1) boron-based fuel-rich propellant
含硼富燃推进剂
1.
Effects of AP content and granularity gradation on pressure exponent of boron-based fuel-rich propellant;
AP含量及粒度级配对含硼富燃推进剂压强指数的影响
2.
In-depth researches on primary combustion of boron-based fuel-rich propellant containing 30% boron were completed on the base of experiments and theoretical analysis, establishing a basis for application on item of missiles.
在大量实验和理论分析的基础上,对含硼量为30%的含硼富燃推进剂一次燃烧进行深入地研究,为含硼富燃推进剂在型号应用奠定基础。
2) boron-based fuel-rich solid propellant
含硼富燃料固体推进剂
3) boron-based fuel-rich solid propellant
含硼富燃料推进剂
1.
In order to study the effect of agglomerated boron powder on the energy release and burning rate characteristics of boron-based fuel-rich solid propellant,the physical and mathematical combustion models of this propellant were established based on the experimental analyses and BDP model.
该模型充分考虑了团聚硼粉体积分数1ζ对推进剂燃面的影响,将硼粉的体积因素引入含硼富燃料推进剂的数学燃烧模型公式,该模型合理解释了这种推进剂的主要燃烧特性。
4) boron-based fuel-rich propellant
含硼富燃料推进剂
1.
Study on burning surface sedimentary deposit of boron-based fuel-rich propellant;
含硼富燃料推进剂燃烧表面“沉积层”研究
2.
Affecting factors on primary combustion ejection efficiency of boron-based fuel-rich propellant;
含硼富燃料推进剂一次燃烧喷射效率影响因素分析
3.
Improved timing device of burning rate test set for boron-based fuel-rich propellant;
含硼富燃料推进剂燃速测试计时系统的改进
6) boron-fuel-rich HTPB propellant
高能含硼HTPB富燃料推进剂
1.
Surface treatment and agglomeration distinctly improve the processing property of boron-fuel-rich HTPB propellants by rendering the boron powder unreactive or compatible with HTPB and optimizing the particle size distribution of solid filler.
采用硼粉表面处理和团聚成球工艺消除了硼表面杂质与HTPB的不良聚合反应,解决了推进剂中固体填料不合理的级配关系,使推进剂药浆5h表观粘度小于500 Pa·s,适用期大于16h,突破了高能含硼HTPB富燃料推进剂工艺难题。
补充资料：固液混合火箭推进剂(见火箭推进剂)
固液混合火箭推进剂(见火箭推进剂)
solid-liguid hybrid rocket propellant
guye hunhe huoiian tui)in)i固液混合火箭推进剂(s olid一Iiguid hy-brid rocket proPellant)见火箭推讲齐，}_
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条