1) colloidal propellant
胶态推进药
3) Propellant grain
推进剂药柱
1.
A calculatlon analysis for structural integrity of solid propellant grains under high overload;
高过载条件下固体推进剂药柱结构完整性分析计算
2.
Stress analysis of propellant grain loaded in composite case motor under vertical storage;
复合材料壳体发动机推进剂药柱立式贮存应力分析
3.
Transient temperature and stress analysis of propellant grains during cooling process after curing;
固化降温过程中推进剂药柱的瞬态响应分析
4) power propellant
火药推进剂
1.
In condition of the simulation test about the evaluation on impact loading on the explosive charge, several buffer materials of the power propellant charge of warhead are tested.
在“炸药装药抗高冲击过载评估技术研究”模拟试验软硬件条件下,对某战斗部火药推进剂装药几种缓冲材料性能进行试验测试研究,并对试验结果进行了分析和讨论,从而为某战斗部装填火药推进剂装药缓冲材料提供可靠依据。
5) gelled propellant
凝胶推进剂
1.
Study on the formulation of NTO gelled propellant;
四氧化二氮凝胶推进剂的配方研究
2.
Research and development of rheological and atomization characteristics of gelled propellants;
凝胶推进剂流变及雾化特性研究与进展
3.
Discussion on gelled propellant fluid characteristics in straight round pipe;
凝胶推进剂直圆管流动特性探讨
6) gel propellant
凝胶推进剂
1.
Preparation and properties research of UDMH/NTO gel propellant;
UDMH/NTO双组元凝胶推进剂的制备及性能研究
2.
Calculation and analysis of gel propellants thermodynamic characteristics;
非金属凝胶推进剂热力特性计算及分析
3.
To evaluate the effect of the tapered round pipe geometry,volumetric flow rate and gellant type or content on the pressure drop,the velocity and viscosity fields,the governing equations of the steady,incompressible,isothermal,laminar flow of a Power-Law,shear-thinning gel propellants in pipe were formulated,discretized and solved.
为讨论管道收敛角、体积流率、胶凝剂类型与含量等三因素对凝胶推进剂管道流动特性的影响,用SIMPLEC算法、二阶迎风格式离散柱坐标系下N-S方程,对凝胶推进剂在圆管中的流动进行了二维数值模拟,计算结果表明:(1)体积流率增大,粘度减小,含量增大,粘度增大,它们的改变引起粘度变化不显著;(2)收敛角增大,出、入口截面平均表观粘度降低幅度不断增大,出口截面平均表观粘度不断减小至近牛顿粘度水平η∞,当角度改变到一定值后,其引起粘度的变化将不再明显。
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