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推进剂    
相关语句
  propellant
    Relation between Variabcle Law of Pressure and Concentration of the Propellant in Aerosol Can
    喷雾罐内推进剂压力及浓度变化的探讨
短句来源
    Portable Propellant Leakage Detector
    便携式推进剂泄漏检测仪
短句来源
    REALIZATION OF ULTRASONIC LONG-DISTANCE MEASUREMENT OF PROPELLANT LIQUID LEVEL OUTSIDE THE TANK
    推进剂液位罐外超声波远距离检测的实现
短句来源
    The sloshing of the propellant fuel have to be suppressed to avoid the coupling between the liquid sloshing and the structure vibration. The sloshing frequency and the natural frequency of the structures structures must be kept out of the frequency bandwidth of the rocket control systems.
    为了使导弹和航天运载器具有良好的飞行稳定性,就必须对其内部液体推进剂的晃动加以抑制,避免使液体的晃动与整体结构的固有振动发生耦合,防止结构的固有振动频率和液体的晃动频率落入控制系统的频带之中。
短句来源
    A portable mass spectrum detector used for propellant leakage is introduced. The design, structure and characteristics of the detector are described, and the performance experiment result and the detection example in satellite propellant are given.
    介绍了一台用于航天器推进剂泄漏检测的便携式小型质谱检测仪,详细阐述了仪器的设计、结构及特性,给出仪器的性能实验结果及卫星的推进剂的检测实例。
短句来源
  propellants
    EVALUATION OF THE PROCESSING HAZARD OF SOLID PROPELLANTS BY MEANS OF FUZZY MATHEMATICS
    固体推进剂制造工艺危险性的模糊评定方法
短句来源
    To prepare high performance solid propellants, superfine particles are often appeared in the components of propellants.
    制备高能、高性能固体火箭推进剂时,推进剂配方中需要加入超细粉体。
短句来源
  propellant
    Relation between Variabcle Law of Pressure and Concentration of the Propellant in Aerosol Can
    喷雾罐内推进剂压力及浓度变化的探讨
短句来源
    Portable Propellant Leakage Detector
    便携式推进剂泄漏检测仪
短句来源
    REALIZATION OF ULTRASONIC LONG-DISTANCE MEASUREMENT OF PROPELLANT LIQUID LEVEL OUTSIDE THE TANK
    推进剂液位罐外超声波远距离检测的实现
短句来源
    The sloshing of the propellant fuel have to be suppressed to avoid the coupling between the liquid sloshing and the structure vibration. The sloshing frequency and the natural frequency of the structures structures must be kept out of the frequency bandwidth of the rocket control systems.
    为了使导弹和航天运载器具有良好的飞行稳定性,就必须对其内部液体推进剂的晃动加以抑制,避免使液体的晃动与整体结构的固有振动发生耦合,防止结构的固有振动频率和液体的晃动频率落入控制系统的频带之中。
短句来源
    A portable mass spectrum detector used for propellant leakage is introduced. The design, structure and characteristics of the detector are described, and the performance experiment result and the detection example in satellite propellant are given.
    介绍了一台用于航天器推进剂泄漏检测的便携式小型质谱检测仪,详细阐述了仪器的设计、结构及特性,给出仪器的性能实验结果及卫星的推进剂的检测实例。
短句来源
  propellant
    Relation between Variabcle Law of Pressure and Concentration of the Propellant in Aerosol Can
    喷雾罐内推进剂压力及浓度变化的探讨
短句来源
    Portable Propellant Leakage Detector
    便携式推进剂泄漏检测仪
短句来源
    REALIZATION OF ULTRASONIC LONG-DISTANCE MEASUREMENT OF PROPELLANT LIQUID LEVEL OUTSIDE THE TANK
    推进剂液位罐外超声波远距离检测的实现
短句来源
    The sloshing of the propellant fuel have to be suppressed to avoid the coupling between the liquid sloshing and the structure vibration. The sloshing frequency and the natural frequency of the structures structures must be kept out of the frequency bandwidth of the rocket control systems.
    为了使导弹和航天运载器具有良好的飞行稳定性,就必须对其内部液体推进剂的晃动加以抑制,避免使液体的晃动与整体结构的固有振动发生耦合,防止结构的固有振动频率和液体的晃动频率落入控制系统的频带之中。
短句来源
    A portable mass spectrum detector used for propellant leakage is introduced. The design, structure and characteristics of the detector are described, and the performance experiment result and the detection example in satellite propellant are given.
    介绍了一台用于航天器推进剂泄漏检测的便携式小型质谱检测仪,详细阐述了仪器的设计、结构及特性,给出仪器的性能实验结果及卫星的推进剂的检测实例。
短句来源

 

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  propellant
Analysis and operational results show that the control system can meet all technical requirements for high energy composite solid propellant manufacturing.
      
Comprehensive Substantiation of the Structure and Parameters of a Power-Propellant System for a Spacecraft
      
The conceptual and methodological principles, as well as some results of the comprehensive substantiation of a technical approach at early stages of design of power-propellant systems (PPS), are presented.
      
The time of turn is minimized, as well as the functional having a meaning of the propellant consumption.
      
The estimations of the propellant consumption for a realization of the programmed turn are made.
      
更多          
  propellants
An experimental method for determination of critical conditions of condensation of metal propellants of electric jet engines (EJEs) on the surfaces of materials of spacecraft thermoregulating covers is presented.
      
Mechanism of combustion of fire-extinguishing propellants based on potassium nitrate
      
A study is made of one-dimensional nonstationary problems of the combustion and detonation of aerosuspensions of unitary fuels or propellants, which contain the oxidant as well as the combustible material (gunpowder, high explosives).
      
The temperature of attainable superheating of rocket propellants is also calculated by the theory of homogeneous nucleation.
      
It is demonstrated that the employed kinetic model of thermochemical processes provides an adequate description of the available experimental data on the rate of combustion of AP- and PBR-based solid propellants.
      
更多          
  propellant
Analysis and operational results show that the control system can meet all technical requirements for high energy composite solid propellant manufacturing.
      
Comprehensive Substantiation of the Structure and Parameters of a Power-Propellant System for a Spacecraft
      
The conceptual and methodological principles, as well as some results of the comprehensive substantiation of a technical approach at early stages of design of power-propellant systems (PPS), are presented.
      
The time of turn is minimized, as well as the functional having a meaning of the propellant consumption.
      
The estimations of the propellant consumption for a realization of the programmed turn are made.
      
更多          
  propellant
Analysis and operational results show that the control system can meet all technical requirements for high energy composite solid propellant manufacturing.
      
Comprehensive Substantiation of the Structure and Parameters of a Power-Propellant System for a Spacecraft
      
The conceptual and methodological principles, as well as some results of the comprehensive substantiation of a technical approach at early stages of design of power-propellant systems (PPS), are presented.
      
The time of turn is minimized, as well as the functional having a meaning of the propellant consumption.
      
The estimations of the propellant consumption for a realization of the programmed turn are made.
      
更多          
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