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助推器喷口火焰温度测量
引用本文:周来福.助推器喷口火焰温度测量[J].宇航计测技术,1993,12(2):48-51.
作者姓名:周来福
作者单位:航空航天部701所 高级工程师
摘    要:火焰温度测量是一个复杂而困难的问题。接触式测温传感器在很多情况下并不适用。固体燃料助推器火焰中有大量固体粒子,这些固体粒子运动速度又很高,采用接触式测温传感器测量这种火焰温度问题较多。介绍用四支小型不调焦光电高温计从不同角度测量固体燃料助推器喷口火焰温度的试验装置和试验结果,并对小型不调焦光电高温计的基本原理、结构、性能作了简单介绍。

关 键 词:火箭推进剂  喷气火焰  温度  测量  Solid  rocket  propellant  Booster  recket  Jet  flame  Temperature  measurement  Photoelectric  pyrometer

Flame temperature measurement in booster jet
Zhou Laifu.Flame temperature measurement in booster jet[J].Journal of Astronautic Metrology and Measurement,1993,12(2):48-51.
Authors:Zhou Laifu
Abstract:Flame temperature measurement is a complicated and difficult problem. Contacted temperature transducers are not applicable in many cases. In solid fuel booster flame, there are a great deal solid particles which are at very high velocity. Therefore, the measurement of flame temperature by contacted temperature transducers will face many problems. This paper will introduce testing derice and testing results of solid fuel booster jet flame temperature measurement by means of four small type nonfocused photoelectric pyrometer, which are arranged at diffirent angles. The basic principle, structure and property of the small type nonfocused photoelectric pyrometer will also be introduced.
Keywords:Solid rocket propellant  Booster recket  Jet flame  Temperature measurement  Photoelectric pyrometer  
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