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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.
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.
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.
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.
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.
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.
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.
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
,
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.
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.
Choice of mission trajectory plans and conceptual design of electrical propulsion module for launching payloads into circumterrestrial orbits
Salmin V.V., Kvetkin A.A., Russkikh A.S.
Control over maintaining accuracy of integrity of reference surfaces of spacecraft components in their joint functioning at various stages of design
Yelenev V.D., Schuplyak Y.P.
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.
Joint work of units and characteristics of elements gas the equipment for the engine of internal combustion with spark ignition
Shishkov V.A., Lesnih U.I.
Modeling and experimental research of the multi-level drawing and geometric training system
Ivashchenko V.I.
Application of additive technology of selective laser melting (SLM) in designing a low emission combustion chamber of a gas turbine plant
Yeliseev Y.S., Fedorchenko D.G., Golanov S.P., Tsibisov Y.I., Tyulkin D.D., Vorotyntsev I.E., Ivchenko A.V.
Use of phase portraits of hydro-mechanical units for diagnosing aircraft hydraulic systems
Gareyev A.M., Popelnyuk I.A.
Locally optimal control of space tug motion between the libration points of the Earth-Moon system
Starinova O.L., Fain M.K.
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
High resolution equipment for the future spacecraft «Resource-PM»
Baklanov A.I., Blinov V.D., Gorbunov I.A., Zabiyakin A.S., Malakhov I.A.
System-mathematical simulation of engine air hydraulic power supply
Goryunova N.R., Goryunov A.A.
Conversion of gas turbine engine oil system
Boev A.A., Grishanov O.A.
Experimental research of internal heat transfer in the vortex heat generator
Zhornik M.N., Piralishvili S.A., Mogileva K.A.
Development of a solar battery orientation robot system for small spacecraft
Beznyakov A.M., Vlasov V.A., Malenin E.N.
Analysis of the thermal state of aircraft engine supports
Vinogradov A.S., Badykov R.R., Fedorchenko D.G.
Control over the financial and economic activity of a joint-stock company carried out by the board of directors
Bogatyryov V.D., Khakimova A.K.
Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation
Shuplyak Y.P., Sorokoletov V.I.
Engineering education on level learning
Shehonin A.A., Tarlykov V.A.
Simulation modeling of stock markets
Steryakov A.A.
Basic approaches and requirements to the formation of polyplatform integrated automated system of aircraft life cycle support based on the product electronic definition
Nazarov V.V., Shabalkin D.Y., Polyanskov Y.V.
Stabilization of steady motions of a single rotor gyrostat with a cavity filled with a liquid of high viscosity
Alekseev A.V., Bezglasny S.P., Krasnikov V.S.
Problems of unmanned spacecraft reengineering in abnormal flight situations and their knowledge-based solutions
Akhmetov R.N., Makarov V.P., Sollogub A.V.
Improvement of the resolution on the basis of use of spatial filters
Savelyev D.A., Khonina S.N.
Ways of the development of the radar space systems of the remote sensing of the Earth
1 1.
Development of information support for the spacecraft controlalgorithm design process
1 1., 1 1.
Features of adaptation of first-year students of SSAU in the application of computer technologies of training
1 1., 1 1.
Methodology complex of hardware-in-the-loop functional modelling of gas turbines and its systems
1 1., 1 1., 1 1., 1 1., 1 1.
Analysis and ballistics project the gun tube system with a joined drive on chamber
Safronov A.I., Potapenko V.V.
An algorithm for extracting invisible information from scanned polygraphic products
Glumov N.I., Mitekin V.A., Sergeev A.V., Fedoseev V.A.
Modelling changes of condition of aircraft hydraulic system working fluid
Gareyev A.M.
Experimental simulation of registration of outer space objects
Baryshev Y.Y., Syomkin N.D., Voronov K.Y.
Design of control moment gyro electric drive with strict requirements on ensuring desired rotational velocities
Polozhentcev D.S., Davidov A.A., Shipov M.G., Kazakov E.P., Malykh B.I.
Fuzzy-controller simulation model as a tool of optimization of a limited availability ground handling system at a hub airport
Romanenko V.A.
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
Research of the possibility of thermal conditions LREST using an infrared thermal imaging system
Ryzhkov V.V., Silyutin M.V.
Analysis and ballistics design of a laboratory installation system a small calibre with a joined drive on chambers
Safronov A.I., Zorkin V.A., Potapenko V.V.
Research of the operability of an air-fuel lubrication and cooling system of gas turbine engine rotor bearings
Klimov V.N., Dud’ev D.Y., Sigaylo V.Y., Klimov N.I., Mashkov Y.K.
Problematic issues of assessing the strength of axisymmetric parachute systems by conducting breakdown tests in flight experiments
Ivanov P.I., Kurinnyy S.M., Krivorotov M.M., Shmerova G.V.
Selecting a squeeze film damper model for solving problems of gas turbine engine rotor dynamics
Leontiev M.K., Kutakov M.N.
Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines
Galperin R.N., Gulyaev Y.I., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Terminal control of aerospace system subhypersonic first stage
Balakin V.L., Kovalyov A.V.
Influence of the suspension system on the accuracy of the aircraft modal testing results
Berns V.A., Dolgopolov A.V., Zhukov E.P., Marinin D.A.
Research of hydrodynamic processes in the lubrication system of gas turbine engines
Gulienko A.I., Shchurovskiy Y.M.
Investigation of the seizing mechanism of aviation hydraulic drive spool–and–sleeves
Gareyev A.M., Popelniuk I.A.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
Conceptual model of the formation of flying skills in the process of training using flight simulators
Godunov A.I., Kuatov B.Z., Yurkov N.K., Kurtaev S.Z.
Information support of aviation embedded information and control systems lifecycle
Akimova T.E.
Method of choosing spacecraft design characteristics on the basis of creating task-oriented systems of computer-aided design
Kucherov A.S., Kurenkov V.I.
Dynamic construction of the educational process in an integrated learning system
Grinberg G.M.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
Developing models of information-analytical monitoring system design, engineering and manufacturing processes aircraft companies
Zheleznov O.V., Blyumenshteyn A.A., Chernikov M.S.
Аcoustical-mechanical sound generators for creating an acoustical impression of а car
Starobinski R.N., Krasnov A.V., Kovaleva A.A., Vilch N.V.
Constructing the specification for the on-board realtime control algorithm
Tyugashev A.A., Bogatov A.Y.
Reduction of the focal spot size in high-aperture focusing systems at inserting of aberrations
Pelevina E.A., Khonina S.N.
Inkjet heat transfer working model phone (fuel transportation) refrigerator drip emitters prospective spacecraft
1 1., 1 1., 1 1.
Solving the problem of stabilizing program deployment of an orbital tether system taking into account limitations on the rotary motion of the tip body
1 1., 1 1.
Motion trajectories of the vehicle with mass injection pre-compressor cooling turbojet engines as the first stage of aircraft-space systems
1 1., 1 1.
Statistical modeling of the process of serving the leaving passengers at the international Kurumotch airport
Romanenko V.A.
3D model didactic properties investigations for geometrical modeling principles training
Ivashchenko V.I.
Optimizing the propulsion of a hypersonic accelerator aircraft of a two-stage aerospace system
Balakin V.L., Bebyakov A.A., Kotchyan A.G.
Analysis of schemes and methods of hydrodynamic cleaning of hydro-fuel system units
Sanchugov V.I., Reshetov V.M.
Disturbed transatmospheric motion of the first stage of an aerospace system
Krikunov M.M.
Analysis of load balancing algorithms using discrete event simulation
Khayrutdinov A.R., Vostokin S.V.
Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses
Shishkov V.A.
The concept of generalized method of calculation and design of wet cleaning duct GTD
Silaev B.M., Malcev E.N.
Development of elements and parameters of LNG fuel system with cryogenic piston pump and gas receiver for road gas turbine locomotive
Bukin V.A., Rudenko V.F.
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