On-Line Combustion Temperature Measurements of Solid Rocket Propellant by Using Radiation Spectroscopy

Bin Yang, Hao Ran Guo, Xin Yang Gui, Xin Liu, Zhi Xin Wang, Xiao Long Chen, Pei Jin Liu

Research output: Contribution to journalArticlepeer-review

9 Scopus citations

Abstract

For the high combustion temperature measurement in harsh environment, the radiation spectroscopy method was proposed to realize the online measurement of combustion temperature of solid rocket propellant. The radiation spectrums in the range of 200~1 100 nm of solid rocket propellant flame in high pressure experimental combustor were obtained by fiber-optic spectrometer. Their representative characteristics were summarized, and the corresponding combustion temperature was determined by the Planck radiation law and the spectral fitting method. The paper provides important reference for combustion diagnostics and mechanism of solid rocket propellant.

Translated title of the contribution利用辐射光谱法在线测量固体火箭推进剂燃烧温度
Original languageEnglish
Pages (from-to)1958-1962
Number of pages5
JournalGuang Pu Xue Yu Guang Pu Fen Xi/Spectroscopy and Spectral Analysis
Volume38
Issue number6
DOIs
StatePublished - 1 Jun 2018

Keywords

  • Combustion diagnostics
  • Radiation spectroscopy
  • Solid rocket propellant
  • Thermometry

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