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Transport vehicle engineering - 629

Scientific articles

In section "Transport vehicle engineering"
Стилевая направленность основных навыков управления автомобилем
Бебинов Сергей Евгеньевич, Сальников Виктор Александрович
Тренажерная подготовка как объект педагогического анализа в рамках авиационной педагогики
Невзоров Роман Викторович
Формирование иноязычной аудитивной компетенции как компонента профессиональной подготовки курсантов военного авиационного вуза
Суслова Юлия Викторовна
Специальная и летно-парашютная подготовка парашютистов по курсу учебно-спортивной подготовки 1937 г
Кононенко Сергей Викторович
Analysis of power capabilities of solar batteries under different operational condition
Bazilevsky A.B., Lukjanenko M.V.
The questions of methodology providing reliability of flying suitability and safety of civil aviation airplanes
Bondarenko V.G.
The problems of monitoring of reliability and flying suitability of civil aviation airplanes
Bondarenko V.G., Shajmardanov L.G.
Mathematical modelling of thermal streams space vehicle
Golikovskaja K.F.
Neural network based automation for vibration testing the space vehicle structural assemblies
Evtifjev M.D., A Lysenko E.
Optimization of the set of diagnostic parameters
Lukasov V.V.
Model of reliability of the satellite
Maksimov Ju. V., Patraev V.E., Tololo V.A.
Probabilistic estimate of knots friction and wear resource
Okladnikova E.N., Sugak E.V.
Computative-experimental assessment of the loading of space crafts in high-intensity pulse actions
Orlov A.S., Shatrov A.K.
The questions of methodology of individual prolongation of the civil aviation airplanes devices resources
Pavlenok A.A., Shajmardanov L.G.
Modelling of the process of the take-off run neavy transport airplane with purpose the definitions of take-off mass and the traction of engines by onboard self-recorder unit data
Pozhilenkov V.A.
Effectiveness of the applying of cellular constructions in aircraft
Slivinsky V.I., Tkachenko G.V., Slivinsky M.V.
Detection of defects in spacecrafts during vibration/acoustic tests under laboratory environment
Khalimanovitch V.I., Shatrov A.K., Lysenko E.A., Evtifjev M.D.
The analysis of technical service strategies of steering wheel drives for airplanes Tu-154M and B
Shajmardanov L.G., Nartov E.A.
Some kinds and problems of technical compatibility
Nosenkov A.A., Medvedev V.I., Mullin A.M.
Numerical research of the space vehicle transfer problem in circular orbit
Dudarev O.K., Okhorzin V.A.
Nonlinerian deformation of an orthotropic membrane stretched on the frame
Lopatin A.V., Shumkova L.V.
Task of the optimization of cabines cylindrical capsule with allowance for its reliability
Nagovizin V.N.
About alone algorithm of analyzing intermittent processes
Orlov V.S., H Khanov V.
The methods of estimation of visibility zones on Earth surface from a space vehicle for different orientations and solid angle values
Demenko V.V.
The energy model of nickel-hydrogen storage battery
Lukyanenko M.V.
An algorithm for analyzing the spacecraft vibration test data and preparing the acceleration input level
Akimov A.N., Evtifiev M.D., Lysenko E.A., Solovyeva T.I., Shatrov A.K.
The methodology to ensure immunity of the satellite equipment of plasma from the stationary plasma thrusters
Ivanov V.V., Maksimov I.A., Balashov S.V., Pervukhin A.V., Nadiradze A.B.
The mathematical models practical applying at flight information processing
Pozhilenkov V.A.
The experimental research of the contamination influence of the own outside atmosphere on the stage of spacecraft orbital operation
Nadiradze A.B., Smirnov V.A., Maksimov I.A., Khartov V.V., Tibildeeva V.V.
The investigation of contamination influence of own outside atmosphere and plasma of the stationary plasma thrusters on "Express-AM" spacecraft
Smirnov V.A., Nadiradze A.B., Maximov I.A., Hartov V.V., Shatrov А.К.
Optimal design of a sandwith beam with given a vibration frequencies
Lopatin A.V., Makarov I.V., Shumkova L.V.
Bases of operation of the glider without the between-repairs resource
Demin I.V., Katsura A.B.
The problems of monitoring of civil aviation airplanes functional systems reliability
Zosimov A.G., Nartov E.A., Shaimardanov L.G.
Computation model to calculate the penetration of electric jet thrasters plasma into the equipment bay of the satellite
Ivanov V.V., Maksimov I.A., Nadiradze А.В., Shaposhnikov V.V., Smirnov V.A.
The technique of definition of flight data for making the mathematical air craft movement describing model more precise
Pozhilenkov V.A.
The basic characteristics of the information supply systems of technical operation of flying devices
Demin I.V., Katsura A.B.
Decision of the problem of modelling of systems of maintenance service of flying devices
Nikushkin N.V., Katsura A.V.
The estimating method of the civil aviation airplanes functional systems reliability with a help of the user’s statistic materials
Madvedev V.L., Boyko O.G., Zosimov A.G., Shaymardanov L.G.
Reliability of the functional systems of long exploiting civil aviation airplanes
Medvedev V.L., Zosimov A.G., Shaymardanov L.G.
Peculiarities of modern stage of aerospace industry development and new requirements for specialists training
Philatov V.V.
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