通过微热电偶测温和火焰单幅照相技术测试了含硼富燃料推进剂燃烧波温度分布及燃烧火焰结构；
The combustion wave temperature profiles and flame structures of fuel-rich propellant containing boron are measured by using W-Re micro-thermal couple and flame photo technique.
为了测试推进剂燃料温度分布，采用彩色CCD比色测温技术，设计了一种非接触式膏体推进剂火焰测温系统。
Based on the colorimetric temperature measurement technology of color CCD, a non-contact pasty propellant flame temperature measurement system was designed.
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