Development of a new fiber-optic multi-target multispectral pyrometer for achievable true temperature measurement of the solid rocket motor plume.
Saved in:
| 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 |
| FullText | Text: Availability: 0 |
|---|---|
| Header | DbId: egs DbLabel: Engineering Source An: 119776443 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
| IllustrationInfo | |
| Items | – Name: Title Label: Title Group: Ti Data: Development of a new fiber-optic multi-target multispectral pyrometer for achievable true temperature measurement of the solid rocket motor plume. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Liang%2C+Mei%22">Liang, Mei</searchLink><relatesTo>1</relatesTo><i> mmglm@163.com</i><br /><searchLink fieldCode="AR" term="%22Sun%2C+Bojun%22">Sun, Bojun</searchLink><relatesTo>1</relatesTo><br /><searchLink fieldCode="AR" term="%22Sun%2C+Xiaogang%22">Sun, Xiaogang</searchLink><relatesTo>1</relatesTo><i> sxg@hit.edu.cn</i><br /><searchLink fieldCode="AR" term="%22Xie%2C+Junyan%22">Xie, Junyan</searchLink><relatesTo>2</relatesTo> – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22Measurement+%2802632241%29%22">Measurement (02632241)</searchLink>. Jan2017, Vol. 95, p239-245. 7p. – Name: Subject Label: Subjects Group: Su 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.) |
| PLink | https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=egs&AN=119776443 |
| 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. Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Liang, Mei – PersonEntity: Name: NameFull: Sun, Bojun – PersonEntity: Name: NameFull: Sun, Xiaogang – PersonEntity: Name: NameFull: Xie, Junyan IsPartOfRelationships: – BibEntity: Dates: – D: 01 M: 01 Text: Jan2017 Type: published Y: 2017 Identifiers: – Type: issn-print Value: 02632241 Numbering: – Type: volume Value: 95 Titles: – TitleFull: Measurement (02632241) Type: main |
| ResultId | 1 |