摘要
研究了防老剂H对IPDI丁羟推进剂(中燃速和高燃速的HTPB/AP/Al推进剂,HTPB/AP/HMX/Al推进剂)低温力学性能的影响,在常温强度相同的条件下,随着防老剂H的加入和用量的增加,IPDI推进剂的低温强度升高和低温伸长率显著降低,这种现象是由于防老剂的加入和用量的增加使粘合剂相中硬段微区型物理交联贡献增大,导致推进剂的拉伸脱湿造成的。
The effect of antioxidant H(N,N′ diphenyl p phenylene diamine)on low temperature mechanical performance of IPDI type HTPB propellants(including HTPB/AP/Al propellant with moderate and high burning rate and HTPB/AP/HMX/Al propellant)has been investigated.Keeping constant tensile strenth at room temperature,with the increase of antioxidant H the tensile strenth σ m is increased and the elongation ε m is decreased at low temerature for IPDI propellants.The phenomenon is attributed to tensile dewetting of the propellants,which is resulted from the increase of hard segment domain type physical crosslinks in binder matrix with the adding and increasing of antioxidant H in the propellants
出处
《推进技术》
EI
CAS
CSCD
北大核心
1998年第1期82-85,共4页
Journal of Propulsion Technology
关键词
端羟基聚丁二烯
推进剂
低温伸长率
防老剂
Hydroxyl terminated polybutadiene propellant,Solid rocket propellant binder,Propellant antioxidant,Performance of low temperature mechanics