2、

The influence of the ratio of composition Mg/ KNO 3 on the burning rate, near-infrared radiation intensity and visible light intensity is determined by experiment in this paper.

通过实验确定了镁/硝酸钾药剂的配比对燃烧速度、近红外辐射强度和可见光强度的影响。

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3、

One-dimensional interior ballistic calculation of solid rocket motors with dual burning rate propellant

串联双燃速固体火箭发动机一维内弹道计算

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4、

Testing method for flammability of clothes burning rate method

织物燃烧试验法:燃烧速度测试法

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5、

Based on the solid propellant burning rate formula, a new method for the combustion time determination during the data treatment in solid rocket motor firing test was studied with a method of numerical integration and interpolation.

以固体推进剂燃速公式为基础,采用计算力学中的数值积分及插值法,并利用计算机技术,研究了用燃烧室药柱的实际肉厚,确定固体火箭发动机试验曲线中燃烧时间的新方法。

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6、

This paper analyzes the effects of burning rate catalysts on the theoretical specific impulse ( ISS) and the pressure exponents of NEPE high energy solid propellants.

分析了燃速催化剂对NEPE高能固体推进剂理论比冲和燃速压强指数的影响。

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7、

The results show that it is content with exponential burning rate law. Based on the experiment data, the burning rate coefficient and exponent were adapted. The research results can give basic data for the interior ballistic design of the liquid propulsion system.

结果表明,它满足指数燃速定律,并从试验数据拟合出燃速系数和燃速指数,其结果可为液体推进系统内弹道设计提供基础数据。

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8、

The bench scale experiments of HTGR graphite ball-element were finished in an improved fixed bed burner, and the burning rate, thermal power, utilization ratio of oxygen, axial distribution of temperature and off-gas component were determined.

用改进的固定床燃烧器进行了台架规模石墨球燃烧实验,测定了燃烧速率,热功率,氧利用率,温度轴向分布和尾气组成。

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9、

Study on Software of Solid Propellant Burning Rate Prediction Based on one-dimensional Steady-state Reaction Gas Flow

基于一维气相稳态反应流的燃速预估软件研究

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10、

Simulating computation of burning rate temperature sensitivity of composite solid propellants

复合固体推进剂燃速温度敏感系数的模拟计算

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11、

And with increasing pressure, the ignition point and maximum burning rate point and burn out point were gradual decline.

并且随着压力的增加,着火点、最大燃烧速率点、燃尽点温度逐步下降。

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12、

Heat release rate, average burned gas temperature and NO formation as well as turbulent burning rate, turbulent flame propagating speel and flame speed ratio in different flame zones were computed as model output.

本模型不仅可以计算出燃烧放热率,燃气平均温度,NO生成规律,还可提供各火焰区的紊流燃烧速度、紊流传播速度和火焰速比等重要参数。

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13、

The function of coarse-particle aluminium powder in high burning rate solid propellant

在高燃速推进剂中粗颗粒铝粉的作用

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14、

The cross action between burning rate and curing reaction catalysts

燃速催化剂与固化催化剂的交叉作用

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15、

The effect of combustion conditions on burning-out time and maximum burning rate is researched, too.

另外,燃烧温度、空气流量、升温速率和试样量影响飞灰最大燃烧速率和燃尽时间。

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16、

A study on the cross action between burning rate and curing reaction catalysts is presented in this paper.

本文研究了燃速催化剂与固化催化剂的交叉作用。

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17、

The combustion characterisitics of GAP propellants containing different oxidizers are studied. Their flame structures and burning surface were observed and the burning rate-pressure relationship was measured.

研究了含不同氧化剂的GAP推进剂燃烧特性,观察了其火焰结构及燃烧表面,测量了推进剂燃速与压强的关系。

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18、

The thermal stability of high burning rate propellant is studied by DSC, methyl violet test and weight loss test.

DSC、甲基紫试验和失重试验研究了高燃速推进剂的热安定性。

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19、

Effects of components of fuel-rich boron-based solid propellant on burning rate in low pressure and explosive heat were investigated by measuring its burning rate with standard burner method and explosive heat with calorie meter of oxygen bomb.

采用推进剂静态燃速测试仪和氧弹式量热器的试验方法,研究了各组分对含硼富燃料推进剂低压燃速和爆热的影响。

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20、

It is found that the near-infrared radiation and visible light intensity are the largest when the ratio of Mg and KNO 3 is 50 ∶ 50.The burning rate is enhanced rapidly along with the increase of Mg in the composition.

经过试验发现:当镁与硝酸钾的配比为50∶50时,近红外辐射和可见光强度最大。随着药剂中镁含量的提高,燃烧速度迅速增加。

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