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Assessment of the possibility of shortening the landing distance of maneuverable aircraft
Strelets M.Y., Tarasov A.Z., Grishin I.A.
The relevance of introducing a requirements management system in the production process of the aircraft engine construction industry
Malinovskiy I.M., Starodumov A.V., Myagkov K.A., Yusipov B.K.
Methodology of designing a space transport system including a “DM” chemical upper stage and an electric rocket transport module
Russkikh A.S., Salmin V.V.
Analysis and improvement of characteristics of power supply systems for the small space vehicle of the AIST-2 type
Mordanov M.R., Safronov S.L.
Application of decision support technology at various stages of the life cycle of space facilities in assembly with the information system of technical condition and reliability
Avtamonov P.N., Bakhmut A.D., Krylov A.V., Okhtilev M.Y., Okhtilev P.A., Sokolov B.V.
The analyze of work of throttle cooling system’s microheat exchanger, wich uses nitrogen with nearly critical parameters
1 1., 1 1., 1 1., 1 1.
Methodology of delivering space parts, tools and accessories to a near Earth orbital station on the basis of the reliability factor
Zheleznov I.V., Uperchuk R.A., Eroshenko V.K.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants
Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Seal designing as element of aircraft engine systems and engine units
Vinogradov A.S.
Investigation of the dynamic characteristics of the pneumatic-mechanical drive of the installation movements of machine mechanisms
Prikhodko S.P., Sidorenko V.S., Korotych D.A.
Reduction of angular velocities of AIST-2D spacecraft using a system of kinetic moment dumping
Shipov M.G.
Models and methods of corporation management in case of inter-corporation interaction
Geraskin M.I.
Results of primary operation of NK-37 engine low emission combustion system
Bantikov D.Y., Yeliseev Y.S., Lavrov V.N., Pchelyakov A.A., Fedorchenko D.G., Tsybizov Y.I.
Method of controllung the angular position of IO ASD relative to the system of coordinates of a gyrostabilized platform
Degtyarev M.S.
Model of knowledge in the expert system of aid to the crew
Vorontsov A.A.
Onboard digital computer systems of the «Malachite» family for extreme conditions
Antimirov V.M., Umansky A.B., Shalimov L.N.
Experimental analysis of instability and self-oscillations in an electrohydraulic servo drive
Petrov P.V., Sunarchin R.A., Mashkov M.A., Krivosheev N.S.
Multi-position control of movements of large-sized structural elements during static loading using a laser tracker
Sazonnikova N.A., Uklein R.V.
Cycle air heating system of gas pumping unit NEVA-25NK
1 1., 1 1., 1 1., 1 1.
Verification of aero-engine numerical rotor models based on virtual static structural and modal tests
Shaposhnikov K.V., Degtyarev S.A., Leontiev M.K., Anisimov S.V.
Development of an experimental plant and a numerical model of an axial magnetic rotor suspension
Benedyuk M.A., Lomachev A.O., Badykov R.R., Bezborodova K.V., Yurtaev A.A.
Control over the deployment of an orbital tether system of great length
Wang C., Zabolotnov Y.M.
Optimization of trajectory motion of the first stage of an aerospace system
Khramov A.A.
Approximate models of air transport queueing systems with partial mutual assistance between service channels
Romanenko V.A.
Dynamics of the hydromechanical system of a production machine with an adaptive tool-feeding drive
Sidorenko V.S., Poleshkin M.S., Rakulenko S.V.
Methodological approaches to the creation and functioning of serial robotic production of small satellites
Tkachenko I.S.
Main approaches and features of the design of aircraft hydro-mechanical control systems
Petrov P.V., Tselischev V.A., Kuderko D.A.
Analisys of the influence of radial displacement of a particle on the parameters of an eddy-current probe
Gudkov S.A., Kudryavtsev I.A.
Analysis estimation of pulse jet engine operation in detonation mode
Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.
Development of classifier of plane’s parts for the solution of taks of automated CNC programs prepairing for CNC machines
Gismetulin A.R., Sergeev O.S.
Problems of testing and operation of hydraulic power transfer units
Polyakov N.A., Frolov G.K., Tselischev V.A., Tselischev D.V.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.
Choice of parameters of an engineering production preparation system
,
Selection of design parameters of a spacecraft electric propulsion engine ensuring the geostationary orbit raising mission
Kolesov A.V., Salmin V.V.
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.
Scalable distributed systems of competitive interacting processes and their optimality
1 1.
Experimental studies of the components of high-frequency ion engine RD0310
Kazbanov A.A., Dronov P.A., Spivak O.O., Derkachev A.B.
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.
Problem of optimization of the number of processors in distributed processing
Pavlov P.A.
Internal combustion engine some cooling system components detailed calculation
Kolomin I.V., Ajukov A.A., Birjuk V.V.
Problems of modern aircraft maintenance
Kovalev M.A., Poddubniy I.V.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Rotor-pendulum self-synchronization of parametrical vibration generators on an isotropic elastic foundation
Koshelev A.V., Dentsov N.N.
Peculiarities of using additional low-power energy sources in the power supply system of small spacecraft
Kargu D.L., Beznyakov A.M., Nemirov A.V., Radionov N.V., Chudnovsky Y.A.
Morphological characteristics of the intermetallic phase of heat resisting nickel alloys
Kirikov S.V., Perevezentsev V.N., Tarasenko Y.P.
Analysis of motion stability of a deployed space tether system with an atmospheric probe
Zhe D., Zabolotnov Y.M., Changqing W.
Analysis of the influence of the scheme of flight of the stage with a reactive recovry system on the energy characteristics of a two-stage medium class launch vehicle
Kuznetsov U.L., Ukraintsev D.S.
Nominal motion control program in a supersonic carrier aircraft
Balakin V.L., Potapov V.I.
Development of a multiparameter model of an optimum coherent system of incentives for workers of aircraft construction enterpricses
Ivanov D.Y.
Vortex cleaning of fuel tank pressurant gas
Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.
Choosing the law of distributing request input flow in the modeling of a trade enterprise queuing system
Duplyakin V.M., Knyazheva Y.V.
Synthesis of dynamic modes of attitude motion of spacecraft with solid propellant rocket engine
Balakin V.L., Doroshin A.V., Krikunov M.M.
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.
Classification of models of basic links in the air transport sector in the context of the process of macrologistic system formation and development
Pakhomov A.A.
Analysis and ballistic design of a medium-caliber system with an attached camera of accelerating
Safronov A.I., Azovsky V.M., Zorkin V.A., Chirkunova N.V.
The machine and methods of tribotehnical tests of materials
Ibatullin I.D., Zhuravlev A.N., Utjankin A.V., Galljamov A.R., Neyaglova R.R.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
Kick-stage control by navigational data of satellite navigation system
1 1.
Tooling system of express assessment of explosive military equipment objects after hitling effects
1 1., 1 1.
Extrapolation of conditions of an information measuring and control system with the iterative algorithm of operation
Zelensky V.A.
Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
The integrated information model architecture for working out, manufacture and operation GTE together with its system of automatic control, the control and diagnostics
Kulikov G.G., Rizvanov K.A., Denisova S.S.
Development of the finite element model of vibroacoustical characteristics of pipe system
Mironova T.B., Prokofiev A.B., Shahmatov E.V.
Computer-aided-design system for calculating adsorption thermodynamic characteristics
Zelenko L.S., Varfolomeyeva V.V., Kuznetsov V.Y., Fed’kayev A.V., Terentyev A.V., Buryak A.K.
Verifying models of mechatronic systems «man-centrifuge» for ground and space usage on the basis of set theory
Anshakov G.P., Akulov V.A., Balakin V.L.
Multilevel system of Earth operational hyperspectral monitoring
Anshakov G.P., Egorov A.S., Raschupkin A.V., Skirmunt V.K.
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
Mathematical model of the “tank – nozzle” cooling system
Shalay V.V., Shcherban K.V.
Methods of validation of the ballistic structure of space surveillance system orbital segment
Fadin I.A., Yanov S.V., Samokhvalov O.A.
Preliminary tests of tank with cryogenic charging for onboard throttle system of cooling
Dovgjallo A.I., Sarmin D.V., Uglanov D.A.
Using of resonance oscillations in intake system for a car noise tuning
Starobinski R.N., Mescheriakova M.A., Nazarov A.G., Sokolov A.V.
Dynamics of a dual-mass resonant vibration screen in a first approximation
Dentsov N.N., Koshelev A.V.
Investigation of the thermal regime of microsatellite optoelectronic telescopic complex under operating conditions
Tsaplin S.V., Bolychev S.A.
Analysis of heat transfer in a helically coiled cooler of a mechatronic sample conditioning system
Gimadiev A.G., Utkin A.V.
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.
Modeling orbital tether system deployment with limitations on the deployment speed
Ishkov S.A., Filippov G.A., Xiaoye X.
Study of characteristics of the vortex throttling valve for the sysytem of water sample conditioning
Gimadiev A.G., Utkin A.V.
Computer-aided design of aircraft gas turbine engines and selection of materials for their main parts
Akhmedzyanov D.A., Kishalov A.E., Markina K.V.
Method of gas turbine malfunction diagnostics using hybrid intellectual systems
Antropov P.G., Dolinina O.N., Shvarts A.Y.
Models of discrete multycriterion optimization for hierarchical systems of corporations
Geraskin M.I.
Measurability of knowledge and competences in studying humanities
Ryabinova E.N., Titov B.A., Pavlova I.O.
The formation of the contoured surface roughness level of optical purity by using a CNC machine
Abulkhanov S.R., Sazonov M.B.
Dynamic process modeling of aircraft engine control system
Blyumin K.V.
Calculating maximum amplitude in an oscillatory system with many-valued perturbation
Lepilov A.N.
Using statistical Markov models for the analysis of electromagnetic compatibility of autonomous electric installations
Kubarkov Y.P., Goldshtein V.G., Inahodova L.M.
Task-oriented systems in the problems of spacecrafts designing
1 1., 1 1., 1 1., 1 1.
Choosing the structure of power-supply systems for low-orbit space vehicles
1 1., 1 1., 1 1., 1 1.
History of small space vehicle progress and development at Plesetsk cosmodrome. Current problems of further development
Korotkov V.V., Vinogradov A.V.
Hydrodynamic rinsing of hydrofuel system’ unflowing units
1 1.
Research of a seal work as an element of the air engine support
Vinogradov A.S., Rempel A.P.
Action of random vibration on non-linear dry friction damping system
Ulanov A.M., Parovay F.V.
Software for investigating the process of catalytical masking layer formation
Kolpakov V.A., Bonyachuk A.A.
Designing of control and expulsion equipment for the pitot-static system of passenger airplanes
Zotin N.A., Lisman E.P.
Optimizing the process of changing spacecraft orbital parameters by using a spinning electrodynamic tether sytem
Lu H., Wang C., Zabolotnov Y.M.
Disturbed motion of the hypersonic first stage of an aerospace system in climb
Balakin V.L., Krikunov M.M.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
Forming professional-significant qualities of students-future engineers in terms of modular-rating technology of education
Rakhimova J.I.
Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation
Tsaplin S.V., Bolychev S.A.
Development of a procedure for the synthesis of a micro gas turbine engine neural controller with account for fuel consumption constraints
Kuznetsov A.V., Makaryants G.M.
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