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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.
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.
Identification of a gas turbine engine mathematical model by the ressults of testing
Botchkaryov S.K., Dmitriyev A.Y.
Planning a factorial experiment for testing a single-stage ultralow power turbine
Grigoryev V.A., Radko V.M., Kalabukhov D.S.
Nondestructive quality control of mechanical-rubber goods vulcanization
Astapov V., Misiyevitch S.K.
Selection of design parameters of a spacecraft electric propulsion engine ensuring the geostationary orbit raising mission
Kolesov A.V., Salmin V.V.
The analysis of real thermodynamic cycle of bypass engine with mixing
Medvedev V.V.
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.
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.
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Determination of relative position and orientation of nanosatellites by video image analysis
Simakov S.P., Ustyugov E.V.
Analysis of technological parameters of production (methodological aspect)
Sosnina T.N.
Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine
Ishkov S.A., Filippov G.A.
Reduction of circumferential variation in the final stage of IPC
Popov G.M., Mamedov A.C., Smirnova Y.D.
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.
Dependence between microscopic characteristics of the material MR and parameters of press forming
1 1., 1 1.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
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.
Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit
Ishkov S.A.
Optimization of fatique validation cost for redesigned transport aircraft
Kleptsov V.I.
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.
Design of sheet and strip rolling modes for drawing articles with minimal earing
Grechnikov F.V., Erisov Y.A., Aryshensky E.V.
Features of designing gas turbine of complex cycle GT24
1 1.
Procedure of coordinating interaction between a bank and a small enterprise
Bogatyryov V.D., Bondarchuk K.L.
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.
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.
Selection of a nanosatellite group separation program for cluster launching from the «Soyuz» launch vehicle orbiter
Avaryaskin D.P., Shcherbakov M.S.
Calculation of sleeve-shaped filter elements made of the MR material
Zhizhkin A.M., Lazutkin G.V., Volkova T.V.
Gas turbine engine designing on the basis of a unified gas generator
Rybakov V.N.
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.
Heat exchange parameters of units and pipelines of the aircraft hydraulic system
Nikolayev V.N.
Estimation the factors, make the greatest influence on reliability parametres of a GTD disk with a glance sudden failures
Belousov A.I., Gritsin A.V.
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.
Development of the method of calculation and design stand installation for testingmodes wet cleaning duct GTE
Silaev B.M., Malcev E.N.
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.
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.
Optimization features of the working process parameters of bypass engine on the basis of given 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.
Experimental research and selection of design parameters of the onboard microaccelerations state and compensation monitoring equipment on the low-orbit space microgravitational platform
1 1.
Multichannel television method of object geometrical parameter remote measurement
Zhiganov I.Y.
Limit values of the Brayton cycle with the use of reduced fuel characteristics
Mikheenkov E.L., Nekrasova S.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.
Heat engine cycle limitations imposed by fuel properties
Mikheyenkov E.L.
Mathematical model of surface layer formation during hydroabrasive jet machining
Meshcheryakov A.V., Shulepov A.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.
Improving the efficiency of gas turbines by regenerating heat
Kulagin V.V., Sokolov M.A.
Development of yield criteria for the calculation of forming high-textured anisotropic blanks
Grechnikov F.V., Yerisov Y.A.
Choice of parameters of an engineering production preparation system
,
The community of the ideal and complex cycles of the gas-turbine installations
Ivanov V.A.
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.
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.
Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle
Grigoriev V.A., Kuznetsov S.P.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
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.
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.
Selection of optimal configuration and workflow parameters of autonomous micro gas turbine plant
Baturin O.V., Smirnova Y.D.
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.
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.
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.
Single-coil eddy-current transducers for measuring mechanical parameters
Borovik S.Y., Sekisov Y.N.
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.
Design procedure of fundamental parameters of the direct-flow detonation pulsing engine
Porshnev V.A.
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.
Calculation of parameters of the Deal–Grove model for the oxidation of silicon
Aizikovich A.A., Demakov Y.P.
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.
The analytical methods modelling dynamical characteristic o put out pulsations of pneumatic and liquid in pipeline
Yudin P.E., Limanova N.I., Limanov I.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.
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.
Method for determination of optimal geometrical parameters of a unit cell of X-shaped truss cores
Mousavi Safavi S.M.
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.
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.
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.
Check and prediction of gas-turbine engine’s technical state
Zotin N.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.
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.
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