| Issue |
Title |
File |
| Vol 18, No 4 (2019) |
Formation of film cooling on the turbine blade back and pressure side in the case of using V-shaped dimples |
(Rus)
|
|
Lebedev V.V., Lebedev O.V., Remizov A.E.
|
| Vol 18, No 4 (2019) |
Computer-aided design of low-thust rocket engines using the domain-specific knowledge database and CAE / CAD systems |
(Rus)
|
|
Ryzhkov V.V., Morozov I.I., Lapshin E.A.
|
| Vol 18, No 4 (2019) |
Control program for noncoplanar heliocentric flight to Venus of non-perfectly reflecting solar sail spacecraft |
(Rus)
|
|
Khabibullin R.M.
|
| Vol 18, No 4 (2019) |
Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control |
(Rus)
|
|
Shorikov A.F., Kalev V.I.
|
| Vol 18, No 4 (2019) |
Optimal control of spacecraft motion in the vicinity of Eros 433 asteroid |
(Rus)
|
|
Shornikov A.Y.
|
| Vol 18, No 3 (2019) |
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 |
(Rus)
|
|
Ananenko V.M., Golyakov A.D., Kalabin P.V.
|
| Vol 18, No 3 (2019) |
Disturbed motion of the hypersonic first stage of an aerospace system in climb |
(Rus)
|
|
Balakin V.L., Krikunov M.M.
|
| Vol 18, No 3 (2019) |
Selection of project structure for nanosatellite propulsion system |
(Rus)
|
|
Belokonov I.V., Ivliev A.V., Bogatyrev A.M., Kumarin A.A., Lomaka I.A., Simakov S.P.
|
| Vol 18, No 3 (2019) |
Determining a rational scheme of machining of gas turbine engine essential parts in magnetorheological environments by the method of expert assessment |
(Rus)
|
|
Boytsov A.G., Kurilovich S.V., Kuritsyna V.V., Siluyanova M.V.
|
| Vol 18, No 3 (2019) |
Gas dynamic calculation of detonation in constant-cross-section ducts |
(Rus)
|
|
Grigoriev A.V., Rudakov O.A., Solovieva A.V.
|
| Vol 18, No 3 (2019) |
Choosing the aerodynamic configuration of a subsonic cruise missile |
(Rus)
|
|
Kovalev M.A., Nikitin A.N.
|
| Vol 18, No 3 (2019) |
Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines |
(Rus)
|
|
Kuz'michev V.S., Omar H., Tkachenko A.Y., Bobrik A.A.
|
| Vol 18, No 3 (2019) |
Prospects of application of additive technologies to develop parts and components of gas turbine engines and ramjets |
(Rus)
|
|
Magerramova L.A., Nozhnitsky Y.A., Volkov S.A., Volkov M.E., Chepurnov V.Z., Belov S.V., Verbanov I.S., Zaikin S.V.
|
| Vol 18, No 3 (2019) |
Method for determination of optimal geometrical parameters of a unit cell of X-shaped truss cores |
(Rus)
|
|
Mousavi Safavi S.M.
|
| Vol 18, No 3 (2019) |
Life of gas turbine engine components under corrosive exposure |
(Rus)
|
|
Pivovarova M.V., Gladkiy I.L.
|
| Vol 18, No 3 (2019) |
Justification of the architecture of an interactive information model of the process of space-mission vehicle launch preparation |
(Rus)
|
|
Privalov A.E., Bugaichenko P.Y.
|
| Vol 18, No 3 (2019) |
Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines |
(Rus)
|
|
Ryzhkov V.V., Morozov I.I.
|
| Vol 18, No 3 (2019) |
Design of experiments for verification of computational life prediction methods |
(Rus)
|
|
Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.
|
| Vol 18, No 3 (2019) |
Methods of validation of the ballistic structure of space surveillance system orbital segment |
(Rus)
|
|
Fadin I.A., Yanov S.V., Samokhvalov O.A.
|
| Vol 18, No 2 (2019) |
Disturbed motion of a hypersonic vehicle in climb |
(Rus)
|
|
Balakin V.L., Krikunov M.M.
|
| Vol 18, No 2 (2019) |
Relative equilibria of dynamically symmetric CubeSat nanosatellite under the action of aerodynamic and gravitational torques |
(Rus)
|
|
Barinova E.V., Timbai I.A.
|
| Vol 18, No 2 (2019) |
Reducing the influence of interference of spacecraft magnetic field on magnetic measurements |
(Rus)
|
|
Beznyakov A.M., Guriev I.S., Ryzhova I.P.
|
| Vol 18, No 2 (2019) |
Determining the dynamics of spacecraft rotational motion with the use of information provided by global navigation satellite systems |
(Rus)
|
|
Belokonov I.V., Kramlikh A.V., Lomaka I.A.
|
| Vol 18, No 2 (2019) |
Theory of gas turbine engine optimal gas generator |
(Rus)
|
|
Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.
|
| Vol 18, No 2 (2019) |
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 |
(Rus)
|
|
Ryzhkov V.V., Morozov I.I.
|
| Vol 18, No 2 (2019) |
Calculation of lubricant flow in the slide bearing of the aviation engine reducer |
(Rus)
|
|
Siluyanova M.V., Fertikov A.О.
|
| Vol 18, No 2 (2019) |
Research of hafnium-containing defects in granular nickel EP741NP alloy using electron microscopy |
(Rus)
|
|
Trunkin I.N., Artamonov M.A., Ovcharov A.V., Vasiliev A.L.
|
| Vol 18, No 2 (2019) |
Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation |
(Rus)
|
|
Tsaplin S.V., Bolychev S.A.
|
| Vol 18, No 2 (2019) |
Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices |
(Rus)
|
|
Chervonyuk V.V., Korovin B.B.
|
| Vol 18, No 2 (2019) |
Reduction of angular velocities of AIST-2D spacecraft using a system of kinetic moment dumping |
(Rus)
|
|
Shipov M.G.
|
| Vol 18, No 1 (2019) |
Convective current experiments using Dakon-P equipment onboard “Progress” cargo spacecraft |
(Rus)
|
|
Ayukaeva D.M., Babushkin I.A., Belyaev M.Y., Zilberman Y.A., Matveeva T.V., Sidorov A.S.
|
| Vol 18, No 1 (2019) |
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system |
(Rus)
|
|
Balakin V.L., Krikunov M.M.
|
| Vol 18, No 1 (2019) |
Imitation models of aircraft hydraulic units with account for typical faults |
(Rus)
|
|
Gareyev A.M., Popelnyuk I.A., Stadnik D.M.
|
| Vol 18, No 1 (2019) |
Gas dynamic calculation of detonation in variable cross-section ducts |
(Rus)
|
|
Grigoriev A.V., Rudakov O.A., Solovieva A.V.
|
| Vol 18, No 1 (2019) |
Research of the operability of an air-fuel lubrication and cooling system of gas turbine engine rotor bearings |
(Rus)
|
|
Klimov V.N., Dud’ev D.Y., Sigaylo V.Y., Klimov N.I., Mashkov Y.K.
|
| Vol 18, No 1 (2019) |
Influence of the geometry fidelity of resonant sound-absorbing liner samples on their acoustic characteristics |
(Rus)
|
|
Kustov O.Y., Khramtsov I.V., Bulbovich R.V.
|
| Vol 18, No 1 (2019) |
Investigation of the technology of mutual navigation and orientation of small space vehicles flying in formation |
(Rus)
|
|
Nebylov A.V., Perliouk V.V., Leontieva T.S.
|
| Vol 18, No 1 (2019) |
Multi-satellite Universat-SOCRAT mission for monitoring technogenic and natural hazards |
(Rus)
|
|
Sadovnichiy V.A., Panasyuk M.I., Lipunov V.M., Belov A.A., Bogomolov V.V., Garipov G.K., Gorbovskoi E.S., Iyudin A.F., Kalegaev V.V., Klimov P.A., Kornilov V.G., Mit S.K., Osedlo V.I., Petrov V.L., Podzolko M.V., Popova E.P., Rubinshtein I.A., Svertilov S.I., Tulupov V.I., Chepurnov A.S., Yashin I.V.
|
| Vol 18, No 1 (2019) |
Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades |
(Rus)
|
|
Sazonov M.B., Solovatskaya L.V.
|
| Vol 18, No 1 (2019) |
Development of the active gas generator for high altitude firing test benches |
(Rus)
|
|
Salich V.L.
|
| Vol 18, No 1 (2019) |
Russian-Azerbaijani space project of a small satellite for science and technology experiments |
(Rus)
|
|
Samedov A.S., Panasyuk M.I., Abdulaev P.S., Bogomolov V.V., Gasanov R.A., Ibragimov R.A., Iyudin A.F., Mammadzada T.G., Musaev A.A., Osedlo V.I., Petrov V.L., Podzolko M.V., Popova E.P., Rustamov R., Svertilov S.I., Seiidov H., Yashin I.V.
|
| Vol 18, No 1 (2019) |
Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle |
(Rus)
|
|
Khramov A.A.
|
| Vol 18, No 1 (2019) |
Use of ultra-small space vehicles for studying near-Earth plasma by radiophysical methods |
(Rus)
|
|
Chugunin D.V., Chernyshov A.A., Mogilevsky M.M., Moiseenko I.L., Petrukovich A.A.
|
| Vol 18, No 1 (2019) |
Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber |
(Rus)
|
|
Matveev S.G.
|
| Vol 17, No 4 (2018) |
Automated construction of a fan blade model according to data of CAD profile measurements |
(Rus)
|
|
Arkhipov A.N., Bugrjashova E.V., Ravikovich Y.A., Savin R.A., Terentjev V.V., Shevjakov A.O.
|
| Vol 17, No 4 (2018) |
Analysis of control programs and flight paths of a hypersonic vehicle in climb |
(Rus)
|
|
Balakin V.L., Krikunov M.M.
|
| Vol 17, No 4 (2018) |
Construction of limitation diagrams for truss core stiffness and strength parameters |
(Rus)
|
|
Gainutdinov V.G., Gainutdinova T.Y., Abdullin I.N.
|
| Vol 17, No 4 (2018) |
Theory and calculation of parameters of the detonation engine thermodynamical cycle |
(Rus)
|
|
Grigoriev A.V., Mitrofanov V.A., Rudakov O.A., Solovieva A.V.
|
| Vol 17, No 4 (2018) |
Оptimization of gas turbine aircraft engine control throughout the engine service life |
(Rus)
|
|
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
|
| Vol 17, No 4 (2018) |
Development of methods for ensuring energy balance for the operation of mission equipment of “AIST”-series small satellites under conditions of power limitations |
(Rus)
|
|
Ivanushkin M.A., Salmin V.V., Tkachenko S.I., Tkachenko I.S., Volgin S.S.
|
| Vol 17, No 4 (2018) |
Programs of time-optimal control in the problem of rendezvous transfer of spacecraft with low transversal thrust |
(Rus)
|
|
Ishkov S.A., Filippov G.A., Fadeenkov P.V.
|
| Vol 17, No 4 (2018) |
Proposals for improving the efficiency and service life of the turbines of turbo-pump assemblies in liquid-propellant rocket engines by using double-sided crest-type radial labyrinth seals |
(Rus)
|
|
Levochkin P.S., Chvanov V.K., Vasiliev V.S., Timushev S.F.
|
| Vol 17, No 4 (2018) |
Optimization of fuel distribution in the afterburner of a gas turbine engine |
(Rus)
|
|
Nelyubin V.R.
|
| Vol 17, No 4 (2018) |
Impact of the turbulence modeling approach on the accuracy of the fan noise level prediction |
(Rus)
|
|
Pyatunin K.R., Arkharova N.V.
|
| Vol 17, No 4 (2018) |
Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft |
(Rus)
|
|
Ryzhkov V.V., Sulinov A.V.
|
| Vol 17, No 4 (2018) |
Experimental research on the development of an “oxygen (gas) + kerosene” – fueled thruster |
(Rus)
|
|
Salich V.L.
|
| Vol 17, No 4 (2018) |
Numerical simulation of low liquid flow in a mixer consisting of two centrifugal swirlers |
(Rus)
|
|
Semkin E.V.
|
| Vol 17, No 4 (2018) |
Comparative analysis of fuel distribution downstream of the gas-dynamic flame holder with various methods of injection |
(Rus)
|
|
Tretyakov V.V., Sviridenkov A.A.
|
| Vol 17, No 3 (2018) |
Mechanical engineer, scientist, teacher. On the occasion of centenary of the birth of I.A. Birger |
(Rus)
|
|
Nozhnitsky Y.A., Belousov A.I.
|
| Vol 17, No 3 (2018) |
Refining methods of vibration diagnostics of wear of turbo-prop engine differential speed reduction unit gear teeth |
(Rus)
|
|
Avramenko A.A., Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.
|
| Vol 17, No 3 (2018) |
Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading |
(Rus)
|
|
Badamshin I.K.
|
| Vol 17, No 3 (2018) |
Refinement of operable state recovery algorithms for “AIST” small satellites on the basis of telemetric information |
(Rus)
|
|
Volgin S.S., Salmin V.V., Tkachenko S.I., Tkachenko I.S., Ivanushkin M.A.
|
| Vol 17, No 3 (2018) |
Use of phase portraits of hydro-mechanical units for diagnosing aircraft hydraulic systems |
(Rus)
|
|
Gareyev A.M., Popelnyuk I.A.
|
| Vol 17, No 3 (2018) |
Analysis of schemes of correction of dynamic characteristics of acoustic probes for measuring pressure pulsations in a gas turbine engine |
(Rus)
|
|
Gimadiev A.G., Bystrov N.D., Dyagileva E.S.
|
| Vol 17, No 3 (2018) |
Estimating the efficiency of a bypass turbojet engine on the basis of a serial gas generator as a part of the power plant of a high-altitude unmanned aerial vehicle |
(Rus)
|
|
Zinenkov Y.V., Lukovnikov A.V., Popov A.V., Nechaev V.N.
|
| Vol 17, No 3 (2018) |
Schemes, parameters, work process, characteristics and structure of long-range interception aircraft engines |
(Rus)
|
|
Kovalev A.V., Sanin V.N., Krivenok A.G., Korolenko V.V.
|
| Vol 17, No 3 (2018) |
Development of a procedure for the synthesis of a micro gas turbine engine neural controller with account for fuel consumption constraints |
(Rus)
|
|
Kuznetsov A.V., Makaryants G.M.
|
| Vol 17, No 3 (2018) |
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines |
(Rus)
|
|
Ryzhkov V.V., Morozov I.I.
|
| Vol 17, No 3 (2018) |
Procedure and mathematical models for the validation of requirements to combat aircraft with account of ensuring its survivability and damage tolerance on exposure to means of destruction |
(Rus)
|
|
Sazhin A.N., Kovalchuk D.V., Kolodezhnov V.N., Malyshev V.A., Shatovkin R.R.
|
| Vol 17, No 3 (2018) |
Engines for domestic drones: past, present and future |
(Rus)
|
|
Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.
|
| Vol 17, No 2 (2018) |
Backstepping synthesis of the height control system of an unmanned aerial vehicle |
(Rus)
|
|
Akhramovich S.A., Barinov A.V., Malyshev V.V., Starkov A.V.
|
| Vol 17, No 2 (2018) |
Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method |
(Rus)
|
|
Balakin V.L., Ishkov S.A., Khramov A.A.
|
| Vol 17, No 2 (2018) |
Forecasting low-cycle fatigue life of gas-turbine engine parts by the method of equivalent tests for specimens with stress concentrator under extension-compression |
(Rus)
|
|
Bukatyy S.A., Pakhomenkov A.V., Solntsev G.A., Bukatyy A.S.
|
| Vol 17, No 2 (2018) |
Accuracy of autonomous navigation by the mutual method in the case of a group flight of space vehicles |
(Rus)
|
|
Golyakov A.D., Richnyak A.M.
|
| Vol 17, No 2 (2018) |
Assuring performance characteristics of gas-turbine engine parts and assemblies using electrospark doping |
(Rus)
|
|
Denisov L.V., Boytsov A.G., Siluyanova M.V.
|
| Vol 17, No 2 (2018) |
Computational investigation of aerodynamic and acoustic characteristics of an ultrahigh-bypass ratio counter-rotating fan |
(Rus)
|
|
Druzhinin Y.M., Mileshin V.I., Rossikhin A.A.
|
| Vol 17, No 2 (2018) |
Biological module “BiNOM” for cubesats of the SamSat family |
(Rus)
|
|
Zakharov V.P., Konyukhov V.N., Bakhtinov P.I., Molchkov E.V., Kornilin D.V., Konovalov S.G.
|
| Vol 17, No 2 (2018) |
Problematic issues of assessing the strength of axisymmetric parachute systems by conducting breakdown tests in flight experiments |
(Rus)
|
|
Ivanov P.I., Kurinnyy S.M., Krivorotov M.M., Shmerova G.V.
|
| Vol 17, No 2 (2018) |
Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft |
(Rus)
|
|
Igolkin A.A., Safin A.I., Filipov A.G.
|
| Vol 17, No 2 (2018) |
Determination of large-size liner impedance based on numerical simulation of sound propagation in a duct with specified azimuthal modal structure |
(Rus)
|
|
Korin I.A., Palchikovskiy V.V., Pavlogradskiy V.V.
|
| Vol 17, No 2 (2018) |
Improvement of friction units of power plants by aplying ceramic composite spray coatings |
(Rus)
|
|
Siluyanova M.V., Fertikov A.O.
|
| Vol 17, No 1 (2018) |
Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle |
(Rus)
|
|
Balakin V.L., Ishkov S.A., Khramov A.A.
|
| Vol 17, No 1 (2018) |
Determination of spacecraft antenna directivity pattern with the use of an Earth-based station |
(Rus)
|
|
Vasyutkina O.V., Vopilin A.V., Raduchev S.V., Khalilov R.R., Yakunin V.S.
|
| Vol 17, No 1 (2018) |
Inertial measuring units for future-generation aerospace products: fault-tolerance |
(Rus)
|
|
Vodicheva L.V., Bel'skiy L.N., Parysheva Y.V., Lystsov A.A.
|
| Vol 17, No 1 (2018) |
Estimation of systematic errors in the results of navigational measurements with the use of spacecraft robot onboard facilities |
(Rus)
|
|
Golyakov A.D., Richnyak A.M.
|
| Vol 17, No 1 (2018) |
Photoelectric converters in the power supply system of an atmospheric pseudo satellite |
(Rus)
|
|
Kovalyov M.A., Zelensky V.A., Nazarov A.A., Оvаkimyan D.N., Мirzoev R.M.
|
| Vol 17, No 1 (2018) |
Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate |
(Rus)
|
|
Kocherova E.E.
|
| Vol 17, No 1 (2018) |
Optimization of ducted counter–rotating fan blades on the basis of solving a 3d inverse problem with the aim of improving fan gasdynamic characteristics |
(Rus)
|
|
Mileshin V.I., Pankov S.V., Fateyev V.A., Shchipin S.K.
|
| Vol 17, No 1 (2018) |
Optimization of open counter – rotation fan blades on the basis of solving a 3D Navier-Stokes inverse problem with the aim of reducing tonal noise |
(Rus)
|
|
Mileshin V.I., Rossikhin A.A., Pankov S.V., Shchipin S.K.
|
| Vol 16, No 4 (2017) |
Application of open-source software for industrial problems of vehicle lift-off gas dynamics |
(Rus)
|
|
Abdurashidov T.O., Osipov A.V., Korchagova V.N., Kraposhin M.V., Smirnova Y.V., Strizhak S.V.
|
| Vol 16, No 4 (2017) |
Methodological and analytical support for the creation and maintenance of aerospace industry technological development strategic programs |
(Rus)
|
|
Gaponenko O.V.
|
| Vol 16, No 4 (2017) |
Сonceptual design of small spacecraft with a high resolution P-VHF band bistatic SAR system |
(Rus)
|
|
Goryachkin O.V., Maslov I.V., Zhengurov B.G.
|
| Vol 16, No 4 (2017) |
The use of gas-dynamic flame stabilization in afterburner combustion chambers of aircraft gas turbine engines |
(Rus)
|
|
Kolesnikov A.S., Pakhol'chenko A.A.
|
| Vol 16, No 4 (2017) |
Development of a new collector device for gas turbine engine afterburner |
(Rus)
|
|
Teslya D.N., Mayatsky S.A., Grasko T.V.
|
| Vol 16, No 3 (2017) |
Constructing 3D fan blade models in CAD-system on the basis of coordinate measuring techniques |
(Rus)
|
|
Arkhipov A.N., Ravikovich Y.A., Fedorov I.M., Kholobtsev D.P.
|
| Vol 16, No 3 (2017) |
Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization |
(Rus)
|
|
Balakin V.L., Ishkov S.A., Khramov A.A.
|
| Vol 16, No 3 (2017) |
Modeling external thermal influence of infrared radiation sources during tests of rocket and space equipment in VK-600/300 |
(Rus)
|
|
Dobritsa D.B., Ushakova A.A., Shabarchin A.F., Yashchenko B.Y.
|
| Vol 16, No 3 (2017) |
Influence of turbulence models on calculated values of aircraft aerodynamic properties |
(Rus)
|
|
Elisov N.A., Ishkov S.A., Shakhov V.G.
|
| Vol 16, No 3 (2017) |
Peculiarities of using additional low-power energy sources in the power supply system of small spacecraft |
(Rus)
|
|
Kargu D.L., Beznyakov A.M., Nemirov A.V., Radionov N.V., Chudnovsky Y.A.
|
| Vol 16, No 3 (2017) |
Estimation of functional efficiency of the air transport service system at a regional airport terminal |
(Rus)
|
|
Koltsov I.V., Romanenko V.A.
|
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