| Issue |
Title |
File |
| Vol 16, No 3 (2017) |
Set-theory model of the aircraft hydraulic system working fluid state |
(Rus)
|
|
Koptev A.N., Gareyev A.M., Popelnyuk I.A.
|
| Vol 16, No 3 (2017) |
Peculiarities of using hot-air balloons in tests of parachute systems |
(Rus)
|
|
Kurinny S.M., Krivorotov M.M., Baranichenko E.A.
|
| Vol 16, No 3 (2017) |
Selecting a squeeze film damper model for solving problems of gas turbine engine rotor dynamics |
(Rus)
|
|
Leontiev M.K., Kutakov M.N.
|
| Vol 16, No 3 (2017) |
Construction of an upper stage flight pattern for placing a group of spacecraft into an orbit plane with the required angular distance between the satellites |
(Rus)
|
|
Poplevin A.S., Panov N.A.
|
| Vol 16, No 3 (2017) |
Locally optimal control of space tug motion between the libration points of the Earth-Moon system |
(Rus)
|
|
Starinova O.L., Fain M.K.
|
| Vol 16, No 3 (2017) |
Iteration procedure of choosing a low-thrust rendezvous transfer control program in problems of space debris disposal in the geostationary orbit |
(Rus)
|
|
Philippov G.A.
|
| Vol 16, No 3 (2017) |
Development of small satellite structure taking into account the use of laser measuring systems |
(Rus)
|
|
Shaposhnikov S.N.
|
| Vol 16, No 3 (2017) |
Mathematical model and optimization of helicopter vertical takeoff considering operational conditions and aerodynamic damping |
(Rus)
|
|
Onushkin Y.P., Sizov D.A., Poluyakhtov V.A., Ostrovoy A.V.
|
| Vol 16, No 2 (2017) |
Control over the deployment of an orbital tether system of great length |
(Rus)
|
|
Wang C., Zabolotnov Y.M.
|
| Vol 16, No 2 (2017) |
Formulas of reducing engine environmental performance and combustion characteristics to standard atmospheric conditions |
(Rus)
|
|
Grigoriev A.V., Kosmatov A.A., Rudakov O.A., Solovieva A.V.
|
| Vol 16, No 2 (2017) |
Fluctuations of liquid fuel in tanks with oil recovery units |
(Rus)
|
|
Dyachenko M.I., Duy Hung N., Temnov A.N.
|
| Vol 16, No 2 (2017) |
Development and analysis of models of heat transfer in compact porous heat exchangers of aero space control systems |
(Rus)
|
|
Konovalov D.A.
|
| Vol 16, No 2 (2017) |
Complex approach to aerodynamic design of inlet ducts with submerged vortex-free air intakes |
(Rus)
|
|
Kornev A.V., Boychuk I.P.
|
| Vol 16, No 2 (2017) |
Some issues of research and development in aviation industry |
(Rus)
|
|
Korchak V.Y., Kuznetsov V.V., Borisenkov I.L., Leonovich G.I., Lukachev S.V., Biryuk V.V.
|
| Vol 16, No 2 (2017) |
Micro gas turbine engine imitation model |
(Rus)
|
|
Kuznetsov A.V., Makaryants G.M.
|
| Vol 16, No 2 (2017) |
Criterion assessment of the possibility to prolong the service life limit of the helicopter tail drive shaft |
(Rus)
|
|
Mashoshin O.F., Semenikhin R.L.
|
| Vol 16, No 2 (2017) |
Mathematical modeling of a controlled electromechanical actuator for special assembly and coupling equipment |
(Rus)
|
|
Nosov A.S.
|
| Vol 16, No 2 (2017) |
Assessment of gas turbine engine airfoil surface microstructure |
(Rus)
|
|
Nosov N.V., Abramov A.D., Kosulin S.I.
|
| Vol 16, No 2 (2017) |
Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments |
(Rus)
|
|
Popov P.A., Sindyukov A.A., Malykhina O.I.
|
| Vol 16, No 2 (2017) |
Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines |
(Rus)
|
|
Ryzhkov V.V., Verjasov Y.N., Galperin R.N., Gulyaev Y.I., Ivashin Y.S.
|
| Vol 16, No 2 (2017) |
Assessment of a liquid rocket engine concept based on innovative technologies |
(Rus)
|
|
Solodovnikov A.V., Akinshin I.A., Golubyatnik V.V., Krivonogov A.V.
|
| Vol 16, No 2 (2017) |
Investigation of the thermal regime of microsatellite optoelectronic telescopic complex under operating conditions |
(Rus)
|
|
Tsaplin S.V., Bolychev S.A.
|
| Vol 16, No 1 (2017) |
Optimization of parameters of a hub aircraft ground handling system on the basis of a fuzzy-controller simulation model |
(Rus)
|
|
Vasileva I.A., Romanenko V.A., Khvostova T.V.
|
| Vol 16, No 1 (2017) |
Information control system for space experiments onboard international space station |
(Rus)
|
|
Voronin F.A., Dunaeva I.V.
|
| Vol 16, No 1 (2017) |
Analysis of the accuracy of autonomous navigation of the space robot in the diagnosis of the technical condition of an orbital object |
(Rus)
|
|
Golyakov A.D., Fominov I.V., Korolev S.Y.
|
| Vol 16, No 1 (2017) |
Design and technical characteristics of transport airplane for arctic exploration |
(Rus)
|
|
Kuprikov N.V., Dolgov O.S., Kuprikov M.Y., Ivanov B.V.
|
| Vol 16, No 1 (2017) |
Improvement of gas turbine engines due to isothermal expansion in the turbine |
(Rus)
|
|
Muraeva M.A., Gorjunov I.M.
|
| Vol 16, No 1 (2017) |
Frequency characteristics of a coaxial gas damper for booster feed line |
(Rus)
|
|
Odinokov D.A., Gimadiyev A.G.
|
| Vol 15, No 4 (2016) |
Development of intelligent peripheral devices of control and emergency protection systems for ground testing of liquid-propellant rocket engines |
(Rus)
|
|
Volnukhin O.A., Liseykin V.A., Tozhokin I.A., Churin M.N.
|
| Vol 15, No 4 (2016) |
Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines |
(Rus)
|
|
Galperin R.N., Gulyaev Y.I., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
|
| Vol 15, No 4 (2016) |
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks |
(Rus)
|
|
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
|
| Vol 15, No 4 (2016) |
Using the «virtual engine» software in automatic control system of gas turbine engine |
(Rus)
|
|
Golberg F.D., Gurevich O.S., Petukhov A.A.
|
| Vol 15, No 4 (2016) |
Development of an exhaust air turbine engine |
(Rus)
|
|
Yeliseev Y.S., Fedorchenco D.G., Tsibizov Y.I., Tyulkin D.D., Tkachenko A.Y.
|
| Vol 15, No 4 (2016) |
Method of transient simulation of combustion processes in a low-thrust rocket engine operating on gaseous hydrogen and oxygen |
(Rus)
|
|
Zubanov V.M., Shabliy L.S., Stepanov D.V.
|
| Vol 15, No 4 (2016) |
Analysis of low-thrust liquid rocket engines with a methane air pump unit |
(Rus)
|
|
Ivanov A.I., Kositsin I.P., Borisov V.A.
|
| Vol 15, No 4 (2016) |
Method of calculating the thickness of the combustion chamber of a liquid rocket engine made with the use of innovative technologies and materials |
(Rus)
|
|
Krivonogov A.V.
|
| Vol 15, No 4 (2016) |
Peculiarities of computer modeling of the working process in small gas turbine engines |
(Rus)
|
|
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
|
| Vol 15, No 4 (2016) |
Simulation of the work process of a two-stage pump with a first-stage hydraulic drive |
(Rus)
|
|
Matveev V.N., Shabliy L.S., Krivtsov A.V., Zubanov V.M., Ivanov A.I., Kositsin I.P., Baturin N.V.
|
| Vol 15, No 4 (2016) |
Peculiarities of the working process of low-thrust hypergolic-propellant liquid rocket engines with a thrust of less than 1 N |
(Rus)
|
|
Nigodjuk V.E., Sulinov A.V.
|
| Vol 15, No 4 (2016) |
Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor |
(Rus)
|
|
Posadov V.V., Remizov A.E.
|
| Vol 15, No 4 (2016) |
Mathematical modelling of the working process of a hot gas pressure feed system |
(Rus)
|
|
Salich V.L.
|
| Vol 15, No 4 (2016) |
Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber |
(Rus)
|
|
Sviridenkov A.A., Tretyakov V.V.
|
| Vol 15, No 4 (2016) |
Research of liquid outflow from low-emission swirl injectors of a low-thrust liquid rocket engine |
(Rus)
|
|
Semkin Y.V.
|
| Vol 15, No 4 (2016) |
Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder |
(Rus)
|
|
Tretyakov V.V., Sviridenkov A.A.
|
| Vol 15, No 4 (2016) |
Application of structure-energy failure theory for determining the probability of failure and durability of turbine and compressor blades of aircraft engines |
(Rus)
|
|
Chernyaev A.I., Trefilov V.A.
|
| Vol 15, No 3 (2016) |
Efficiency of terminal control in the trans-atmospheric first stage of an aerospace system under atmospheric and aerodynamic disturbances |
(Rus)
|
|
Balakin V.L., Kovalyov A.V., Krikunov M.M.
|
| Vol 15, No 3 (2016) |
Spacecraft power supply system using additional low-power sources of energy |
(Rus)
|
|
Kargu D.L., Beznyakov A.M., Nemirov A.V.
|
| Vol 15, No 3 (2016) |
Evaluation of the influence of the number of blades and diameter on propeller noise |
(Rus)
|
|
Moshkov P.A., Samokhin V.F.
|
| Vol 15, No 2 (2016) |
Terminal control of aerospace system subhypersonic first stage |
(Rus)
|
|
Balakin V.L., Kovalyov A.V.
|
| Vol 15, No 2 (2016) |
СWSME – complex of wide-swath multispectral equipment for the «Resource-P» spacecraft |
(Rus)
|
|
Baklanov A.I., Afonin A.N., Blinov V.D., Zabiyakin A.S.
|
| Vol 15, No 2 (2016) |
High resolution equipment for the future spacecraft «Resource-PM» |
(Rus)
|
|
Baklanov A.I., Blinov V.D., Gorbunov I.A., Zabiyakin A.S., Malakhov I.A.
|
| Vol 15, No 2 (2016) |
Analysis of the accuracy of Earth remote sensing satellite angular motion control and track guidance during route observation intervals |
(Rus)
|
|
Galkina A.S., Platoshin I.V.
|
| Vol 15, No 2 (2016) |
Application of simulation modelling in static tests of space-rocket vehicles |
(Rus)
|
|
Grebnev D.N., Duplihin V.K., Zuperman J.A., Aistov A.I., Kukushkin V.E.
|
| Vol 15, No 2 (2016) |
On-board algorithm for SamSat-218D nanosatellite orientation and stabilization system |
(Rus)
|
|
Kramlikh A.V., Melnik M.E.
|
| Vol 15, No 2 (2016) |
Optimal control laws of onboard coils for the reduction of angular momentum and damping of angular velocity of nanosatellites and microsatellites with magnetic coils on board |
(Rus)
|
|
Lyubimov V.V., Podkletnova S.V.
|
| Vol 15, No 2 (2016) |
Procedure of comparative assessment of the efficiency of Earth remote sensing satellites with different optoelectronic telescopic complexes |
(Rus)
|
|
Stratilatova N.N., Kurenkov V.I., Kucherov A.S., Egorov A.S.
|
| Vol 15, No 2 (2016) |
Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem |
(Rus)
|
|
Tsaplin S.V., Bolychev S.A.
|
| Vol 15, No 2 (2016) |
Analysis of motion stability of a deployed space tether system with an atmospheric probe |
(Rus)
|
|
Zhe D., Zabolotnov Y.M., Changqing W.
|
| Vol 15, No 1 (2016) |
Selection of a nanosatellite group separation program for cluster launching from the «Soyuz» launch vehicle orbiter |
(Rus)
|
|
Avaryaskin D.P., Shcherbakov M.S.
|
| Vol 15, No 1 (2016) |
Influence of the suspension system on the accuracy of the aircraft modal testing results |
(Rus)
|
|
Berns V.A., Dolgopolov A.V., Zhukov E.P., Marinin D.A.
|
| Vol 15, No 1 (2016) |
System-mathematical simulation of engine air hydraulic power supply |
(Rus)
|
|
Goryunova N.R., Goryunov A.A.
|
| Vol 15, No 1 (2016) |
Monostatic P-band radar system for advanced small satellites |
(Rus)
|
|
Goryachkin O.V., Zhengurov B.G., Maslov I.V.
|
| Vol 15, No 1 (2016) |
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system |
(Rus)
|
|
Zabolotnov Y.M., Lobankov A.A.
|
| Vol 15, No 1 (2016) |
Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit |
(Rus)
|
|
Ishkov S.A.
|
| Vol 15, No 1 (2016) |
Modeling orbital tether system deployment with limitations on the deployment speed |
(Rus)
|
|
Ishkov S.A., Filippov G.A., Xiaoye X.
|
| Vol 15, No 1 (2016) |
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 |
(Rus)
|
|
Kuznetsov U.L., Ukraintsev D.S.
|
| Vol 15, No 1 (2016) |
Thermal design of «AIST» small spacecraft |
(Rus)
|
|
Kulikov D.S., Erilkin J.N.
|
| Vol 15, No 1 (2016) |
Simulation of the process of angular rate damping of the SamSat-218D nanosatellite after separation from the launching-transporting container |
(Rus)
|
|
Melnik M.E.
|
| Vol 15, No 1 (2016) |
Mathematical model of angular motion of nanosatellites with inertial actuators |
(Rus)
|
|
Moldabekov M.M., Ahmedov D.S., Elubaev S.A., Sukhenko A.S., Bopeev T.M., Alipbayev K.A., Mikhailenko D.L.
|
| Vol 15, No 1 (2016) |
Results of operation of scientific hardware «Space system of microacceleration compensation» |
(Rus)
|
|
Semkin N.D., Piyakov I.V.
|
| Vol 15, No 1 (2016) |
Small spacecraft for the registration of micrometeorites and space debris |
(Rus)
|
|
Semkin N.D., Telegin А.М., Vidmanov A.S.
|
| Vol 15, No 1 (2016) |
Determination of relative position and orientation of nanosatellites by video image analysis |
(Rus)
|
|
Simakov S.P., Ustyugov E.V.
|
| Vol 15, No 1 (2016) |
Monitoring of the Earth’s ionosphere by a small satellite constellation |
(Rus)
|
|
Phylonin O.V., Nikolayev P.N.
|
| Vol 15, No 1 (2016) |
Technologies of reducing the technological environmental impact of space rocket launches |
(Rus)
|
|
Shatrov J.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y., Sitnikov D.V., Lempert D.B.
|
| Vol 14, No 4 (2015) |
Method of creating digital terrain models and its practical application as exemplified by Samara region |
(Rus)
|
|
Anshakov G.P., Myatov G.N., Malinovskii V.A.
|
| Vol 14, No 4 (2015) |
Bypass as an attribute of unmanned spacecraft operability in anomalous flight situations |
(Rus)
|
|
Akhmetov R.N., Makarov V.P., Sollogub A.V.
|
| Vol 14, No 4 (2015) |
Procedure of accomodation of earth remote sansing satellite external devices with regard for the satellite target operation |
(Rus)
|
|
Akhmetov R.N., Shilov L.B., Kurenkov V.I., Yakischik A.A.
|
| Vol 14, No 4 (2015) |
Choosing a program for controlling the deployment of an orbital tether system with deployment speed limitations |
(Rus)
|
|
Ishkov S.A., Xiaoye X., Filippov G.A.
|
| Vol 14, No 4 (2015) |
Flight development tests and attempted operation of «AIST» small satellites |
(Rus)
|
|
Kirilin A.N., Tkachenko S.I., Salmin V.V., Semkin N.D., Papkov A.P., Abrashkin V.I., Tkachenko I.S., Zheleznov Y.E., Galaeva E.Y.
|
| Vol 14, No 4 (2015) |
Optimization of spatial turns of «AIST-2» small spacecraft on the basis of the principle of minimum control |
(Rus)
|
|
Petrishchev V.F., Shipov M.G.
|
| Vol 14, No 4 (2015) |
Stochastic optimal integration of hub airport technological resources |
(Rus)
|
|
Romanenko V.A.
|
| Vol 14, No 4 (2015) |
Control of in-plane orbit parameters of a geostationary low-thrust satellite |
(Rus)
|
|
Salmin V.V., Chetverikov A.S.
|
| Vol 14, No 3 (2014) |
Stochastic method of investigating perturbed motion of a space vehicle in the atmosphere |
(Rus)
|
|
Sokolov N.L.
|
| Vol 14, No 3 (2014) |
Models of reliability and determination of acceptable periodicity of maintenance of ageing aircraft fleet |
(Rus)
|
|
Pisarenko V.N.
|
| Vol 14, No 2 (2015) |
Computational algorithm of forming program motion in a scheduled turn of small spacecraft |
(Rus)
|
|
Salmin V.V., Filatov A.V., Tkachenko I.S., Tyugashev A.A., Sopchenko E.V.
|
| Vol 14, No 1 (2015) |
Development of a solar battery orientation robot system for small spacecraft |
(Rus)
|
|
Beznyakov A.M., Vlasov V.A., Malenin E.N.
|
| Vol 14, No 1 (2015) |
Analytical evaluation of the accuracy of spacecraft autonomous navigation according to the results of flight altitude adaptive measurement |
(Rus)
|
|
Golyakov A.D., Fominov I.V.
|
| Vol 14, No 1 (2015) |
Research of small spacecraft dynamiсs taking into account the influence of elastic vibrations of asjacent solar panels and aerodynamic moment |
(Rus)
|
|
Yelenev V.D., Titov B.A., Davydov E.I., Davydov I.E., Kochyan A.G., Yudintsev V.V.
|
| Vol 14, No 1 (2015) |
Optimization of fatique validation cost for redesigned transport aircraft |
(Rus)
|
|
Kleptsov V.I.
|
| Vol 14, No 1 (2015) |
Electrization of the surface of low-orbiting small spacecraft “AIST” |
(Rus)
|
|
Syomkin N.D., Bragin V.V., Piyakov A.V., Telegin A.M., Ryazanov D.M., Matviets M.G.
|
| Vol 14, No 1 (2015) |
Device for monitoring radiation situation on spacecraft |
(Rus)
|
|
Syomkin N.D., Plokhotnichenko P.G., Ilyin A.B., Kalaev M.P., Ryazanov D.M., Pomel'nikov P.A.
|
| Vol 14, No 1 (2015) |
Missile control on the basis of construction of attainability domains |
(Rus)
|
|
Tolpegin O.A.
|
| Vol 14, No 1 (2015) |
Concept of multilevel adaptation of integrated navigation systems of small spacecraft |
(Rus)
|
|
Fominov I.V.
|
| Vol 14, No 1 (2015) |
Method of parametric optimization of each component of adaptive compensatng inertial sensors operating in a self-oscilation mode |
(Rus)
|
|
Fominov I.V.
|
| Vol 13, No 4 (2014) |
Conceptual model of the formation of flying skills in the process of training using flight simulators |
(Rus)
|
|
Godunov A.I., Kuatov B.Z., Yurkov N.K., Kurtaev S.Z.
|
| Vol 13, No 4 (2014) |
Accuracy control method for space complex products at the stage of design engineering |
(Rus)
|
|
Yelenev V.D., Shuplyak Y.P.
|
| Vol 13, No 4 (2014) |
Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine |
(Rus)
|
|
Ishkov S.A., Filippov G.A.
|
| Vol 13, No 4 (2014) |
Assessing skills level of flying cadets |
(Rus)
|
|
Kuatov B.Z., Kurtaev S.Z.
|
| Vol 13, No 4 (2014) |
Identification of scale factor of a pendulum compensating accelerometer during an orbital spacecraft mission |
(Rus)
|
|
Fominov I.V.
|
| Vol 15, No 2 (2016) |
Metodological basis of the development of a problem-oriented system for selecting design parameters of space vehicles |
(Rus)
|
|
Stratilatov N.R., Kurenkov V.I., Kucherov A.S., Yakishik A.A.
|
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