摘要
推进剂燃烧;;火焰传播;;
The combustion characteristics of double-base and composite prope-llant grains with interior cracks were studied experimentally at atmospheric temperature and various pressures. It is shown that the flame propagation speed is increased with the reduce of the crack depth and as the depth of crack decreases, the maximum pressure coursed by combustion in cracks is increased. It is also discovered that when the flame spreads to the end of a crack, a combustion zone is formed immediately near the crack tip accompanied with a obvious pressure protrusion.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1990年第2期29-34,共6页
Journal of Propulsion Technology
关键词
固体推进剂
燃烧
火焰传播
火箭发动机
Propellant combustion, Flame propagation, Solid rocket engine
