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Simulating the process of retargeting of optoelectronic Earth observation spacecraft during object shooting
Kurenkov V.I., Pupkov E.A., Kucherov A.S.
Optimization of operation mode and design parameters of a finely-dispersed metallic liquid-alloy generator
Egorychev V.S., Ryazanov A.I., Khaimovich A.I.
Forecasting the parameters of performance monitoring of complex technical systems
Zolotov A.A., Rodchenko V.V., Gusev E.V., Karyagin I.A.
Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing
Parovay E.F.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Optimization of the workflow of multistage axial turbines with platforms
Matveev V.N., Baturin O.V., Popov G.M., Goryachkin E.S.
Modelling of an ejector for turbine aeroengines for application in performance synthesis tools
Georgi J., Staudacher S., Falaleev S.V.
Engines for domestic drones: past, present and future
Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.
Problems of ultralow power turbine design in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Two-dimentional axial rotor compressor off-design performance prediction model with the use of simulation methods and tools
Mikhailova A.B., Akhmedzyanov D.A., Akhmetov Y.M., Mikhailov A.Y.
Refinement of operable state recovery algorithms for “AIST” small satellites on the basis of telemetric information
Volgin S.S., Salmin V.V., Tkachenko S.I., Tkachenko I.S., Ivanushkin M.A.
Validation of CFD-models of gas turbine engine uncooled turbines
Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.
analysis of demands on the evolution and development of new domestic booster population
1 1., 1 1.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
Micro gas turbine engine imitation model
Kuznetsov A.V., Makaryants G.M.
Experimental research of shaft sealing with elastic element made of MR material
Zhizhkin A.M., Zrelov V.A., Zrelov V.V.
Investigation of extreme opportunities of stand supporting systems
Samsonov V.N., Kozyreva M.S., Cherevan A.A.
Design and technical characteristics of transport airplane for arctic exploration
Kuprikov N.V., Dolgov O.S., Kuprikov M.Y., Ivanov B.V.
Measuring system for investigation flow rate and fluid pressure features of control devices for the position hydrodrive
Poleshkin M.S., Sidorenko V.S.
Test rig for a hydraulic drive under switched inertance control
Shorin V.P., Sverbilov V.Y., Gimadiev A.G., Greshniakov P.I., Ilyukhin V.N., Stadnik D.M.
Isotopy of spacecraft compartment hull shapes
Belyakov A.A., Shulepov A.I.
Planning a factorial experiment for testing a single-stage ultralow power turbine
Grigoryev V.A., Radko V.M., Kalabukhov D.S.
Robust research of the fuzzy logic controllers using a fuel flow control loop of the gas-turbine engine as an example
Chicherova E.V.
Analysis of landing process dynamics for different reentry vehicle landing device support schemes
Borzykh S.V., Voronin V.V., Shchiblev Y.N.
Development of improved performance electromagnetic valve for liquid rocket engine
Igolkin A.A., Chubenko T.A., Maksimov A.D.
Quality forecasting solder joint electronic components
Shumskikh I.Y.
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.
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.
Analysis of the effectiveness of predictive models of quality parameters of the chips
Tyulevin S.V., Arhipov A.I., Piganov M.N., Elizarov S.V.
Operational testing of thermoplastic reinforced blades
Krutsilo V.G., Krotinov N.B.
1 - 30 of 30 Items

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