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Ensuring vibration characteristics of reactor plant centrifugal pumping equipment
Savchuk D.V., Bescherov D.E., Kulikov D.A., Panov V.A., Patrushev V.L., Porfiriev M.S., Soloviev S.A.
Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
Blinov V.L., Zubkov I.S.
The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review)
Alendar A.D., Lanshin A.I., Evstigneev A.A., Yakubovsky K.Y., Siluyanova M.V.
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.
Special features of assessing the strength of nuclear reactor equipment under dynamic loads
Lonin K.A., Panov V.A., Patrushev V.L., Savchuk D.V., Soloviev S.A.
Method of first-approximation calculation of take-off weight of a light aircraft with a hybrid propulsion system
Sychev A.V., Arbuzov I.V., Ravikovich Y.A.
Aircraft electric power plants
Kondryakov A.D., Leontiev M.K.
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.
Prospects and problems of movement and power plants in powder metal fuel
Egorov A.G., Tizilov A.S.
Neural network controller of a gas turbine plant low emission combustor
Avgustinovich V.G., Kuznetsova T.A., Sukharev A.A.
Methodology of designing a space transport system including a “DM” chemical upper stage and an electric rocket transport module
Russkikh A.S., Salmin V.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.
Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine
Kvetkin A.A., Kolesov A.V.
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.
Power plants of the first aircraft
Drygin A.S.
Selection of the optimum configuration and calculation studies of the parameters of a cryogenic propulsion system for an unmanned aerial vehicle
Tremkina O.V., Uglanov D.A., Urlapkin V.V., Korneev S.S., Komisar Y.V.
Selection of project structure for nanosatellite propulsion system
Belokonov I.V., Ivliev A.V., Bogatyrev A.M., Kumarin A.A., Lomaka I.A., Simakov S.P.
System-mathematical simulation of engine air hydraulic power supply
Goryunova N.R., Goryunov A.A.
Development of a prototype of a multi-loop closedbrayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Comparative evaluation of the effectiveness of the application of perspective types of electric propulsion thrusters in the small spacecraft
Kulkov V.M., Obukhov V.A., Yegorov Y.G., Belik A.A., Krainov A.M.
Hard & soft complex for “Angara” family launch vehicles engine system development
Partola I.S.
Use of the mathematical tool of hypervector ranging for selection energy-power plant of flight vehicles
Safronov V.V., Zhebrakov A.S.
Special aspects of numerical simulation of a two-stage axial-flow compressor with defective blades
Blinov V.L., Zubkov I.S., Iskortsev E.Y., Belyaev O.V., Plishkin P.I.
Preliminary tests of tank with cryogenic charging for onboard throttle system of cooling
Dovgjallo A.I., Sarmin D.V., Uglanov D.A.
Experimental research of combined technology for parts assembly
Glushchenkov V.A., Khardin M.V., Belyaeva I.A.
Research of shaft seals made of porous wire «metal rubber» material
Zhizhkin A.M., Zrelov V.A., Zrelov V.V., Ardakov A.Y., Osipov A.A.
Reduction of circumferential variation in the final stage of IPC
Popov G.M., Mamedov A.C., Smirnova Y.D.
The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage
Ivanov V.P., Partola I.S.
The main trends of aviation science development
Alyoshin B.S., Chernyshev S.L.
Analysis of characteristics of electric propulsion systems intended for carrying out maneuvers of maintenance of low Earth working orbit of small satellites
Salmin V.V., Volotsuev V.V., Nikitin A.V.
Development of the method of calculation and design stand installation for testingmodes wet cleaning duct GTE
Silaev B.M., Malcev E.N.
Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components
Titov B.A., Koltsov I.V.
Validation of CFD-models of gas turbine engine uncooled turbines
Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.
Vortical gaz-wind-energy plant
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Experimental determination of acoustic loads daunches of Strela LV and calculation of test modes for a spacecraft to be delivered by it to space
1 1., 1 1., 1 1., 1 1.
Optimal design of an induction heater of minimum length
Mednikova V.A.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
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.
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.
Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS
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.
Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy
Sinitsin L.I., Belokonov I.V.
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.
Examination of the theoretical possibility of creating a vernier electrorocket engine
Baigaliev B.E., Chernoglazova A.V., Tumakov E.A., Temnikova S.V.
Installation for strengthening local thermoplastic turbulent disc
Krutsilo V.G., Nikishov O.V.
Thermodynamic shape of the combined power installations, based on GTU and solid oxide fuel cells
Loskutnikov A.A., Gorjunov I.M., Bakirov F.G.
The story of invention and development of supercharge units of internal combustion engines
1 1., 1 1., 1 1.
Vortex wind power plant
Biryuk V.V., Krasnorutskiy A.S.
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.
Engines for domestic drones: past, present and future
Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.
11D58MF combined propulsion unit operating on oxygen-hydrogen fuel for an average-sized booster
Lupyak D.S., Smolentsev A.A., Sokolov B.A., Tumanin E.N., Tupitsin N.N.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.
Increase durability of gas turbine disks
Nikishov O.V., Krutsilo V.G.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
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.
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.
Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft
Kurenkov V.I., Kucherov A.S., Yakishik A.A.
Off-line long-life unservice close gas organic fuel-powered turbine
Arbekov A.N.
Problems development of nuclear electric propulsion
Belogurov A.I., Kolbaya T.C., Rachuk V.S.
Way of increase in efficiency of cycle gas turbine units
1 1.
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.
Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control
Shorikov A.F., Kalev V.I.
Mathematical modelling of the working process of a hot gas pressure feed system
Salich V.L.
Experimental investigation of a small-sized centrifugal compressor for a closed-brayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Development liquid roket engine on component fuel liquefied natural gas and oxygen for reusable space launching systems
Efimochkin A.F., Khrisanfov S.P., Golubyatnik V.V., Kafarena P.V., Yeliseyev A.V.
Rotor in gas bearings dynamics experiment-calculated investigation
Temis Y.M., Temis M.Y., Egorov A.M., Gavrilov V.V., Ogorodov V.N.
Project of 30 000 h.p. power gas turbine
Zrelov V.A.
1 - 67 of 67 Items

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