复合固体推进剂用键合剂的研究进展

键合剂是改善黑索金(RDX)、奥克托金(HMX)等硝胺和氧化剂填料与黏合剂间界面作用的关键功能材料,也是提高推进剂力学性能的有效、方便、实用的策略。综述复合推进剂中硼酸酯(BEBA)与中性聚合物(NPBA)等键合剂的研究进展,归纳了键合剂的作用机理,梳理了当前和未来高性能推进剂用键合剂的发展动向,针对不同的黏合剂体系和新的固化方式等发展趋势,设计具有多种功能基团的键合剂结构,积极开发可同时与硝胺、氧化剂及黏合剂相匹配的键合剂,进一步完善补充键合机理,以满足高新武器系统对高力学性能推进剂的需求。     

复合固体推进剂松弛模量的获取方法

采用传统方法、Joonas方法以及基于Prony级数的数据拟合法分别研究了HTPB复合固体推进剂的松弛模量,并以Prony级数形式表示.利用线黏弹性理论,得到哑铃型试件应力松弛实验和等速率拉伸实验的应力响应理论值,并与实验结果进行对比.结果表明,传统方法由于忽视了应变加载阶段,弹性模量小于实验值,Joonas方法需要计...     

复合固体推进剂老化研究

针对复合固体推进剂的老化问题,探讨了复合固体推进剂老化的主要因素;从复合固体推进剂组分的影响、环境湿度、储存温度等方面分析了其影响复合固体推进剂老化的机理;综述了复合固体推进剂贮存寿命的几种预估方法:力学性能法、阿累尼乌斯方程式法、凝胶含量法、傅里叶红外光谱法和动态粘弹法,并对这些研究方法的内容和结果可信度进行了分析。最后对复合固体推进剂老化研究的发展趋势进行了展望。     

HTPB复合固体推进剂材料声发射的特性

阐述了声发射原理及应用,指出ＡＥ技术适应于研究ＨＴＰＢ复合固体推进剂动态损伤过程。在声发射实验结果分析的基础上,得出了ＨＴＰＢ 合固体推进剂材料声发射特性。     

从复合固体推进剂中浸取高氯酸铵的动力学过程

为了探索以水为介质从复合固体推进剂中浸取高氯酸铵(AP)的动力学过程,分析了AP在水中的浸取过程,比较了不同浸取温度和试样厚度条件下AP的浸取平衡分离常数及其回收率,用SEM观察了浸取后的推进剂试样内部结构.结果表明,浸取速率常数随温度提高和推进剂试样厚度的减小而增大.浸取温度及试样厚度一定时,速率常数是定值,浸取速率...     

Burning Behavior of Composite Solid Propellant containing porous ammonium perchlorate

A pilot scale fluidized bed process was developed for preparing porous ammonium perchlorate (PAP) in various particle sizes. The oxidizer, ammonium perchlorate (AP), of composite solid propellant was partially replaced by PAP which was obtained by the fluidization process. The burning rate of propellants containing PAP was found to increase as compared with that of propellants without PAP. In the present study, the effects of percentage content and particle size of PAP incorporated in propellant compositions, on the burning rate were investigated. The results showed that the burning rate increases with increasing of PAP content and with decreasing of PAP particle size for trimodal oxidizer propellants.     

复合固体推进剂的催化热分解研究

用热分析技术研究复合固体推进剂凝聚相的催化热分解反应，得到大量的热分解参数和有关催化剂的作用规律。     

高固含量改性双基推进剂的热分解

采用高压DSC方法研究了不同固含量(RDX含量)推进剂的热行为.结果表明,随着RDX含量的增加,GLX推进剂中双基组分的分解峰逐渐变小,峰温前移,而RDX的分解峰随含量的增加而变强;随着压力的增大,GLX推进剂中两个放热分解峰的DSC峰温均有不同程度的下降,GLX推进剂的放热量也明显提高,放热分解峰变得更加明显,两峰温...     

复合固体推进剂生产中减少气孔的工艺研究

分析了工艺上导致某型复合固体推进剂生产中气孔产生的原因,给出了一些经过实践证明的行之有效的工艺措施及控制要求,对当前用类似的工艺生产复合固体推进剂具有一定的指导意义。     

复合固体推进剂在石灰石矿山深孔爆破中的应用

通过前期对石灰石矿山露天深孔爆破技术的了解和考察,首次将复合固体推进剂余药应用于石灰石矿山爆破工程,基于原有使用炸药的设计方法,结合现场情况,针对复合固体推进剂设计了一套爆破方案,并不断优化爆破参数,爆破结果表明,复合固体推进剂能够很好的满足石灰石矿山露天深孔爆破的要求,解决了长期以来以焚烧方式进行复合固体推进剂余药的销毁工作,为复合固体推进剂余药的销毁提供了一条新途径。     

Modeling of the Agglomeration Phenomena in Combustion of Aluminized Composite Solid Propellant

A theoretical model was developed in order to predict the size of agglomerates ejected from aluminized composite solid propellants. The model accounts for aspects of both mechanistic and geometric approaches. A thin mobile surface layer is assumed to dominate particle accumulation. Agglomeration number N_ag expressing the ratio between ignition and accumulation times, was found to greatly affect the characteristics of agglomeration phenomena, as noted in previous works. The concept of a characteristic distance D_e of the mobile surface layer was introduced, depending mostly on coarse AP particle diameter and loading. It was found to have a significant effect on the resulting agglomerate diameter. An agglomeration threshold was defined as the particle diameter equal to the mobile layer thickness. Particles smaller than this threshold have shown tendency to form large agglomerates, whereas particles with a somewhat larger diameter have demonstrated faster ignition and smaller ejected agglomerates. Model predictions for a number of propellant compositions showed good agreement with other theoretical studies as well as with experimental results.     

CTPB复合固体推进剂贮存老化性能研究概述

综述了端羧基聚丁二烯(CTPB)复合固体推进剂贮存过程中主要性能变化规律、老化影响因素及老化机理.     

B-GAP对复合固体推进剂能量性能影响理论研究

提高复合固体推进剂的能量性能的方法之一,是将普通的HTPB黏合剂替换成为含能黏合剂B-GAP.利用最小自由能法,对含能黏合剂B-GAP对复合固体推进剂的能量性能影响进行了理论研究,并计算出应用B-GAP的推进剂的燃烧室平衡温度、喷管出口温度、比冲等能量性能参数,将这些性能参数与丁羟推进剂进行比较,发现均有一定程度的提高...     

Three‐dimensional Structural Analysis Approach for Aging Composite Solid Propellant Grains

The viscoelastic aging behavior of composite solid propellant grains is studied by a three‐dimensional thermoviscoelastic constitutive model with aging evolution, in which the crosslinking degree is taken as an aging variable. The resulting viscoelastic constitutive equations are numerically discretized into incremental form by integration algorithms, and the stress‐updating method is presented according to incremental law. Subsequently, the Abaqus‐based user material subroutine and its structural analysis module are constructed and validated through typical examples. Studies show that the results of structural analysis have high accuracy and are in well agreement with each other. The designed analysis module presents an effective aging‐mechanical analysis platform for further lifespan estimation of solid rocket motors.     

用临界液萃取技术处理复合固体推进剂的工艺研究

通过对火箭发动机含高氮酸铵（AP）的复合推进剂用临界液氨销毁来介绍这一工艺方法。销毁工艺由四个连续的步骤构成：第一步采用临界液氨把含AP的复合推进剂从火箭发动机中取出;第二步萃取AP并将含AP的液氨和粘结剂残渣分离开;第三步从氨水中蒸发出AP;四第步将氨蒸气冷凝并重新循环使用。     

Development of Composite Solid Propellant Based on Nitro Functionalized Hydroxyl‐Terminated Polybutadiene

This paper presents an overview of a modified composite propellant formulation to meet future requirements. The composite propellant mixtures were prepared using nitro functionalized Hydroxyl‐Terminated Polybutadiene (Nitro‐HTPB) as a novel energetic binder and addition of energetic plasticizer. The new propellant formulation was characterized and tested. It was found that the Nitro‐HTPB propellant with and without energetic plasticizer exhibited high solid loading, high density, and reasonable mechanical properties over a wide range of temperatures. It was shown that the burning rate of Nitro‐HTPB propellant is up to 40% faster than that of the HTPB propellant. These results are encouraging and suggest that it should be possible to improve the ballistic performance of popular HTPB propellants through use of the studied Nitro‐HTPB binder.     

定应力和拉伸速率对复合固体推进剂反复拉伸试验的影响

为了获得交变应力作用下推进剂的疲劳性能参数,利用材料试验机对推进剂试件进行了反复拉伸试验,考察了定应力和拉伸速率对推进剂疲劳破坏的影响.结果表明,当拉伸速率一定时,推进剂试件所受的定应力越大,其循环破坏次数越少,而且应力水平和循环破坏次数的自然对数符合指数函数关系;当应力不变时,拉伸速率越快推进剂试件越容易发生破坏.试...     

固体贫氧推进剂研究

系统地综述了国内外固体贫氧推进剂的研究成果，对碳氢推进剂，含镁中能推进剂和含硼高能推进剂的配方特征，燃烧特征和燃速调节方法进行了评述，提出了各类推进剂应解决的主要问题。     

Numerical Prediction of Interior Ballistics Performance of Projectile Accelerator Using Granular or Tubular Solid Propellant

Two‐dimensional axisymmetric interior ballistics simulations in projectile acceleration systems that use granular or long slotted tubular solid propellants are performed using the solid/gas two‐phase fluid dynamics code of the Euler‐Lagrange approach. For validation, the simulation results are compared with experimental data for tubular solid propellants. In the series of the interior ballistics simulations, the propellant grain size and shape effects on the firing performance of 50 mm gun are numerically investigated. The propellant grain size and shape affect the energy release rate of the solid propellant charged in the chamber, the projectile kinetic energy at the muzzle, and even the fluctuations of the chamber pressure history. An appropriate burning surface area of the propellant grain exists, so that the projectile can achieve the maximum kinetic energy from the released energy of the solid propellant. Based on the simulation results, guidelines are proposed for the grain size design that enables the propellant energy to be used efficiently.