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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.
Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft
Kurenkov V.I., Kucherov A.S., Yakishik A.A.
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.
Analysis of schemes and methods of hydrodynamic cleaning of hydro-fuel system units
Sanchugov V.I., Reshetov V.M.
Computational and experimental research of exhaust gas treatment systems
Galevko V.V., Rakhmatov R.I.
Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet
Ivanov A.I., Borisov V.A.
Discrete phase converters moving elements rotating units power units
Danilin A.I., Grechishnikov V.M.
Development of load – bearing frames of space telescopes with invariable dimensions adaptive to temperature gradients
1 1., 1 1., 1 1., 1 1.
On the efficiency of using the Navier-Stokes approximation in thermogasdynamic calculation of low-thrust liquid-propellant rocket engines at low Reynolds numbers
Maksimov A.D., Shustov S.A.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
Doppler method for measuring fluctuations of elements rotationg parts power
Danilin A.I., Gretskov A.A.
Primary converters for the implementation of Doppler method for measuring blade oscillation power unit
Danilin A.I., Gretskov A.A.
Assessment of technicaland economical efficiency of developing carrier rockets with first-stage reusable units
1 1., 1 1.
An experimental study of the influence of valve drive type on the dynamic loading and service life of valve seals of units
Kondrashov Y.I., Ermilova E.N., Vidyaskina A.N.
Analysis of information characteristics of a dynamic displacement doppler transducer signal
Danilin A.I., Gretskov A.A.
Resources management and planning of product realization in ERP “1C” and MES “Sprut” (ERP: Enterprise Resource Planning; MES: Manufacturing Execution System)
Abramova I., Lisitsin M.S., Abramov D.A.
System-simulator load the steering organs
Aliluev A.V.
Special methodic of economics indexes determination of turbocompressor stations for central air supply of industrial factories
1 1., 1 1.
Method for determination of optimal geometrical parameters of a unit cell of X-shaped truss cores
Mousavi Safavi S.M.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Crystal lattice identification on the basis of assessing unit cell parameters
Kirsh D.V.
Rotor in gas bearings dynamics experiment-calculated investigation
Temis Y.M., Temis M.Y., Egorov A.M., Gavrilov V.V., Ogorodov V.N.
Structure and mehanpichesky properties of the shovel 1 steps of the rotor of turbine GTE-45-3 after the long operating time and regeneration
1 1., 1 1., 1 1.
Design build process for the accuracy of eligibility
Grechnikov F.V., Tlustenko S.F.
Experimental research of internal heat transfer in the vortex heat generator
Zhornik M.N., Piralishvili S.A., Mogileva K.A.
Mathematical model and peculiarities of operating mobile robots with hybrid drives
Ilyukhin Y.V., Tatarintseva A.V.
Allan variance-based assessment of basic characteristics of a strapdown inertial sensing unit
Kutovoy D.A., Sitnikov P.V., Fedotov A.A., Yakimov V.L.
Increasing efficiency of pressurization of the rocket tanks in the flight
1 1., 1 1.
Research of the postoperational condition of the restored compressor shovels of GTD gas-transfer of the units which have fulfilled the appointed resource
Tarasenko Y.P., Tsareva I.N., Krivina L.A.
Optimization of strength characteristics of lighting devices aircraft by construction of virtual models
Abulkhanov S.R., Goryainov D.S., Skuratov D.L.
Determination of mass-power propertions for parametric range of launch vehicle modifications
Baranov D.A., Yelenev V.D.
Increasing efficiency of pressurization of the rocket tanks in the flight
Biryuk V.V., Kapitonov V.A., Smorodin A.V.
Refining methods of vibration diagnostics of wear of turbo-prop engine differential speed reduction unit gear teeth
Avramenko A.A., Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.
Differential bynary optical-mechanical sensors for automated management and control systems
Korban D.V.
Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection
Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.
Development of turbopump unit design for hydrogen liquid-propellant rocket engines without generators developed at the design bureau of chemical automation
Dmitrenko A.I., Ivanov A.V., Rachuk V.S.
Identification of a gas turbine engine mathematical model by the ressults of testing
Botchkaryov S.K., Dmitriyev A.Y.
Inertial measuring units for future-generation aerospace products: fault-tolerance
Vodicheva L.V., Bel'skiy L.N., Parysheva Y.V., Lystsov A.A.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.
Models for choosing admission campaign strategy of university in the contemporary context
Simanchuk N.V.
1 - 40 of 40 Items

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