摘要
采用热分析技术和单幅近距摄影实验,考察了过渡金属氧化物(TMO)对HTPB推进剂凝聚相反应和气相反应的催化作用,讨论了TMO的主要催化部位。
Catalytic effects of transition-metal oxide (TMO) on the reactions inboth condensation and vapor phases of HTPB propellant are observed by means ofthermal analysis technique and close shot experiment and TMO′s catalytic position isdiscussed.
出处
《固体火箭技术》
EI
CAS
CSCD
1992年第1期55-60,共6页
Journal of Solid Rocket Technology
关键词
推进剂
过渡金属
燃速
Hydroxyterminated polybutadiene propellant
Transition-metal compound
Combustion catalyst of propellant
Propellant buring rate
