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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.
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.
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.
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.
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
,
Problems of testing and operation of hydraulic power transfer units
Polyakov N.A., Frolov G.K., Tselischev V.A., Tselischev D.V.
Scalable distributed systems of competitive interacting processes and their optimality
1 1.
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.
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.
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.
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.
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.
Cycle air heating system of gas pumping unit NEVA-25NK
1 1., 1 1., 1 1., 1 1.
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.
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.
Prospective lines of improving the process of evaluating the technical condition of aircraft hydraulic system working fluid
Koptev A.N., Gareyev A.M., Popelnyuk I.A.
Mathematical model of fuel sloshing in the measuring channel of the fuel expenditure control system
Kryukov Y.A.
Using the theory of dynamic analogies for modelling automated manufacturing systems
Gareyev A.M., Koptev A.N., Gareyev T.M.
Research of a sleeve connection of the aircraft pipeline under the influence of dynamic loading
Agafonov V.M., Pykhalov A.A.
Iodine as an alternative propellant for electrojet engines
Ostrovskiy V.G., Smolentsev A.A., Scherbina P.A.
Thermal medical software hardware-based thermal imager COX CX - 320U
Davydov I.E., Agafonov A.N.
Internal controls board computer system running real time operation system as an iterative aggregate
Dolbnya N.A.
Improvement of the flight attitude control accuracy of the Earth observation spacecraft
Akhmetov R.N., Sollogub A.V., Makarov V.P., Golovchenko A.A., Filatov A.V.
Development of a virtual prototype of gasturbine engine at the stage of conceptual thermogasdynamic designusing the CAE-system «ASTRA»
Tkachenko A.Y., Krupenich I.N.
Pressure pulsation dampers as a means of improving the inherent vibroacoustic charateristics of hydraulic test rigs
Berestovitsky E.G., Gladilin Y.A., Kryuchkov A.N., Fyodorov A.Y., Frantov A.A., Shakhmatov Y.V.
Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system
Veretennikov S.V., Khasanov S.M.
Dynamic positioning of a manned submersible over the service object
Alekseev A.V., Olenin A.L., Smirnov G.V., Fendrikov A.N.
Analysis of on-board equipment robustness on the basis of COTS-products
Yefanov V.N., Bondarev A.V.
Tether parameters consideration during motion simulation of orbital tether system
1 1.
Statistical analysis of a capsule’s motion during its reentry into the atmosphere with the aid of a space tether system
1 1., 1 1.
Methodology of the adaptive graphic and geometric training for the computer aided design teaching
1 1.
Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered
1 1.
Reliability indicators of information control systems with hardware and software failures as complex time functions
Maryukhnenko V.S.
Solving the least squares problem using the method of an extended set of equations with sparse matrix
Gogoleva S.Y., Zoteeva O.V.
Means of illumination of an underwater situation of manned submersibles
Alekseev A.V., Belenky V.N., Olenin A.L., Smirnov G.V.
Comparison of mass properties of high- pressure cylinders with cryogenic fill for a throttle cooling system
Dovgjallo A.I., Sarmin D.V., Uglanov D.A.
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.
Imitation models of aircraft hydraulic units with account for typical faults
Gareyev A.M., Popelnyuk I.A., Stadnik D.M.
Biological module “BiNOM” for cubesats of the SamSat family
Zakharov V.P., Konyukhov V.N., Bakhtinov P.I., Molchkov E.V., Kornilin D.V., Konovalov S.G.
Peculiarities of using hot-air balloons in tests of parachute systems
Kurinny S.M., Krivorotov M.M., Baranichenko E.A.
Dynamics of feed water flow rate control system with low- noise regulator
Berestovitskiy E.G., Kizilov P.I., Kruchkov A.N., Pialov N.V.
Spacecraft power supply system using additional low-power sources of energy
Kargu D.L., Beznyakov A.M., Nemirov A.V.
Possibility of using leo satellite communication systems for on-line data interchange
Davydov D.D.
Developing a problem-oriented system for automated design of observation space vehicles capable of interacting with a PDM-system
Yakishchik A.A.
Method and apparatus for evaluating the efficiency of energy transfer from combustion products to abrasive particles at the exit of a sand blaster nozzle
Kornilin D.V., Medvedev M.V.
Computational algorithm of forming program motion in a scheduled turn of small spacecraft
Salmin V.V., Filatov A.V., Tkachenko I.S., Tyugashev A.A., Sopchenko E.V.
Creation of a data retrieval system for choosing the optimal cutting tool in manufacturing aircraft engine parts
Shulepov A.P., Meshcheryakov A.V., Ramzaeva E.A.
Building foundations of virtual information-based educational environment
Zelenko L.S., Zagumennov D.A., Zinchenko A.O.
Increasing the equivalence of realize full scale tests with the influence of geometrics parameters of the load system
Kulikov E.N.
Investigation of the influence of non-axisymmetric elements in secondary air system on gas turbine engine flow parameters, the temperature field and deformation of components
Tisarev A.Y., Vasilevich N.M.
The influence of tether jamming on the motion of a space tether system during dynamic deployment
Ledkov A.S., Dyukov D.I.
Optimization of strength characteristics of lighting devices aircraft by construction of virtual models
Abulkhanov S.R., Goryainov D.S., Skuratov D.L.
Effect of cavity width on performance of pre-swirl systems
Didenko R.A., Karelin D.V., Ievlev D.G., Lebedev V.V., Belousova E.V.
Transformation of longitudinal deformation wave at the boundary of conjugation of bars with an elastic element
Manzhosov V.K., Novikova I.A.
Simulation of fluid contamination control process
Gareyev A.M.
Using active noise suppression non-adaptive systems with a transfer function model for the reduction of medical equipment noise
Sementsov S.G.
Conception of the student work place arrengement for the computer aided design base teaching
1 1., 1 1.
Inkjet heat transfer working model phone (fuel transportation) refrigerator drip emitters prospective spacecraft
1 1., 1 1., 1 1.
Flight path of a supersonic aeroplane as the first stage of an aerospace system
Balakin V.L., Potapov V.I.
Analysis of industrial subject area stability and dimensionality characteristics using automated systems of document turnover
Khaimovitch I.N.
Integrated assessment of the efficiency of an orbital inspection space system based on small satellites
Tkachenko I.S., Kaurov I.V.
System of satellite navigation of «Bion-M» space vehicle
Manturov A.I., Rublyov V.I., Muntyan R.Y.
Mathematical modeling of the evolution of a tribosystem in the process of formation of equilibrium roughness of a frictional contact
Kolesnikov I.V., Koropets P.A., Manturov D.S., Shakhmatov Y.V.
Technology of low-emission fuel combustion and conceptual structure of the combustion chamber of a gas-turbine power plant
Tsybizov Y.I., Tyulkin D.D., Vorotyntsev I.E.
Vector optimization of the parameters of a queueing system with partial mutual assistance between channels
Romanenko V.A.
Theoretical and experimental investigation of the photographic reconnaissance plane instrument bay thermal state
Nikolayev V.N.
Use of the methods of the structural programming to form the «reliability» diagrams of the fuel supply system of the gas turbine engines with the control elements failure order of no less than four
Smurova N.A.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
Balakin V.L., Krikunov M.M.
Backstepping synthesis of the height control system of an unmanned aerial vehicle
Akhramovich S.A., Barinov A.V., Malyshev V.V., Starkov A.V.
Set-theory model of the aircraft hydraulic system working fluid state
Koptev A.N., Gareyev A.M., Popelnyuk I.A.
Information control system for space experiments onboard international space station
Voronin F.A., Dunaeva I.V.
Efficiency of terminal control in the trans-atmospheric first stage of an aerospace system under atmospheric and aerodynamic disturbances
Balakin V.L., Kovalyov A.V., Krikunov M.M.
Thermal design of «AIST» small spacecraft
Kulikov D.S., Erilkin J.N.
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