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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.
      
Shock-Acoustic Waves Generated during Rocket Launches and Earthquakes
      
Shock-acoustic waves generated during rocket launches and earthquakes are investigated by a method developed earlier for processing data from a global network of receivers of the GPS navigation system.
      
Classification of Gas-Dust Structures in the Upper Atmosphere Associated with the Exhausts of Rocket-Engine Combustion Products
      
This paper presents the results of investigating optical phenomena in the upper atmosphere that accompany rocket launches and are associated with specific features of the structure and dynamics of gas-dust formations in the upper atmosphere.
      
The insufficient energy resources of the rocket launchers is compensated by multiple gravity-assist maneuvers near terrestrial planets.
      
Risk Factors of Negative Impact on Objects of the Environment upon Accidents during Launches of Rocket-Space Hardware
      
The probabilistic aspects of rocket accidents during their launching and the motion in the troposphere are discussed.
      
The widely known problem of optimum control of the motion of a high-altitude rocket probe is also considered, and it is proved that in this problem no intermediate section can exist in the law of variation of the thrust.
      
A combination of a super gun and subsequent rocket propulsion using advanced chemical fuels appears to be the best solution for space flights of the near future.
      
It is pointed out that both problems can be solved in the near future using comparatively cheap standardized space vehicles launched into near-Earth orbits by the Soyuz carrier rocket and boosted further by electro-jet engines of small thrust.
      
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.
      
Such flows occur in elements of the gas-dynamic channel of turbojet engines and liquid-fuel rocket engines, ejector pumps, and other technical devices.
      
The development of rocket and space technology confronts experimental aerodynamics with the problem of reproducing more accurately the parameters of hypervelocity flow past bodies under laboratory conditions.
      
Equations of motion of ball lightning in a rocket airstream
      
Specific impulse losses due to friction and dispersion in a gas-film cooled liquid rocket engine nozzle
      
 

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