氧化铁可用以制出超高燃速的推进剂。
Iron oxide may be utilized in achieving propellants of ultrahigh burn rate.
分析了这种推进剂能提高燃速的机理。
For the propellant mechanism of increasing burning rate is discussed.
为高燃速推进剂比冲测试提供了可靠的试验依据。
It is a reliable measuring method of the specific impulse for the high-burning rate propellants.
整机具有自动控制测试、计算各种燃速参数等功能。
The instrument functions include autocontrol, automatic measurement and calculation of parameters, etc.
密闭燃烧器法是一种间接测定固体推进剂燃速的方法。
Closed burner method is used for determining burning rate of the solid propellants.
“燃速”基于迭代长度显示已完成和所需的工作速度。
The burn rate shows the completed and required rate of work based on the length of the iteration.
研究了多孔超高燃速推进剂代料的双螺杆混合挤出工艺。
Twin screw extrusion technology of porous ultra high burning rate propellant (UHBRP) substitutes was studied.
使用燃速催化剂是调节丁羟推进剂燃速的最佳途径之一。
Applying burning-rate catalysts is one of optimal approaches to regulate the burning rate of HTPB propellant.
甲基紫试验和失重试验研究了高燃速推进剂的热安定性。
The thermal stability of high burning rate propellant is studied by DSC, methyl violet test and weight loss test.
应用激光方法测量压力振荡过程中的固体推进剂瞬态燃速。
A laser method was used for measuring transient burning rate delay of solid propellant in oscillatory combustion.
在一些简化假设的基础上，找到了液滴质量燃速的近似解析解。
The approximate analytical solution on the burning rate of droplet mass is also found on the basis of some simplified hyPotheses.
用神经网络技术对固体燃料冲压动机的燃速辨识问题进行了研究。
The neural network is adopted to study the burning rate identification of the solid fuel ramjet.
分析表明促进凝相反应有利于含硼富燃料推进剂低压燃速的提高。
Thus, improving the condensed-phase reaction can increase of the burning rate for fuel-rich propellant with boron in low pressure condition.
含KD的推进剂燃速和平台范围可通过组合催化剂的变化来调节。
The burning rates and the plateau range of the propellant containing KD can be adjusted by means of the change of composite catalysts.
燃尽和燃速“燃尽”显示指定时间段内已完成和剩余工作的趋势。
Burndown and Burn Rate Burndown shows the trend of completed and remaining work over a specified time period.
采用声发射燃速测试方法研究了复合固体推进剂方坯燃速的均匀性。
The homogeneity of certified reference material is studied by acoustic emission method for composite solid propellant burning rate.
研究了某些无机铅盐和氧化铝对燃速压力指数及温度敏感系数的影响。
Effect of some inorganic lead salt and aluminium oxide on burning rate pressure exponent and temperature sensitive coefficient of polyurethane composite solid propellant have been investigated.
含不同增塑剂的推进剂的燃速随增塑剂中硝酸酯基含量的增加而增加；
The more nitrate ester group, the higher the combustion rate of propellant with different plasticizers;
本文对BDP稳态燃烧模型进行了必要修正，并用于预估推进剂稳态燃速。
The BDP steady burning model is revised in this paper and the revised BDP model is used in the prediction of steady burning rates of composite propellants.
同时，从基本模型出发，讨论了影响推进剂燃速压力指数的化学结构因素。
In the meantime, based on the basic model, the chemical structure factors which influence the pressure index are discussed.
结果表明，燃速缓慢下降是影响高能推进剂发动机内弹道性能变化的主要因素。
The results showed that the main influencing factor to the interior ballistics of solid motor with high energy propellant is the slow descending of burning rate.
并测量了推进剂的爆热和燃速，比较了AP包覆硼粒子对推进剂燃烧性能的影响。
The difference of the burning peculiarity between propellants whose boron was coated with and without AP was compared by measuring the explosive heat and burning rate of the propellants.
在提高固体推进剂燃速的众多方法中，采用纳米催化剂被认为是最有前途的方法之一。
Among those methods to improve the burning rate of solid propellant, the nanometer-sized catalyst has been considered as one kind of most prospective methods.
结果表明：二茂铁衍生物（RMT）能大幅提高推进剂燃速和降低高压燃速压强指数。
The results show that ferrocene derivant (RMT) can effectively enhance burn rate of propellants and reduce its pressure exponent under high pressures;
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。
When FG and YB are incorporated, they may obviously reduce the pressure exponent of HTPB propellant as well as enhancing the burning rate.
根据试验结果，论述了燃速增加率与燃烧历程的关系，提出和探讨了燃烧物理模型问题。
Based on the results of tests, the relationship between burning rate augmentation and burning time is discussed. A physical model is also presented and studied.
增加AP含量和金属添加剂中镁粉含量均有助于提高推进剂的燃速和拓宽其低压可燃极限。
The greater the contents of AP and magnesium are, the higher burning rates of the propellant and the broader flammability limit.
本文介绍了近年来国外进行的有关探讨等离子体提高发射药燃速的实验装置、方法和结果。
This paper mainly introduced the experimental studies on burn rates of the propellant with plasma abroad, including experimental equipments, methods and results.
分析讨论了用一根药条测量固体推进剂燃速系数和压力指数的方法，并给出了测量和处理结果。
The method to measure the burning rate coefficient and pressure index of a solid propellant with only one strand is discussed and analyzed, and the measured and processed results are given.
密闭燃烧器法是一种能测定很宽压强范围内固体火箭推进剂燃速特性及变化情况的快速测量方法。
Burning rate measurement with closed burner is a rapid method for measuring burning rate character and its change of solid rocket propellants in a wide pressure range.
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