The ignition and combustion characteristics of pasty propellant are important parameters for the motor design.
膏体推进剂的点火和燃烧特性是发动机设计的重要参数。
The pasty propellant flame temperature measurement is very important to the propellant formula development and rocket motor design.
膏体推进剂火焰温度测量对推进剂配方的研制及火箭发动机的设计具有重要意义。
Based on the colorimetric temperature measurement technology of color CCD, a non-contact pasty propellant flame temperature measurement system was designed.
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。
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