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Exploratory analysis of hybrid polymer metal-composite structures
Khaliulin V.I., Petrov P.A., Kostin V.A., Levshonkov N.V.
Determining aerodynamic characteristics of small unmanned aerial vehicles involving flight experiment
Lukyanov O.E., Zolotov D.V., Espinosa Barsenas O., Komarov V.A.
Optimization of operation mode and design parameters of a finely-dispersed metallic liquid-alloy generator
Egorychev V.S., Ryazanov A.I., Khaimovich A.I.
Selection of design parameters of a spacecraft electric propulsion engine ensuring the geostationary orbit raising mission
Kolesov A.V., Salmin V.V.
Justification of geometric parameters of the engine air particle separator
Gishvarov A.S., Rakhimov A.R.
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.
The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters
Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.
Optimization of the parameters of a ground speed meter of low-flying aircraft based on the application of the theory of optimal filtration
Ivanov M.E., Yezerskiy V.V.
Improving the efficiency of aviation turbofan engines by using an intercooler and a recuperative heat exchanger
Omar H., Kuz'michev V.S., Tkachenko A.Y.
Heat engine cycle limitations imposed by fuel properties
Mikheyenkov E.L.
The analysis of real thermodynamic cycle of bypass engine with mixing
Medvedev V.V.
Procedure of accomodation of earth remote sansing satellite external devices with regard for the satellite target operation
Akhmetov R.N., Shilov L.B., Kurenkov V.I., Yakischik A.A.
Nondestructive quality control of mechanical-rubber goods vulcanization
Astapov V., Misiyevitch S.K.
Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine
Kvetkin A.A., Kolesov A.V.
Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD
Ryzhkov V.V., Morozov I.I.
Identification of a gas turbine engine mathematical model by the ressults of testing
Botchkaryov S.K., Dmitriyev A.Y.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Study of uncertainty of measuring geometrical parameters of gas turbine engine compressor blade profiles
Pechenin V.A., Bolotov M.V., Ruzanov N.V., Yanyukina M.V.
Motion of an upper stage rocket with a toroidal tank around the mass center in parameters of Cayley-Klein
Alekseev A.V., Krasnikov V.S.
Calculation of sleeve-shaped filter elements made of the MR material
Zhizhkin A.M., Lazutkin G.V., Volkova T.V.
Assessing reduction gear mass in the problem of optimizing parameters of the working process of a turboprop engine at the initial design stage
Grigoryev V.A., Zagrebelnyi A.O., Prokaev A.S., Kuznetsov S.P.
Improving the efficiency of gas turbines by regenerating heat
Kulagin V.V., Sokolov M.A.
Problem formulation of bypass engine parameters optimization with a preselected gas generator
Kuzmichev V.S., Kulagin V.V., Tkachenko A.Y., Krupenich I.N., Rybakov V.N.
Simulation of thermal field of fluid flow in the presence of parametric disturbances
1 1.
The detecting improvement by laser surface sounding
1 1.
Parameter measurement quality control in automated testing of series gas turbine engines
Botchkaryov S.K.
Preliminary study of principles of effective efficiency change of turboshaft engines of various schemes with heat recovery and intermediate cooling of working medium
Sokolov M.A., Kuzmichev V.S., Kulagin V.V., Krupenich I.N., Tkachenko A.Y.
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.
Procedure of comparative assessment of the efficiency of Earth remote sensing satellites with different optoelectronic telescopic complexes
Stratilatova N.N., Kurenkov V.I., Kucherov A.S., Egorov A.S.
Quality forecasting solder joint electronic components
Shumskikh I.Y.
Development of the technology of diagnostics of turbo-jet aviation engines by a filtering element with a diagnostic layer
Drokov V.V., Drokov V.G., Muryshenko V.V., Mukhutdinov F.I., Khaliullin V.F.
Research of the influence of the diamond burnishing process parameters on the surface roughness of a steel 15CR12NI2MOVWANB-S workpiece when using an indenter made of natural diamond
Shvetsov A.N., Skuratov D.L.
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.
Choice of parameters of an engineering production preparation system
,
The determination of the efficient parameters of surface strenghtening the thin-walled and the small-hard parts of gas turbine engines based on deformation tolerance
1 1., 1 1.
Procedure of coordinating interaction between a bank and a small enterprise
Bogatyryov V.D., Bondarchuk K.L.
Investigation of laser beam influence on aircrafts surface condition estimation efficiency
Sazonnikova N.A.
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.
Metodological basis of the development of a problem-oriented system for selecting design parameters of space vehicles
Stratilatov N.R., Kurenkov V.I., Kucherov A.S., Yakishik A.A.
Forecasting technique of semiconductor diodes quality indicators
Kozlova I.N., Tyulevin S.V., Tokareva A.V.
Development of methods of carrying out experimental research of measurement errors for sets of geometrical parameters on NC equipment as in the case of a turbine disk
Bolotov M.A., Alexeev V.P., Pronichev N.D.
Check and prediction of gas-turbine engine’s technical state
Zotin N.A.
Test verification of flow stabilizer calculated parameters provided flow stabilization of propellant in wide range of input parameters
Beshenev Y.A., Volkov A.V., Kazankin F.A.
Research and optimization of parameters of a system controlling the process of tube inside surface coating
Skvortsov B.V., Zaretskaya M.I., Kurylyova P.A.
Optoelectronic device for the control of hydrocarbon fuel cavitation treatment
1 1.
Multichannel television method of object geometrical parameter remote measurement
Zhiganov I.Y.
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.
Protocols of stitching image strips formed by optoelectronic converters and their application
Kuznetsov P.K., Martem’ianov B.V., Miatov G.N., Yudakov A.A.
Determination of relative position and orientation of nanosatellites by video image analysis
Simakov S.P., Ustyugov E.V.
Calculation of parameters of the Deal–Grove model for the oxidation of silicon
Aizikovich A.A., Demakov Y.P.
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.
Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine
Ishkov S.A., Filippov G.A.
Estimate of key parameters of a gas turbine engines with application of the modelling procedure of the equilibrium state of homogeneous mixture of hydrocarbon fuel combustion products
Boldyrev O.I., Gorynov I.M.
Determining the interrelation between detonation characteristics indicators and electrodynamic parameters of hydrocarbon fuels on the basis of statistical modelling of componental structure
1 1., 1 1., 1 1.
The community of the ideal and complex cycles of the gas-turbine installations
Ivanov V.A.
Limit values of the Brayton cycle with the use of reduced fuel characteristics
Mikheenkov E.L., Nekrasova S.O.
Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
Ananenko V.M., Golyakov A.D., Kalabin P.V.
Diagnostics of state gas-fluid of flows in the field of cross vibration
Limanova N.I., Levkin U.S.
Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines
Ryzhkov V.V., Verjasov Y.N., Galperin R.N., Gulyaev Y.I., Ivashin Y.S.
Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit
Ishkov S.A.
Formation of a method of choosing rational values of ultralow power turbine parameters in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Thin coating for printed circuit boards in industrial production technology of modern equipment
Erendeev J.P.
Crystal lattice identification on the basis of assessing unit cell parameters
Kirsh D.V.
Diagnostics of constructions' materials in the early stages of fatigue failure and estimation of the stress-strain condition of constructions’ material by methods of non-destructive testing
Mishakin V.V., Danilova N.V., Kurashkin K.V., Klyushnikov V.A., Gonchar A.V.
Dynamic analysis and optimization of turbojet engine nozzle control mechanism
Creation of the database for electrochemical processing with the purpose of optimization of process of the choice of electrolit
Smelov V.G., Shitarev I.L., Smirnov G.V.
Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers
Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.
Optimizing the process of changing spacecraft orbital parameters by using a spinning electrodynamic tether sytem
Lu H., Wang C., Zabolotnov Y.M.
Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle
Grigoriev V.A., Kuznetsov S.P.
Mathematical model of surface layer formation during hydroabrasive jet machining
Meshcheryakov A.V., Shulepov A.P.
Planning a factorial experiment for testing a single-stage ultralow power turbine
Grigoryev V.A., Radko V.M., Kalabukhov D.S.
Bypass as an attribute of unmanned spacecraft operability in anomalous flight situations
Akhmetov R.N., Makarov V.P., Sollogub A.V.
Peculiarities of laser welding of thin parts of aerospace equipment
Smelov V.G., Sotov A.V., L’vov M.V.
Study of processes production scheduling in multiproduct manufactures
Larin S.N., Timirzyanov V.V.
The influence of grain orientation and structure parameters on the limiting formability of skin sheets during stretch-wrap forming
Aryshensky V.Y., Grechnikova A.F., Yerisov Y.A.
Design of sheet and strip rolling modes for drawing articles with minimal earing
Grechnikov F.V., Erisov Y.A., Aryshensky E.V.
Some results of analysing theoretical cutting models
Vinokurov M.V., Druzhin A.N.
Ways 3D parametrization TJ blades for use CAD/CAM/CAE packages
Smelov V.G., Shitarev I.L.
Spacecraft preset orbital parameters control by means of thrusters
Salmin V.V., Volotsuev V.V., Shikhanov S.V.
Method for determination of optimal geometrical parameters of a unit cell of X-shaped truss cores
Mousavi Safavi S.M.
Design procedure of fundamental parameters of the direct-flow detonation pulsing engine
Porshnev V.A.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Problems of ultralow power turbine design in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Gas turbine engine designing on the basis of a unified gas generator
Rybakov V.N.
Choice of design parameters of universal platforms of small space vehicles
Volotsuev V.V., Tkachenko I.S., Safronov S.L.
Optimization of thermomechanical parameters of high speed forging of titanium alloys
Khaimovich A.I., Mikheyev V.A.
Mathematical modelling and parametric research of flow of the twisted turbulent single-component stream of the propulsive mass in the trance- and supersonic areas of Laval nozzles
1 1., 1 1.
Structural model of individual forecasting of space radioelectronic equipment parameters
Tyulevin S.V., Piganov M.N.
Single-coil eddy-current transducers for measuring mechanical parameters
Borovik S.Y., Sekisov Y.N.
Analytical determination of motion parameters of the center of mass of an uncooperative orbiter on the basis of measurement information provided by on-board systems of a space robot in a coplanar orbit
Ananenko V.M., Golyakov A.D., Kalabin P.V.
Development of the criteria of analyzing the stress-strain state of gas turbine engine parts in the elastoplastic range
Bukaty A.S., Bukaty S.A.
Experimental investigation of the efficiency of laserelectronic systems for aircraft surface remote sounding
Sazonnikova N.A.
Analysis of technological parameters of production (methodological aspect)
Sosnina T.N.
Research of gas turbine engine operation in dust-filled atmosphere
Abdullin B.R., Akmaletdinov R.G., Goumerov K.S., Nigmatullin R.R.
Optimization features of the working process parameters of bypass engine on the basis of given gas generator
Rybakov V.N.
Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine
Kuzmichev V.S., Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Kulagin V.V.
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