摘要
从理论上阐述了某新型靶场氢排放燃烧系统设计思想,并对相关设计参数进行了分析计算,形成了比较完整可行的氢排放燃烧系统设计方案,对某新型靶场低温加注系统建设具有参考意义。
The system design idea of liquid hydrogen emission combust in a new launch range was discussed in theory, the correlative desigfi parameters were analyzed and calculated, a complete feasible schematic of liquid hydrogen emission combust system formed which could have reference significance to the construction of cryogenic fueling systems in the new launch range.
出处
《低温工程》
CAS
CSCD
北大核心
2010年第6期41-45,共5页
Cryogenics
关键词
液氢排放
氢气排放
固体火焰模型
安全燃烧
liquid hydrogen emission
hydrogen exhaust
solid flame model
safe combustion
