurement (02632241)</searchLink>. Jan2017, Vol. 95, p239-245. 7p.
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  Data: <searchLink fieldCode="DE" term="%22Optical+pyrometers%22">Optical pyrometers</searchLink><br /><searchLink fieldCode="DE" term="%22Temperature+measuring+instruments%22">Temperature measuring instruments</searchLink><br /><searchLink fieldCode="DE" term="%22Plumes+%28Fluid+dynamics%29%22">Plumes (Fluid dynamics)</searchLink><br /><searchLink fieldCode="DE" term="%22Rocket+engine+exhaust%22">Rocket engine exhaust</searchLink><br /><searchLink fieldCode="DE" term="%22Photodiodes%22">Photodiodes</searchLink>
– Name: Abstract
  Label: Abstract
  Group: Ab
  Data: This paper describes the development of a novel multi-target multispectral pyrometer to remotely measure the true temperature of the plume of a solid fuel rocket engine in a harsh environment ground test. Using an optical fiber transmission technique, the core part of the instrument can be located 100 m away from the test site, so the influence of the harsh environment can be reduced and the instrument reliability improved. Optics are separated from prisms to accurately locate targets. Based on preamplifier circuits and parallelly adjacent pixels of the photodiode detectors, the measurement lower limit can reach 900 °C. The pyrometer is validated against experimental data from field measurements of a solid fuel rocket motor plume. The results demonstrate that the true temperature of the solid fuel rocket engine plume can be acceptably measured with the proposed pyrometer. [ABSTRACT FROM AUTHOR]
– Name: AbstractSuppliedCopyright
  Label:
  Group: Ab
  Data: <i>Copyright of Measurement (02632241) is the property of Elsevier B.V. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)
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RecordInfo BibRecord:
  BibEntity:
    Identifiers:
      – Type: doi
        Value: 10.1016/j.measurement.2016.10.033
    Languages:
      – Code: eng
        Text: English
    PhysicalDescription:
      Pagination:
        PageCount: 7
        StartPage: 239
    Subjects:
      – SubjectFull: Optical pyrometers
        Type: general
      – SubjectFull: Temperature measuring instruments
        Type: general
      – SubjectFull: Plumes (Fluid dynamics)
        Type: general
      – SubjectFull: Rocket engine exhaust
        Type: general
      – SubjectFull: Photodiodes
        Type: general
    Titles:
      – TitleFull: Development of a new fiber-optic multi-target multispectral pyrometer for achievable true temperature measurement of the solid rocket motor plume.
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            NameFull: Liang, Mei
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            NameFull: Sun, Bojun
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            NameFull: Sun, Xiaogang
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            NameFull: Xie, Junyan
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          Dates:
            – D: 01
              M: 01
              Text: Jan2017
              Type: published
              Y: 2017
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              Value: 95
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