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Analysis and improvement of characteristics of power supply systems for the small space vehicle of the AIST-2 type
Mordanov M.R., Safronov S.L.
Comparison of quasi-three-dimensional and full three-dimensional formulations of thrust bearing operation
Sokolov N.V., Khadiev M.B., Fedotov P.E., Fedotov E.M.
Bench tests of an electric engine-propeller group, as the first stage in the creation of a hybrid power plant
Sychev A.V., Ravikovich Y.A., Borisov D.A.
Influence of space vehicle remote power supply on thermal regimes of solar batteries
Steganov G.B., Beznyakov A.M., Nemirov A.V.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Analysis of basic concepts of advanced engines for supersonic civil aircraft on the basis of foreign designers’ experience
Alendar A.D., Grunin A.N., Siluyanova M.V.
Reducing energy consumption of vertical take-off and landing unmanned aerial vehicle using hybrid technical solutions
Lukyanov O.E., Hoang V.H., Komarov V.A., Nazarov D.V., Kurkin E.I., Quijada Pioquinto J.G., Chertykovtseva V.O.
Power plants of the first aircraft
Drygin A.S.
Analysis of temperature separation efficiency in vortex gas flows
Biryuk V.V., Kurnosov N.Y., Tarnopolsky A.V.
Interaction of high-speed particles and temperature control elements of a space vehicle
Izyumov M.V., Syomkin N.D., Kalayev M.P.
Using statistical Markov models for the analysis of electromagnetic compatibility of autonomous electric installations
Kubarkov Y.P., Goldshtein V.G., Inahodova L.M.
Spacecraft preset orbital parameters control by means of thrusters
Salmin V.V., Volotsuev V.V., Shikhanov S.V.
Increasing the efficiency of low-temperature power plants by selecting the optimal working fluid of the auxiliary circuit
Eliseev I.A., Tochenov V.V., Panshin R.A.
Heat engine cycle limitations imposed by fuel properties
Mikheyenkov E.L.
Mathematical models for evaluating the energy efficiency of ultralow power turbine drives
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Analysis of the stressed state of high-speed extrusion process
Kostyshev V.A., Pityugov M.S.
Mathematical model and peculiarities of operating mobile robots with hybrid drives
Ilyukhin Y.V., Tatarintseva A.V.
Device for fitting thick-film resistors
Piganov M.N., Shopin G.P., Stolbikov A.V., Erendeev Y.P.
Problems of simulation and calculation of modes of electrical engineering complexes and off-line systems of electrical power supply
Kubarkov Y.P., Goldshtein V.G., Amelin S.V.
The efficiency of aligning gratings at engine inlet of ground power plants
,
Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200
Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.A.
Prospects and problems of movement and power plants in powder metal fuel
Egorov A.G., Tizilov A.S.
Mathematical description of the interaction between a probing microwave signal and the helicopter main rotor blade
Danilin A.I., Zhukov S.V., Popov M.S.
Statistical physics and cycles of operation of heat engines
Mikheenkov E.L.
The application of technology microarc oxidation to repair and restore characteristics of products from aluminum alloy AK9
Krishtal M.M., Yasnikov I.S., Ivashin P.V., Polunin A.V.
Experimental study of a power absorber of accelerated fluid flow in pipelines
Gimadiev M.A., Gimadiev A.G.
Calculation of power dissipation in corps of onboard equipment of space vehicle in direct electrostatic discharge
Kostin A.V.
Parametric analysis of thermoacoustic travelling-wave engine operation with external heat application
Dovgyallo A.I., Zynovyev Y.A., Vorotnikov G.V.
Optimization characteristics of rotor-support system from NK-14ST free power turbine with consider statics and dynamics propertys
1 1., 1 1.
Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics
Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.
Method of coordinating joint operation of air starter and auxiliary power unit and determining the gas turbine engine starting time
Popov G.M., Baturin O.V., Novikova Y.D., Zubanov V.M., Volkov A.A., Korneeva A.I.
Development of a pulsation dampener for hydraulic systems of power plants
Kryuchkov A.N., Еrmilov M.A., Еrmilova E.N., Balakhonov I.V., Vidyaskina A.N.
Analysis of information characteristics of a dynamic displacement doppler transducer signal
Danilin A.I., Gretskov A.A.
Common properties of hydrocarbon combustion products and Brayton cycle
Mikheenkov E.L.
Volume and mass mathematical models of single-stage centripetal ultralow power turbines
Grigoriev V.A., Kalabukhov D.S., Rad'ko V.M.
Approaches to modeling work of gas turbine engine`s core as a connected task
Krivcov A.V., Shabliy L.S., Baturin O.V.
Primary converters for the implementation of Doppler method for measuring blade oscillation power unit
Danilin A.I., Gretskov A.A.
Technical analysis tools improvement by spectral analysis and diginal filtration theory using
Sitnikova A.U.
The algorithm of calculation combined energy installations, based on turbojet and SOFC
Loskutnikov A.F., Bakirov F.G., Gorjunov I.M.
Limit values of the Brayton cycle with the use of reduced fuel characteristics
Mikheenkov E.L., Nekrasova S.O.
Technology of low-emission fuel combustion and conceptual structure of the combustion chamber of a gas-turbine power plant
Tsybizov Y.I., Tyulkin D.D., Vorotyntsev I.E.
Application of additive technology of selective laser melting (SLM) in designing a low emission combustion chamber of a gas turbine plant
Yeliseev Y.S., Fedorchenko D.G., Golanov S.P., Tsibisov Y.I., Tyulkin D.D., Vorotyntsev I.E., Ivchenko A.V.
Resonant converter with PWM output voltage adjustment
Vorokh D.A., Makhov A.I.
Possibility of using a bi-directional impulse turbine in a thermo-acoustic engine
Dovgjallo A.I., Shimanov A.A.
Selection of optimal configuration and workflow parameters of autonomous micro gas turbine plant
Baturin O.V., Smirnova Y.D.
Vortical gaz-wind-energy plant
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Thermodynamic shape of the combined power installations, based on GTU and solid oxide fuel cells
Loskutnikov A.A., Gorjunov I.M., Bakirov F.G.
High energy sypply spacebus with nuclear reactor power source for earth remote sensing purposes
1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.
Method of calculation and analysis of gas flow aerodynamic indices in a vortex wind power plant
Biryuk V.V., Uglanov D.A., Gorshkalev A.A., Bolshov D.V., Krasnorutskiy A.S., Lapshina V.A., Chertykovtsev P.A.
Choise of the range and levels of varying the factors of the experiment plan for testing single-stage ultralow power turbine
Grigoryev V.A., Radko V.M., Kalabukhov D.S.
Development of methods for ensuring energy balance for the operation of mission equipment of “AIST”-series small satellites under conditions of power limitations
Ivanushkin M.A., Salmin V.V., Tkachenko S.I., Tkachenko I.S., Volgin S.S.
Analysis of the features of Earth surface clutter formation in the case of low-flying target detection with the use of a bistatic radar
Vorontsova S.A.
Experimental investigation of a small-sized centrifugal compressor for a closed-brayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Gas turbine engine simulation strategy in CAE systems
Krivcov A.V.
Adhesion strength of heat-insulating and wear-resistant ceramic coatings on aluminum alloys
Krishtal M.M., Ivashin P.V., Polunin A.V., Pavlov D.A., Nikerov K.N.
Prospects for the forcing of gas turbine and steam power plants
Pavlova A.A.
Choosing the structure of power-supply systems for low-orbit space vehicles
1 1., 1 1., 1 1., 1 1.
Development of the finite element model of vibroacoustical characteristics of pipe system
Mironova T.B., Prokofiev A.B., Shahmatov E.V.
Vortex wind power plant
Biryuk V.V., Krasnorutskiy A.S.
Efficiency of technical workings out in batch production GTE
Aleksentsev E.I., Shitarev I.L., Kurbatov V.P., Gritsenko E.A.
Engines for domestic drones: past, present and future
Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.
Spacecraft power supply system using additional low-power sources of energy
Kargu D.L., Beznyakov A.M., Nemirov A.V.
Development of a prototype of a multi-loop closedbrayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Doppler method for measuring fluctuations of elements rotationg parts power
Danilin A.I., Gretskov A.A.
Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection
Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.
The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage
Ivanov V.P., Partola I.S.
Use of control volume method for the temperature field calculation by laser influence
Murzin S.P., Mezhenin A.V., Osetrov E.L.
Method of reduced fuel characteristics and parameters of the operating cycles of heat engines
Anastaseev V.V., Belozertsev S.V., Mikheenkov E.L., Nekrasova S.O.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
The determination of the thermoacoustic generator aspect from electrodynamic unit features by the parametric-studies
Vorotnikov G.V., Kruchkov A.N., Zynovyev E.A.
Schemes, parameters, work process, characteristics and structure of long-range interception aircraft engines
Kovalev A.V., Sanin V.N., Krivenok A.G., Korolenko V.V.
Empirical metod of predicting aviation piston engine noise
Moshkov P.A.
Post-operation state and extension of service life of compressor blades of the gas-turbine power plant GTE-45-3
Tarasenko Y.P., Berdnik O.B., Tsareva I.N.
Pressure pulsation dampener for air controller
Igolkin A.A., Safin A.I., Shakhmatov E.V.
Forecasting the individual performance capabilities of the rocket engine powerplant units at the maintanance stage
Biryuk V.V., Bronshtein V.M., Presnyakova A.S., Shatilova M.Y., Dostovalova S.S.
The use of regression models for estimating the standards of electric power losses in its transfer by territorial network companies
Goldshtein V., Kubarkov Y., Rygalov A., Revyakina E., Stepanov V.
The story of invention and development of supercharge units of internal combustion engines
1 1., 1 1., 1 1.
Verification of a complex of mathematical models of aerodynamics and dynamics of Savonius rotor motion
Sizov D.A., Onushkin Y.P., Krasnova O.A., Dzhanibekov O.T.
Increasing the lifetime of power gyroscopes and momentum wheels
Khrutskaya M.V., Kamaldinov A.M.
Increase of welded joints strength at welding nickel-based alloys by pulse laser influence
Murzin S.P., Tregub V.I., Nikiforov A.M.
Peculiarities of using additional low-power energy sources in the power supply system of small spacecraft
Kargu D.L., Beznyakov A.M., Nemirov A.V., Radionov N.V., Chudnovsky Y.A.
Planning a factorial experiment for testing a single-stage ultralow power turbine
Grigoryev V.A., Radko V.M., Kalabukhov D.S.
Control of the aircraft hydraulic system technical conditions on the basis of monitoring viscidity values and purity level of fluid power
Kovalev M.A., Borodkin G.V.
Log-periodic oscillations in hierarchical models
Pivovarova A.S.
Discrete phase converters moving elements rotating units power units
Danilin A.I., Grechishnikov V.M.
Application’s ways of gas–turbine power plants of NK-family for upgrading of heat electric generation plant
1 1., 1 1., 1 1., 1 1.
The main trends of aviation science development
Alyoshin B.S., Chernyshev S.L.
1 - 87 of 87 Items

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