摘要
用“高低压声发射燃速测试系统”研究测定了特低燃速丁羟推进剂(r=2mm/s~4mm/s)在2MPa低压下的燃速和2MPa~14MPa范围内的燃速压强指数。结果表明,特低燃速的测试精度可达1%,某HTPB-AP-Al-T29-HMX推进剂的燃速测试临界压强为2MPa。
The measurement accuracy of burning rate at 2MPa low pressure and the burning rate pressure exponent at the range of 2MPa^14MPa for lower burning rate HTPB propellant(r=2mm/s^4mm/s)are studied using a burning rate measurement system at high and low pressure by means of acoustic emissionThe obtained results show that the measurement accuracy of lower burning rate can be within 1% and the critical pressure of burning rate measurement for HTPBAPAlT29HMX propellant is 2MPa
出处
《推进技术》
EI
CAS
CSCD
北大核心
1998年第3期94-97,共4页
Journal of Propulsion Technology
关键词
复合
固体推进剂
推进剂燃速
燃速测试
声发射
Composite solid propellant Propellant burning rate,Burning rate testing,Acoustic emission