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   双基推进剂 的翻译结果: 查询用时:1.131秒
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双基推进剂     
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  double base propellant
     Synthesis and Characterization of P(E-CO-T)-N100 and Its Application in Crosslinked Modified Double Base Propellant Binder
     P(E-CO-T)-N100预聚物的合成、表征及其在改性双基推进剂粘合剂体系中的应用
短句来源
     Dynamic mechanical characterization of aging properties for SJ-1 double base propellant
     SJ-1双基推进剂老化性能的动态力学表征
短句来源
     Study on the composite modified double base propellant containing3,4-dinitrofurazanfuroxan (DNTF)
     含3,4-二硝基呋咱基氧化呋咱(DNTF)的改性双基推进剂
短句来源
     Improvement of Combustion Property of Double Base Propellant by N,N'-dinitropiperazine
     利用N,N’-二硝基哌嗪改善双基推进剂燃烧性能
短句来源
     The propellant containing an organic potassium salt (symbolized by KD) maintains the flame structure characteristics of plateau double base propellant, but the propellant containing K 3AlF 6 possesses completely different flame structure.
     含有机钾盐KD的推进剂的火焰结构保持了平台双基推进剂火焰结构的特征 ,而含K3AlF6 的推进剂却有着完全不同的火焰结构。
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  double-base propellant
     Catalysis of Bismuth 2,4-Dihydroxylbenzoate in Combustion of Double-base Propellant
     2,4-二羟基苯甲酸铋对双基推进剂燃烧的催化作用
短句来源
     Combustion mechanism of double-base propellant containing bismuth 2,4-dihydroxylbenzoate
     含2,4-二羟基苯甲酸铋催化剂的双基推进剂燃烧规律
短句来源
     CARS Diagnostics for Combustion Flame Temperature of Double-base Propellant
     双基推进剂燃烧火焰温度CARS测定技术
短句来源
     Microwave Attenuation of the Exhaust Plume for Double-Base Propellant Rockets
     双基推进剂火箭排气羽流的微波衰减
短句来源
     Especially the difference is more obvious in the experiments of the high temperature. But the result is same as the "171" propellant around 100 centigrade. The article test the chemical stability through the different method and estimate the safety store age is more than 15 years of the new modified double-base propellant.
     新型高燃速改性双基推进剂由于配方中含有较多的硝化甘油和新型的燃烧催化剂,其化学安定性比一般双基推进剂安定性差一些,特别是试验温度较高时,这种差别更为明显,但是在100℃左右的温度下,其试验结果与171火药相似,本文通过采用不同的方法对这种推进剂的安定性进行了测试,预估这种新型的改性双基推进剂的安全贮存寿命可达15年以上。
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  double base propellants
     Influence of plasticizers on dynamic mechanical properties of double base propellants
     增塑剂对双基推进剂动态力学性能的影响
短句来源
     The influence of the nitrogen contents of nitrocellulose,liquid energetic plasticizers DDXZ and NG,and solid plasticizer P on the dynamic mechanical properties of double base propellants was investigated by the dynamic mechanical analysis method.
     用动态热机械分析方法考察了NC含氮量、液态含能增塑剂DDXZ和NG以及固态增塑剂P对双基推进剂动态力学性能的影响。
短句来源
     This is a comment with 58 references on the plateau combustion mechanism of the double base propellants.
     这是一篇关于双基推进剂平台燃烧机理的评论,参考文献58篇。
短句来源
     EXPERIMENTAL STUDIES ON CATALYTIC COMBUSTION OF DOUBLE BASE PROPELLANTS
     双基推进剂催化燃烧的实验研究
短句来源
     Safety Characteristics of Three Extruded Composite Modified Double Base Propellants
     三种挤压成型的改性双基推进剂的安全特性
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  double-based propellant
     Effect of Active-additive upon the Combustion Catalysis of Double-based Propellant
     活性添加剂对双基推进剂燃烧催化作用的影响
短句来源
     Response of High Energy Modified Double -Based Propellant to Shock Loading
     改性双基推进剂冲击波响应过程的研究
短句来源
     Development of HTPB Liner for Double-based Propellant
     双基推进剂用丁羟胶包覆层研制
短句来源
     It was showed that the model of combustion process of smokeless XLDB propellant is transferred from that of double-based propellant type to composite propellant type.
     结果表明,压力升高,无烟交联改性双基推进剂的燃烧模式由双基推进剂的燃烧模式转变为与复合推进剂类似的燃烧模式。
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  double base propellant
At TNO-PML a mastercurve of a double base propellant was constituted using dynamical mechanical analysis (DMA) and compared with a mastercurve reduced from conventional (static) stress relaxation tests.
      
The mechanical properties of this double base propellant determined by DMA were compared with conventional (quasi-static) tensile test results.
      
Figure 2 containstypical double base propellant burn rates which are comparedto AP and HMX monopropellant burning rates.
      
However, a double base propellant with an energy level equivalentto HMX will have a slightly higher rate than HMX.
      
The energy release has been measured for double base propellant, but measurements for AP or HMX are not available.
      
  double-base propellant
The linear expansions of two materials have been measured, a double-base propellant and a carboxyl-terminated polybutadiene.
      
Thermal decomposition studies on double-base propellant compositions
      
Thermal reactivity studies were carried out in the temperature range 100-160? on two double-base propellant compositions which differ significantly in chemical composition, calorimetric value and ballistic characteristics.
      
The thermal decompositions of a double-base propellant (DB), five triple-base propellants (TB) and nitroguanidine (NGV) were examined.
      
In the multi-component systems, DATH undergoes a strong interaction with the binder of the double-base propellant and a weak interaction with RDX.
      
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  double base propellants
Thermal decomposition studies of catalysed double base propellants
      
Results obtained suggest that condensed phase reactions may be the site for the action of lead salts in the combustion of double base propellants
      
However, the more conventional double base propellants consist of a solid gel matrix with additives, such as stabilizers.
      
For double base propellants the inner flame is -1200 to 1700 K depending on both pressure and binder energy.
      
In double base propellants HMX has little effect on the burning rate.
      
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