double base propellant

英 [ˈdʌbl beɪs prəˈpelənt] 美 [ˈdʌbl beɪs prəˈpelənt]

双元(基)燃料火箭推进剂

化学



双语例句

  1. The effects of TPUE on the mechanical properties, technique properties, combustion and energy properties of nitramine modified double base propellant are studied.
    研究了热塑性聚氨酯弹性体对硝胺改性双基推进剂的能量性能、力学性能、燃烧性能以及工艺性能的影响。
  2. Numerical Simulation for Burning Rate of Composite Modified Double Base Propellant Containing CL-20
    含CL-20的改性双基推进剂燃速数值模拟
  3. Effects of Carbon Black on Burning properties of Plateau Double Base Propellant with Low Flame Temperature
    炭黑对低燃温双基平台推进剂燃烧性能的影响
  4. The Study on NC Content in Double Base Propellant with GPC Method
    GPC法测定双基火药中硝化棉含量的研究
  5. Aerodynamic Design for an Inflatable Reentry and Descent Decelerator Study on Probability of Double Base Propellant for Airbag Inflation
    充气气囊减速方案的气动设计研究双基推进剂用于气囊充气的可行性探讨
  6. Heat Ageing Experiment and Application of Initial Void Content ─ A New Method to Predict Storage Life of Double Base Propellant Grains
    初始气孔率热老化试验研究与应用&预测双基推进剂储存寿命的一种新方法
  7. Research on Low Burning Temperature Mesa Double Base Propellant
    低燃温麦撒双基推进剂研究
  8. The effect of carbon black on burning properties of modified nitramine double base propellant was detailed in this paper.
    分析了在硝胺改性双基推进剂中炭黑对其燃烧性能的影响。
  9. Experimental Research on Increasing the Burning Rate of Screw Extrusion Modified Nitramine Double Base Propellant
    提高螺压硝胺改性双基推进剂燃速的试验研究
  10. A Non-lead Catalyzed Nitramine Modified Double Base Propellant with Low Burning Rate and Low Flame Temperature
    一种非铅催化硝胺改性双基低燃速低燃温推进剂
  11. In order to improve the mechanical properties, a novel thermoplastic polyurethane elastomer ( TPUE) with good miscibility with NG and NC is synthesized and used in modified double base propellant.
    为了改善力学性能,合成了与硝化甘油(NG)、硝化纤维素(NC)具有良好相溶性的新型热塑性聚氨酯弹性体(TPUE),并应用于改性双基推进剂研究中。
  12. When the ingredient RDX of the composite modified double base propellant with plateau effect was replaced with DNTF, the propellant still possesses lower pressure exponent.
    DNTF代替具有平台燃烧特性的改性双基推进剂中的RDX后,推进剂仍可获得较低的压强指数。
  13. The deterioration of double base propellant SFM-3 for coastal defence missile during storage
    海防战术导弹用SFM-3双基药的贮存变质问题
  14. The adding of octogen also does not result in a obvious change of stability index of composite modified double base propellant.
    且含有奥克托今的改性双基推进剂的安定性指标没有明显变化。
  15. Application Research of Octogen Explosives in Screw Extrusion Composite Modified Double Base Propellant Safety Characteristics of Three Extruded Composite Modified Double Base Propellants
    奥克托今炸药在螺压改性双基推进剂中的应用研究三种挤压成型的改性双基推进剂的安全特性
  16. The propellant is characterized by low signature and insensitivity. The combustion catalyst adopted by ordinary double base propellant can adjust the burning rate. It's necessary to study further on the combustion mechanism.
    该推进剂具有低特征信号、低易损性等特点,用一般双基药所采用的燃烧催化剂可调节燃速,深入研究其燃烧机理很有意义。
  17. The action mechanism of an organic matter to double base system propellant was discussed in this paper. The effect of this matter to combustion performance was studied by a series of experiments.
    探讨了某有机化合物在双基系推进剂吸收工艺中的作用机理,用一系列实验研究了此工艺助剂对推进剂燃烧性能的影响。
  18. Studies on Foundational Formulation of Composite Modified Double Base Propellant Containing RDX and its Burning Rate
    含RDX改性双基推进剂基础配方及其燃速探索
  19. The paper gives the performance characteristic of a new type modified double base solid propellant, and it is compared with the traditional double base propellant.
    论文研究了一种新型改性双基固体推进剂的性能特点,并与传统的双基推进剂进行了比较。
  20. The Experimental Study on the Thermal Aging Combustion Property of the Composite Modified Double Base Propellant and its Life Time Calculation
    改性双基推进剂热老化燃烧性能试验研究与寿命预估
  21. Method based on ATR FTIR system is successfully introduced to measure the concentration curve of polymer deterrent in small arms double base gun propellant.
    研究表明采用ATR-FTIR方法可以定量测试小尺寸钝感枪药表面高分子钝感剂浓度分布曲线,钝感双基球扁药表面高分子钝感剂浓度呈指数规律分布。
  22. Recent Progresses of Models for Predicting the Burning Rate of Nitramine Propellant and Double-Base Propellant
    硝胺推进剂和双基系推进剂燃速预估模型进展
  23. The manufacturing technology of seismic charge with high detonation velocity containing single base propellant and double base propellant is researched.
    研制含单基药、双基药的高爆速震源药柱,并对其制造工艺进行了研究。
  24. Temperature distribution of combustion flame of double base propellant, composite propellant and NEPE propellant ( taking HNIW or HMX as oxidizer) were measured by using relative light intensity method.
    采用相对光强度法测定了双基推进剂、复合推进剂及NEPE(氧化剂为HNIW或HMX)推进剂的燃烧火焰温度分布。
  25. Molecular Design of the Bonding Agent for Double Base Propellant
    双基推进剂硝胺脱湿及其键合剂分子设计
  26. A Study on Application of Technical-aid-agent to Double-base System Propellant
    工艺助剂在双基系推进剂中的应用研究
  27. Analysis of Burning Characteristics for Double Base System Propellant at Environment Temperature 100 ℃
    初温为100℃时双基系推进剂的燃烧特性分析
  28. 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