| Issue |
Title |
File |
| Vol 23, No 3 (2024) |
Development of the numerical differentiation method for approximating pitch acceleration using sensor fusion approach |
(Rus)
|
|
Korsun O.N., Goro S., Om M.H.
|
| Vol 23, No 3 (2024) |
Automation of conceptual design and modification of aircraft type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 1: Methods and models |
(Rus)
|
|
Komarov V.A., Lukyanov O.E., Hoang V.H., Kurkin E.I., QuijadaPioquinto J.G.
|
| Vol 23, No 3 (2024) |
Selection of design parameters of a spacecraft electric propulsion engine ensuring the geostationary orbit raising mission |
(Rus)
|
|
Kolesov A.V., Salmin V.V.
|
| Vol 23, No 3 (2024) |
Estimating the design parameters of a space-based radio surveillance system |
(Rus)
|
|
Ivanushkin M.A., Zhaldybina O.D., Safronov S.L., Korovin M.D.
|
| Vol 23, No 3 (2024) |
Selection of aerodynamic characteristics and engine parameters of a maneuverable aircraft under epistemic uncertainty |
(Rus)
|
|
Veresnikov G.S., Ogorodnikov O.V.
|
| Vol 23, No 2 (2024) |
Method of first-approximation calculation of take-off weight of a light aircraft with a hybrid propulsion system |
(Rus)
|
|
Sychev A.V., Arbuzov I.V., Ravikovich Y.A.
|
| Vol 23, No 2 (2024) |
Aircraft electric power plants |
(Rus)
|
|
Kondryakov A.D., Leontiev M.K.
|
| Vol 23, No 2 (2024) |
Reliability-oriented design of PCM thermodimensionally stable space structures |
(Rus)
|
|
Klimakova L.A.
|
| Vol 23, No 2 (2024) |
Comparative results of computational and theoretical study of the annular nozzle with a flat central body |
(Rus)
|
|
Kirshina A.A., Levikhin A.A., Kirshin A.Y.
|
| Vol 23, No 2 (2024) |
Automation of the process of testing on-board systems of unmanned aerial vehicles |
(Rus)
|
|
Kirillov A.V., Sitnikov V.V., Tuchin A.L.
|
| Vol 23, No 2 (2024) |
Increasing the efficiency and stability of fuel supply to the combustion chamber of a liquid rocket engine by spray nozzles |
(Rus)
|
|
Ageenko Y.I., Bubnova A.S.
|
| Vol 23, No 1 (2024) |
Verification of aero-engine numerical rotor models based on virtual static structural and modal tests |
(Rus)
|
|
Shaposhnikov K.V., Degtyarev S.A., Leontiev M.K., Anisimov S.V.
|
| Vol 23, No 1 (2024) |
Optimization of trajectory motion of the first stage of an aerospace system |
(Rus)
|
|
Khramov A.A.
|
| Vol 23, No 1 (2024) |
Main approaches and features of the design of aircraft hydro-mechanical control systems |
(Rus)
|
|
Petrov P.V., Tselischev V.A., Kuderko D.A.
|
| Vol 23, No 1 (2024) |
Analysis and improvement of characteristics of power supply systems for the small space vehicle of the AIST-2 type |
(Rus)
|
|
Mordanov M.R., Safronov S.L.
|
| Vol 23, No 1 (2024) |
Reducing energy consumption of vertical take-off and landing unmanned aerial vehicle using hybrid technical solutions |
(Rus)
|
|
Lukyanov O.E., Hoang V.H., Komarov V.A., Nazarov D.V., Kurkin E.I., Quijada Pioquinto J.G., Chertykovtseva V.O.
|
| Vol 23, No 1 (2024) |
Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface |
(Rus)
|
|
Kovalev V.V., Marchenko A.D., Starostina T.V., Sharipova A.R.
|
| Vol 23, No 1 (2024) |
Mathematical model of a generalized quadcopter kinematic scheme and its software implementation |
(Rus)
|
|
Zelenskiy V.A., Kovalev M.A., Ovakimyan D.N., Kirillov V.S.
|
| Vol 22, No 4 (2023) |
Theoretical aspects of designing the components of an aircraft onboard cable network |
(Rus)
|
|
Myasnikov A.Y.
|
| Vol 22, No 4 (2023) |
Optimization of the parameters of a ground speed meter of low-flying aircraft based on the application of the theory of optimal filtration |
(Rus)
|
|
Ivanov M.E., Yezerskiy V.V.
|
| Vol 22, No 4 (2023) |
Methodology of delivering space parts, tools and accessories to a near Earth orbital station on the basis of the reliability factor |
(Rus)
|
|
Zheleznov I.V., Uperchuk R.A., Eroshenko V.K.
|
| Vol 22, No 4 (2023) |
Designing an active electronically scanned array as part of onboard equipment of a high-speed radio communication channel |
(Rus)
|
|
Zhdanov E.R., Slavyanskiy A.O., Kharina O.S., Shpack A.V.
|
| Vol 22, No 4 (2023) |
Features of the use of directional fixed antennas of a high-speed radio link on a small spacecraft AIST-2T |
(Rus)
|
|
Eremina V.V., Erkov I.O., Zhuravlev A.A., Maslov I.V., Pyrinov N.I.
|
| Vol 22, No 4 (2023) |
Algoritms for determining the attitude position of an unmanned aerial vehicle relative to the landing platform by using computer vision |
(Rus)
|
|
Gainutdinova T.Y., Novikova S.V., Gainutdinov V.G., Trusfus M.V., Litvin V.M.
|
| Vol 22, No 4 (2023) |
JSC “ODK” experience in implementing digital twin technologies in the design of gas turbine engines |
(Rus)
|
|
Vinogradov K.A., Nikulin A.S., Shmotin Y.N.
|
| Vol 22, No 4 (2023) |
Method of automated arrangement of devices in a spacecraft compartment taking into account connection to interface connectors of feed-through plates of an on-board cable system |
(Rus)
|
|
Belyakov A.A., Prihodko V.I., Shulepov A.I.
|
| Vol 22, No 3 (2023) |
Bench tests of an electric engine-propeller group, as the first stage in the creation of a hybrid power plant |
(Rus)
|
|
Sychev A.V., Ravikovich Y.A., Borisov D.A.
|
| Vol 22, No 3 (2023) |
Assessment of the possibility of shortening the landing distance of maneuverable aircraft |
(Rus)
|
|
Strelets M.Y., Tarasov A.Z., Grishin I.A.
|
| Vol 22, No 3 (2023) |
Features of design calculation of compressor spool flow path of a twin-shaft gas turbine engine core on the basis of 1D and 2D models of their working process |
(Rus)
|
|
Matveev V.N., Goriachkin E.S., Popov G.M., Baturin O.V., Kudryashov I.A.
|
| Vol 22, No 3 (2023) |
Determining aerodynamic characteristics of small unmanned aerial vehicles involving flight experiment |
(Rus)
|
|
Lukyanov O.E., Zolotov D.V., Espinosa Barsenas O., Komarov V.A.
|
| Vol 22, No 3 (2023) |
Models for determining the orientation of the solar battery of an observation spacecraft relative to the Sun during object survey and retargeting |
(Rus)
|
|
Kurenkov V.I., Pupkov E.A.
|
| Vol 22, No 3 (2023) |
Modal analysis of a spacecraft solar panel |
(Rus)
|
|
Kryuchkov A.N., Safin A.I., Ermilov M.A., Vidyaskina A.N., Igolkin A.A., Ye. V. Shakhmatov Y.V.
|
| Vol 22, No 3 (2023) |
Classification and comparative analysis of methods for limiting technogenic pollution in the near-Earth space |
(Rus)
|
|
Klyushnikov V.Y., Zakharova A.P., Usovik I.V.
|
| Vol 22, No 3 (2023) |
Digital model of the drag force of the Earth’s upper atmosphere for the design of low-orbit spacecraft |
(Rus)
|
|
Volotsuev V.V.
|
| Vol 22, No 3 (2023) |
Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine |
(Rus)
|
|
Belonozhkin V.V., Teslya D.N.
|
| Vol 22, No 2 (2023) |
Simulating the process of retargeting of optoelectronic Earth observation spacecraft during object shooting |
(Rus)
|
|
Kurenkov V.I., Pupkov E.A., Kucherov A.S.
|
| Vol 22, No 1 (2023) |
Survey of the flight efficiency of a long-haul aircraft under uncertainty of tasks |
(Rus)
|
|
Markiewicz P.
|
| Vol 22, No 1 (2023) |
The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review) |
(Rus)
|
|
Alendar A.D., Lanshin A.I., Evstigneev A.A., Yakubovsky K.Y., Siluyanova M.V.
|
| Vol 21, No 4 (2022) |
Methodology of designing a space transport system including a “DM” chemical upper stage and an electric rocket transport module |
(Rus)
|
|
Russkikh A.S., Salmin V.V.
|
| Vol 21, No 4 (2022) |
Optical characteristics of a multilayer solar sail and their effect on its heliocentric motion |
(Rus)
|
|
Rozhkov M.A.
|
| Vol 21, No 4 (2022) |
Calculation of aircraft lever-float valves using neural networks |
(Rus)
|
|
Pushkarev D.O., Kiselev D.Y., Kiselev Y.V.
|
| Vol 21, No 4 (2022) |
Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor |
(Rus)
|
|
Panchenko S.L., Gras’ko T.V.
|
| Vol 21, No 4 (2022) |
Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine |
(Rus)
|
|
Kvetkin A.A., Kolesov A.V.
|
| Vol 21, No 4 (2022) |
Basic aspects of topological technology of automated on-board equipment layout in space vehicle compartments using the example of “Yantar-2k” Earth remote sensing space vehicle |
(Rus)
|
|
Belyakov A.A., Shulepov A.I.
|
| Vol 21, No 3 (2022) |
Procedure of assessing the error of the device for measuring mass-centering and inertial characteristics of nanosatellites using reference objects |
(Rus)
|
|
Vasin P.V., Barinova E.V.
|
| Vol 21, No 3 (2022) |
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle |
(Rus)
|
|
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
|
| Vol 21, No 3 (2022) |
Two-channel optimal discrete law of control of spacecraft with aerodynamic and inertial asymmetry during descent in Mars atmosphere |
(Rus)
|
|
Lyubimov V.V., Bakry I.
|
| Vol 21, No 3 (2022) |
Gas-dynamic losses in the flow part of the channel charge of a solid-propellant rocket engine |
(Rus)
|
|
A. N. Sabirzyanov A.N., Khamatnurova C.B., Kuzmin V.V.
|
| Vol 21, No 3 (2022) |
Kinetic model and kerosene surrogate for calculating gas turbine engine emission of carcinogenic hydrocarbons |
(Rus)
|
|
Semenikhin A.S., Idrisov D.V., Chechet I.V., Matveev S.G., Lukachev S.V.
|
| Vol 21, No 3 (2022) |
Formation of a rotating ring-shaped three-body tethered nanosatellite system with limited control |
(Rus)
|
|
Chen S., Zabolotnov Y.M.
|
| Vol 21, No 2 (2022) |
Validation of the “stage – diffuser” system numerical study and its use for design modernization |
(Rus)
|
|
Cherkasova M.G., Semakina E.Y., Chernikov V.A.
|
| Vol 21, No 2 (2022) |
Standardization of diagnostic indicators of gearbox teeth wear in aircraft gas-turbine engines |
(Rus)
|
|
Sunduckov A.Y., Shakhmatov Y.V.
|
| Vol 21, No 2 (2022) |
3D investigation of heat exchange and hydrodynamics of high pressure turbine nozzle block platforms with different cooling schemes |
(Rus)
|
|
Gorelov Y.G., Ananyev V.V., Zolotuhina D.A.
|
| Vol 21, No 2 (2022) |
Justification of geometric parameters of the engine air particle separator |
(Rus)
|
|
Gishvarov A.S., Rakhimov A.R.
|
| Vol 21, No 1 (2022) |
Influence of space vehicle remote power supply on thermal regimes of solar batteries |
(Rus)
|
|
Steganov G.B., Beznyakov A.M., Nemirov A.V.
|
| Vol 21, No 1 (2022) |
Isotopy of spacecraft compartment hull shapes |
(Rus)
|
|
Belyakov A.A., Shulepov A.I.
|
| Vol 20, No 4 (2021) |
Selection of the optimum configuration and calculation studies of the parameters of a cryogenic propulsion system for an unmanned aerial vehicle |
(Rus)
|
|
Tremkina O.V., Uglanov D.A., Urlapkin V.V., Korneev S.S., Komisar Y.V.
|
| Vol 20, No 4 (2021) |
Choice of gas temperature at the turbopump turbine inlet |
(Rus)
|
|
Ivanov A.V.
|
| Vol 20, No 4 (2021) |
Specific features of pressure pulsation control in combustion chambers of land based gas turbine units |
(Rus)
|
|
Skiba D.V., Maksimov D.A., Kashapov R.S., Kharisov T.S.
|
| Vol 20, No 4 (2021) |
Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics |
(Rus)
|
|
Tishchenko K.O., Brykov N.A., Belyaeva A.S.
|
| Vol 20, No 4 (2021) |
The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies |
(Rus)
|
|
Ryzhkov V.V.
|
| Vol 20, No 4 (2021) |
Special aspects of numerical simulation of a two-stage axial-flow compressor with defective blades |
(Rus)
|
|
Blinov V.L., Zubkov I.S., Iskortsev E.Y., Belyaev O.V., Plishkin P.I.
|
| Vol 20, No 3 (2021) |
Analysis of characteristics of electric propulsion systems intended for carrying out maneuvers of maintenance of low Earth working orbit of small satellites |
(Rus)
|
|
Salmin V.V., Volotsuev V.V., Nikitin A.V.
|
| Vol 20, No 3 (2021) |
Estimation and analysis of the influence of ionizing radiation on the operation of nanosatellite onboard radio electronic equipment |
(Rus)
|
|
Tsaplin S.V., Bolychev S.A.
|
| Vol 20, No 3 (2021) |
Analysis of basic concepts of advanced engines for supersonic civil aircraft on the basis of foreign designers’ experience |
(Rus)
|
|
Alendar A.D., Grunin A.N., Siluyanova M.V.
|
| Vol 20, No 3 (2021) |
Laser-scanning rangefinder fixed on a gimbal with two degrees of freedom |
(Rus)
|
|
Zelenskiy V.A., Kapalin M.V.
|
| Vol 20, No 3 (2021) |
Experimental studies of the components of high-frequency ion engine RD0310 |
(Rus)
|
|
Kazbanov A.A., Dronov P.A., Spivak O.O., Derkachev A.B.
|
| Vol 20, No 3 (2021) |
Introduction to the problem of calculating the parameters of the mixing chamber of an afterburning bypass engine |
(Rus)
|
|
Karev O.D.
|
| Vol 20, No 3 (2021) |
Design and development of combustion chambers for gas turbine engines based on calculations of various levels of complexity |
(Rus)
|
|
Aleksandrov Y.B., Nguyen T.D., Mingazov B.G.
|
| Vol 20, No 2 (2021) |
Mathematical model of acoustic characteristics of polyurethane foam used for sound absorption in aerospace engineering |
(Rus)
|
|
Kuznetsov A.V., Igolkin A.A., Safin A.I., Pantyushin A.O.
|
| Vol 20, No 2 (2021) |
Deployment and stabilization of the motion of a space tethered system in a lunar orbit |
(Rus)
|
|
Ledkova T.A., Zabolotnov Y.M.
|
| Vol 20, No 2 (2021) |
Three-dimensional inhomogeneous thermal fields of the “Photon-Amur 2.0” payload electronic board developed for nanosatellites |
(Rus)
|
|
Fomin D.V., Barulinа M.A., Golikov A.V., Strukov D.O., German A.S., Ogorodnikov A.A.
|
| Vol 20, No 2 (2021) |
Designing of control and expulsion equipment for the pitot-static system of passenger airplanes |
(Rus)
|
|
Zotin N.A., Lisman E.P.
|
| Vol 20, No 2 (2021) |
Optimal design of sandwich floor panels made of high-strength composite materials considering stiffness constraints |
(Rus)
|
|
Komarov V.A., Pavlova S.A.
|
| Vol 20, No 2 (2021) |
Calculation of flow characteristics of liquid fuel supplied through pressure jet atomizers of small-sized gas turbine engines |
(Rus)
|
|
Gurakov N.I., Zubrilin I.A., Hernandez Morales M., Yakushkin D.V., Didenko A.A., Matveev S.G., Komisar Y.V.
|
| Vol 20, No 2 (2021) |
System of differential equations of aircraft spatial motion dynamics with arbitrary tensor of inertia and center of gravity position |
(Rus)
|
|
Vereshchikov D.V.
|
| Vol 20, No 1 (2021) |
Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy |
(Rus)
|
|
Sinitsin L.I., Belokonov I.V.
|
| Vol 20, No 1 (2021) |
Algorithm for solving optimal open-loop terminal control problem for spacecraft rendezvous with account of constraints on the state |
(Rus)
|
|
Shorikov A.F., Goranov A.Y.
|
| Vol 20, No 1 (2021) |
Mathematical model of turbofan engine weight estimation taking into account the engine configuration and size |
(Rus)
|
|
Avdeev S.V.
|
| Vol 20, No 1 (2021) |
Methodological support for the training of UAV designers and operators |
(Rus)
|
|
Lukyanov O.E., Zolotov D.V.
|
| Vol 19, No 4 (2020) |
Designing of minimum mass airframes under several loadings |
(Rus)
|
|
Danilin A.I.
|
| Vol 19, No 4 (2020) |
Development of improved performance electromagnetic valve for liquid rocket engine |
(Rus)
|
|
Igolkin A.A., Chubenko T.A., Maksimov A.D.
|
| Vol 19, No 4 (2020) |
Choice of mission trajectory plans and conceptual design of electrical propulsion module for launching payloads into circumterrestrial orbits |
(Rus)
|
|
Salmin V.V., Kvetkin A.A., Russkikh A.S.
|
| Vol 19, No 4 (2020) |
Investigation of the characteristics of the component of vibration of gas turbine engine gearbox that causes fatigue failures of its structural elements in case of tooth flank wear |
(Rus)
|
|
Sundukov A.E.
|
| Vol 19, No 4 (2020) |
Determination of loads on perforated tank partition |
(Rus)
|
|
Filipov A.G., Glazkov I.E.
|
| Vol 19, No 4 (2020) |
The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters |
(Rus)
|
|
Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.
|
| Vol 19, No 3 (2020) |
Method of coordinating joint operation of air starter and auxiliary power unit and determining the gas turbine engine starting time |
(Rus)
|
|
Popov G.M., Baturin O.V., Novikova Y.D., Zubanov V.M., Volkov A.A., Korneeva A.I.
|
| Vol 19, No 3 (2020) |
Disturbed transatmospheric motion of the first stage of an aerospace system |
(Rus)
|
|
Krikunov M.M.
|
| Vol 19, No 3 (2020) |
Design of control moment gyro electric drive with strict requirements on ensuring desired rotational velocities |
(Rus)
|
|
Polozhentcev D.S., Davidov A.A., Shipov M.G., Kazakov E.P., Malykh B.I.
|
| Vol 19, No 3 (2020) |
Improving the efficiency of the powerplant of an unmanned aerial vehicle through the use of cryogenic fuel |
(Rus)
|
|
Kolesnikov A.S., Grasko T.V., Raznoschikov V.V.
|
| Vol 19, No 2 (2020) |
Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter |
(Rus)
|
|
Ananenko V.M., Golyakov A.D., Kalabin P.V.
|
| Vol 19, No 2 (2020) |
Conceptual framework of designing complex bundles of aircraft on-board cable network |
(Rus)
|
|
Koptev A.N., Myasnikov A.Y.
|
| Vol 19, No 2 (2020) |
Optimal command control of flight paths of aerospace system hypersonic first stage in conditions of atmospheric disturbances |
(Rus)
|
|
Krikunov M.M.
|
| Vol 19, No 2 (2020) |
Gas turbine engine dynamic model based on variable-memory LSTM architecture |
(Rus)
|
|
Kuznetsov A.V., Makaryants G.M.
|
| Vol 19, No 1 (2020) |
Using signals from the gas-turbine engine shaft speed sensor in the diagnosis of the technical condition of its reduction gearbox |
(Rus)
|
|
Avramenko A.A., Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.
|
| Vol 19, No 1 (2020) |
Algorithm for predicting the vibrational state of a turbine rotor using machine learning |
(Rus)
|
|
Bolotov M.A., Pechenin V.A., Pechenina E.J., Ruzanov N.V.
|
| Vol 19, No 1 (2020) |
Control over maintaining accuracy of integrity of reference surfaces of spacecraft components in their joint functioning at various stages of design |
(Rus)
|
|
Yelenev V.D., Schuplyak Y.P.
|
| Vol 19, No 1 (2020) |
Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances |
(Rus)
|
|
Krikunov M.M.
|
| Vol 19, No 1 (2020) |
Method of calculating dynamic designs of space launch vehicles for designing systems of stabilization of their motion |
(Rus)
|
|
Lobanov V.A.
|
| Vol 19, No 1 (2020) |
Optimizing the process of changing spacecraft orbital parameters by using a spinning electrodynamic tether sytem |
(Rus)
|
|
Lu H., Wang C., Zabolotnov Y.M.
|
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