Combustion wave temperature distribution of GAP/AN propellant was studied by means of advanced double W Re microthermocouple technique.
利用先进的双钨铼微热电偶技术，研究了GAP／AN 推进剂的燃烧波温度分布。
Combustion wave temperature distribution of GAP/AN propellant was studied by means of advanced double W Re microthermocouple technique.
利用先进的双钨铼微热电偶技术，研究了GAP／AN 推进剂的燃烧波温度分布。
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