摘要
介绍了ＡＰ／ＨＭＸＨＴＰＢ推进剂能量特性。理论计算表明，ＨＭＸ取代部分ＡＰ可增加比冲，降低火焰温度和燃气中ＨＣＩ含量，ＨＭＸ代替２０％ＡＰ，比冲增加２５．４６Ｎ·Ｓ·ｋｇ－１。用ＢＳＦ１６５ｍｍ发动机所做的对比试验进一步验证了ＨＭＸ代替ＡＰ对比冲的贡献。
The energy performance of AP/HMX/HTPB composite propellant is discussed. Theorertical calculation shows that pactially replacing AP with HMX can make a increment of specific impulse of the propellant, for example, the increment of specific impulse is 25. 46 N·S·kg-1 when 20% of AP is replaced by HMX. It also results in flame temperature drop and HCl content decreasing in exhaust combustion gas of propellant. The comparative tests by BSF165mm motor have further confirmed the contribution of HMX to specific impulse.
出处
《固体火箭技术》
EI
CAS
CSCD
1996年第2期26-29,共4页
Journal of Solid Rocket Technology
关键词
端羟基苯丁二烯
推进剂
比冲
能量增益
Hydroxy terminated polybutadiene propellant
HMX(octogen)
specific impulse Energy gain
