The experimental results indicate that coarse aluminium powder can be used in HTPB propellant.
结果表明粗铝粉在推进剂中使用是可行的。
The effect of the HMX content on the microwave attenuation of HTPB propellant has been studied.
研究了HMX含量对HTPB复合固体推进剂微波衰减的影响。
The experimental results show that TPB is an ideal curing catalyst of HTPB propellant binder system.
实验结果表明，TPB是丁羟推进剂粘合剂体系比较理想的固化催化剂。
Applying burning-rate catalysts is one of optimal approaches to regulate the burning rate of HTPB propellant.
使用燃速催化剂是调节丁羟推进剂燃速的最佳途径之一。
Nanometer metal powders also have catalytic effects on the thermal decomposition of AP/HTPB solid propellant.
纳米金属粉对AP/HTPB推进剂的热分解同样具有一定的催化效果。
The change rule of mechanical property of HTPB composite propellant with test time was studied by humidity test.
通过常温湿度试验，研究了HTPB复合推进剂力学性能随试验时间的变化规律。
The existence of any extender is not necessary for increasing the elongation of HTPB propellants by bonding agent MAPO.
扩链剂的存在不是键合剂MAPO提高丁羟推进剂伸长率的必要条件。
In this paper, the effects of the storage temperature on the ageing characteristics of HTPB propellants have been studied.
本文研究了贮存温度对丁羟推进剂老化性能的影响。
The result shows that the viscosity of propellant is lower by the bond of HTPB in the condition of same diameter particles.
结果表明：在粒径相同的条件下，采用粘合剂为推进剂组分的HTPB，其推进剂药浆粘度相对较低。
This paper has mainly studied the properties of HTPB and of blending adhesive improved by EP, 123 resin and nano materials .
主要研究了丁羟胶性能及其采用环氧胶、纳米材料、12 3树脂等改性后胶的拉伸性能、扯断伸长率。
The use of chain extenders ACTS as an important way to control the morphological structure of HTPB propellants binder matrix.
把扩链剂的使用作为调整丁羟推进剂粘合剂网络及其形态结构的一个重要手段。
This paper introduces the design and tests of a motor ignitor loaded with high energy propellant which is a mixture of HTPB and HMX.
介绍了一种装有高能推进剂的发动机点火器的设计和试验，高能推进剂选用HTPB、HMX混合药剂。
The influence of prepolymers (HTPB and 784) on the function of the bonding agent were also studied by chemical analysis, DTA, IRelc.
采用化学分析、红外分析、差热分析等手段，研究了HTPB和784两种粘合剂对键合剂效能的影响。
When FG and YB are incorporated, they may obviously reduce the pressure exponent of HTPB propellant as well as enhancing the burning rate.
当FG与亚铬酸铜组合使用时，可在提高推进剂燃速的同时大幅度地降低燃速压强指数。
The relationships between damage energies of HTPB propellants and storage ageing time were investigated by uniaxial repeated tensile test.
由单轴反复拉伸试验分别研究了含键合型防老添加剂和防老剂h的HTPB推进剂破坏能与贮存老化时间的关系。
Since most of the HTPB propellants possess similar aging mechanism, this model can be used to predict storage life of all HTPB propellants.
考虑到大部分HTPB推进剂的老化机理相似，所以该模型具有一定普遍性，适用于HTPB推进剂贮存期的预估。
To investigate the main aging mechanism of HTPB/TDI/MAPO polyurethane material, the aging properties were studied by accelerating aging method.
通过加速老化试验，研究了HTPB/TD I/MAPO类聚氨酯材料的老化性能，探讨了其老化机理。
The effect of AP particle size distributions and aluminum on the rheological behaviour of the HTPB propellant slurry were studied experimentally.
用实验流变学的方法研究了AP级配和铝粉对HTPB推进剂药浆流变性能的影响。
The effects of different silane end-capped ratios and HTPB content on mechanical properties, hardness and surface dry time of the sealant were discussed.
探讨了烷氧基硅烷封端率及端羟基聚丁二烯的含量对单组分密封胶的力学性能、硬度及表干时间的影响。
Cold flow field and simple reaction flow field of the combustion of HTPB and PS within the solid fuel ramjet (SFRJ) are simulated using PHOENICS program.
应用PHOENICS软件模拟了固体燃料冲压发动机(SFRJ)的冷流和以HTPB、PS为推进剂的简单反应流。
The pollutant samples in air of mixing, casting and vulcanizing sections of small-scale HTPB propellant processing line were taken by use of activated carbon.
以活性碳为吸附剂，对HTPB推进剂小型装药线混合、浇注、硫化岗位空气中的污染物进行了富集采样。
When blend modification of HTPB and PU are done, the apparent crosslinking density of PU matrix in - creases, and the tensile strength of propellant enhances.
将端羟基聚丁二烯与聚氨酯进行共混改性，提高了聚氨酯基体的表观交联度及推进剂的拉伸强度。
The effectiveness of coating boron particles coated with HTPB was characterized by using FT-IR, X-ray photoelectron spectroscopy and transmission electron microscope.
经过红外光谱、X-光电子能谱、透射电镜等对包覆效果进行了表征。
During the molding and storing process, humidity is the foremost factor affecting the characteristics of HTPB propellant grain and adhesion strength between interfaces.
在成型及贮存过程中，湿度是影响丁羟推进剂药柱性能及各界面的联合粘接强度的首要因素。
The effect of AP/HTPB Composite propellant thermal decomposition characteristics on initial change rate of fracture property during aging has been studied in this paper.
研究了AP／HTPB复合固体推进剂热分解性能对贮存老化期间增长断裂能初始变化率的影响。
An application investigation of the nitramine (RDX, HMX) to the low burning rate HTPB propellants was carried out in the view of energetic property and combustion performance.
从推进剂的能量特性和燃烧性能的角度探索了硝胺(rdx、HMX)在低燃速丁羟推进剂应用的可能性。
The results show that primary action of bonding agent improving RDX/HTPB propellant mechanical property was bonding agent improving interface adhesive effect of RDX grain to HTPB binder.
结果表明，键合剂改善RDX／HTPB推进剂力学性能的主要原因在于它们改善了RDX颗粒与HTPB粘结剂基体间的界面粘结效能。
Based on the ageing experimental results, the ageing dynamic equation of HTPB propellant is obtained. A calculation and reliability analysis for propellant storage life are also presented.
在分析老化实验数据的基础上，建立了丁羟推进剂老化的动力学方程，以此为基础预估了推进剂的贮存寿命，分析了贮存寿命的可靠性。
This paper expatiates upon the principle and application of Acoustic Emission (AE), and it is known that AE technique is applicable to HTPB composite solid propellant dynamic damage process.
阐述了声发射(AE)原理及应用，指出AE技术适用于研究HTPB复合固体推进剂动态损伤过程。
This paper expatiates upon the principle and application of Acoustic Emission (AE), and it is known that AE technique is applicable to HTPB composite solid propellant dynamic damage process.
阐述了声发射(AE)原理及应用，指出AE技术适用于研究HTPB复合固体推进剂动态损伤过程。
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