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火箭     
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  rocket
     Studies on Theory and Strategy of Intelligent Fault Diagnosis for Liquid-Propellant Rocket Engine
     液体火箭发动机智能故障诊断理论与策略研究
短句来源
     Investigation on Performance and Influence Factors of Rocket Ejector Mode of RBCC
     RBCC引射火箭模态性能与影响因素研究
短句来源
     Virtual Prototype Design and Simulation of the Rocket Launcher System Based on WIDSS
     基于WIDSS的火箭发射装置虚拟样机设计及动力学仿真
短句来源
     Optimization Design for Cost of Solid Rocket Motors
     固体火箭发动机面向成本优化设计
短句来源
     Fuzzy Reliability Analysis for a Flanged Connection System of Rocket Motors
     火箭发动机法兰连接系统模糊可靠性分析
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  propellant rocket
     Let the liquid propellant rocket engine parameter X be the normal probability distribution of μ and σ2, σ2 = σA2 + σE2, where σE2 is the engine run to run variance and σA2 is the engine to engine variance.
     一批液体燃料火箭发动机的性能指标X是。 N(μ,σ),σ~2=σ_A~2+σ_E~2,σ_A~2是发动机性能的台间方差,σ_E~2是台内方差。
短句来源
     APPLICATION OF ANNULAR INSTABILITY MODEL TO FY-20 LIQUID PROPELLANT ROCKET ENGINE
     环形不稳定性计算模型在FY-20液体火箭发动机上的应用
短句来源
     FAULT DIAGNOSIS AND MONITORING OF A LIQUID OXYGEN/KEROSENE PROPELLANT ROCKET ENGINE
     液氧/煤油火箭发动机故障诊断与监控
短句来源
     Study of the fault diagnosis technology for liquid propellant rocket enging by plume UV-VIS radiation
     羽流UV-VIS辐射在液体火箭发动机故障诊断中的应用技术研究
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     Mass analysis of pump-pressurized hydrogen/oxygen liquid propellant rocket engine
     泵压式氢/氧液体火箭发动机质量分析
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更多       
  rockets
     Kings Beat Rockets 91-89in NBA Beijing Game 91-89
     NBA中国赛北京站:国王91比89战胜火箭
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     Research into POGO Vibration of Liquid Rockets
     液体火箭的POGO振动研究
短句来源
     A nonlinear model on the simulation of pogo vibrations in liquid rockets
     液体火箭Pogo振动蓄压器非线性仿真研究
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
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     Analysis of Radar Echoes on Effects of Rain Enhancement by AgI-Loading Rockets
     火箭增雨效果雷达回波分析
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更多       
  rocket motors
     Research on low frequency unstable combustion of H_2O_2-PE hybrid rocket motors
     H_2O_2-PE固液火箭发动机低频不稳定燃烧研究
短句来源
     CAD System Structure for Solid Rocket Motors
     固体火箭发动机CAD系统结构
短句来源
     CONCEPTUAL PRELIMINARY DESIGN EXPERTSYSTEM FOR SOLID ROCKET MOTORS
     固体火箭发动机概念设计 CAD 专家系统设计
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     Analysis of impact signal response spectrum of solid rocket motors
     固体火箭发动机冲击信号响应谱分析
短句来源
     ANALYSIS OF CALCULATING METHODS FOR STRUCTURAL RELIABILITY IN SOLID ROCKET MOTORS
     固体火箭发动机结构可靠性计算方法分析
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  rocket
Microbiological Degradation of Asymmetric Dimethylhydrazine, a Toxic Rocket Fuel Ingredient
      
The possibility of microbiological cleaning of water and soil polluted with asymmetric dimethylhydrazine (ADMH), a highly toxic ingredient of rocket fuel (IRF), was studied.
      
Consideration was given to the controlled solid bodies such as aircraft, rocket, and so on moving in the aerodynamic medium.
      
Peculiarities of Estimating the Aircraft Performance Characteristics of the Rocket-and-Space Facilities under Conditions of Fuzz
      
The method is based on the results of measurements of the state parameters and geophysical conditions of the employment of the rocket-and-space facilities under conditions of uncertainty of the a priori data on measurement errors.
      
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  propellant rocket
Monte Carlo simulation algorithms are given which are intended for the calculation of the spectral emissivity of jets of combustion products of solid-propellant rocket motors (SRM).
      
The Outflow of a Two-Phase Gas-Liquid Mixture from the Mixing Head of a Gas Generator when Starting a Liquid-Propellant Rocket E
      
This paper deals with the problems of mathematical simulation of the start-up of a liquid-propellant rocket engine (LPRE), which are associated with two-phase flows in the mixing heads (MH) of combustors and gas generators.
      
The instability of the working process in the combustion chamber of a solid-propellant rocket engine
      
Heat transfer in the thrust chamber is of great importance in the design of liquid propellant rocket engines.
      
更多          
  rockets
Ions with a Mass Number of Two in Mass-Spectrometric Experiments aboard Rockets and Satellites
      
Results of the calculation of the structure of relaxation shock waves in gas suspensions of the solid fuel of rockets are given in [8].
      
The mass-energy and specific characteristics of the propulsive jet discharges of rockets were factorized.
      
Variations in the electron density in the midlatitude ionospheric D region during launches and flights of different-type rockets at various distances from the launching site have been experimentally studied using partial reflections.
      
Coning motion stability of wrap around fin rockets
      
更多          
  rocket motors
The operation of rocket motors is often accompanied by the development of powerful secondary vortices in the combustion chamber [1-3], The superposition of the secondary vortices on the main flow leads to the formation of a cellular flow structure.
      
Monte Carlo simulation algorithms are given which are intended for the calculation of the spectral emissivity of jets of combustion products of solid-propellant rocket motors (SRM).
      
For technological reasons many high-performance solid rocket motors are made from segmented propellant grains with non-uniform port geometry.
      
This research demonstrated that hybrid rockets offer a safe, reliable upper stage option that is a versatile, cost-effective alternative to solid rocket motors.
      
Comprehension of wall-injection flow in a channel in the presence of different geometric discontinuities is necessary as part of the general investigations concerning combustion instabilities of solid propellant rocket motors.
      
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