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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.
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.
Efficiency of technical workings out in batch production GTE
Aleksentsev E.I., Shitarev I.L., Kurbatov V.P., Gritsenko E.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.
Spacecraft preset orbital parameters control by means of thrusters
Salmin V.V., Volotsuev V.V., Shikhanov S.V.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Empirical metod of predicting aviation piston engine noise
Moshkov P.A.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
Mathematical model and peculiarities of operating mobile robots with hybrid drives
Ilyukhin Y.V., Tatarintseva A.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 determination of the thermoacoustic generator aspect from electrodynamic unit features by the parametric-studies
Vorotnikov G.V., Kruchkov A.N., Zynovyev E.A.
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.
Parametric analysis of thermoacoustic travelling-wave engine operation with external heat application
Dovgyallo A.I., Zynovyev Y.A., Vorotnikov G.V.
The story of invention and development of supercharge units of internal combustion engines
1 1., 1 1., 1 1.
Engines for domestic drones: past, present and future
Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.
The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage
Ivanov V.P., Partola I.S.
1 - 18 of 18 Items

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