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Vol 23, No 1 (2024)

Reducing energy consumption of vertical take-off and landing unmanned aerial vehicle using hybrid technical solutions

Lukyanov O.E., Hoang V.H., Komarov V.A., Nazarov D.V., Kurkin E.I., Quijada Pioquinto J.G., Chertykovtseva V.O.

(Rus)

Vol 23, No 1 (2024)

Mathematical model of a generalized quadcopter kinematic scheme and its software implementation

Zelenskiy V.A., Kovalev M.A., Ovakimyan D.N., Kirillov V.S.

(Rus)

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

Belyakov A.A., Prihodko V.I., Shulepov A.I.

(Rus)

Vol 21, No 4 (2022)

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.

(Rus)

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

Belyakov A.A., Shulepov A.I.

(Rus)

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

Komarov V.A., Lukyanov O.E., Hoang V.H., Kurkin E.I., QuijadaPioquinto J.G.

(Rus)

Vol 14, No 3 (2014)

Stochastic method of investigating perturbed motion of a space vehicle in the atmosphere

Sokolov N.L.

(Rus)

Vol 23, No 3 (2024)

Selection of design parameters of a spacecraft electric propulsion engine ensuring the geostationary orbit raising mission

Kolesov A.V., Salmin V.V.

(Rus)

Vol 23, No 2 (2024)

Automation of the process of testing on-board systems of unmanned aerial vehicles

Kirillov A.V., Sitnikov V.V., Tuchin A.L.

(Rus)

Vol 20, No 1 (2021)

Methodological support for the training of UAV designers and operators

Lukyanov O.E., Zolotov D.V.

(Rus)

Vol 17, No 4 (2018)

Analysis of control programs and flight paths of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 16, No 2 (2017)

Fluctuations of liquid fuel in tanks with oil recovery units

Dyachenko M.I., Duy Hung N., Temnov A.N.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

11D58MF combined propulsion unit operating on oxygen-hydrogen fuel for an average-sized booster

Lupyak D.S., Smolentsev A.A., Sokolov B.A., Tumanin E.N., Tupitsin N.N.

(Rus)

Vol 11, No 1 (2012)

Visual approach to verifictaion of real-time control software

Tyugashev A.A., Bogatov A.Y., Shulyndin A.V.

(Rus)

Vol 9, No 4 (2010)

Dynamic loading and questions of assuring the reliability of functioning of superheavy launch vehicle cryogenic pressure-operated valves

Sazanov V.P.

(Rus)

Vol 8, No 2 (2009)

Dependence of the extent to which the space vehicle’s own atmosphere and plasma generated by stationary plasma engines affect the space vehicle on its structural lay-out

Testoyedov N.A., Smirnov V.A.

(Rus)

Vol 12, No 4 (2013)

On-stand emergency protection and control system for propulsion tests of «Soyuz-2-1B» launch vehicle

Liseykin V.A., Tozhokin I.A.

(Rus)

Vol 19, No 4 (2020)

Determination of loads on perforated tank partition

Filipov A.G., Glazkov I.E.

(Rus)

Vol 17, No 3 (2018)

Engines for domestic drones: past, present and future

Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.

(Rus)

Vol 15, No 4 (2016)

Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks

Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.

(Rus)

Vol 11, No 7 (2012)

Calculation of the electromagnetic field in homogeneous hull of on board equipment of space vehicle under influence of electrostatic discharges

Kostin A.V.

(Rus)

Vol 13, No 2 (2014)

Calculation of power dissipation in corps of onboard equipment of space vehicle in direct electrostatic discharge

Kostin A.V.

(Rus)

Vol 9, No 2 (2010): Special Issue

Technical approach for estimation of engineering level of universal launch complexes for space launch vehicles witn use of overal parameter

1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 8, No 1 (2009)

Experiments aboard the space vehicle “Photon-M” NO.3 and some reseelts of the mission

Abrashkin V.I., Shatokhin S.M., Kovalyova T.B., Safronov S.L.

(Rus)

Vol 12, No 4 (2013)

Analysis of landing process dynamics for different reentry vehicle landing device support schemes

Borzykh S.V., Voronin V.V., Shchiblev Y.N.

(Rus)

Vol 19, No 3 (2020)

Improving the efficiency of the powerplant of an unmanned aerial vehicle through the use of cryogenic fuel

Kolesnikov A.S., Grasko T.V., Raznoschikov V.V.

(Rus)

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

Zinenkov Y.V., Lukovnikov A.V., Popov A.V., Nechaev V.N.

(Rus)

Vol 15, No 3 (2016)

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.

(Rus)

Vol 11, No 4 (2012)

Mathematical model of investigating normal acoustic modes of launch vehicle modules

Popov P.A., Belov A.S., Kryuchkov A.N.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Problems and prospect of microgasturbines development for unmanned aerial vehicle propulsion

Zhdanov I.A., Staudacher S., Falaleev S.V.

(Rus)

Vol 9, No 2 (2010): Special Issue

Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust

1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 7, No 1 (2008)

Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II

Salmin V.V., Vassiliev V.V., Ishkov S.A., Romanenko V.A., Sokolov V.O., Starinova O.L., Yurin V.V.

(Rus)

Vol 12, No 4 (2013)

Selecting the conditions of nanosatellite separation from the upper stage of the arrier-rocket "Soyuz" in undirected flight

Avaryaskin D.P., Belokonov I.V., Timbay I.A., Lagno O.G.

(Rus)

Vol 18, No 4 (2019)

Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control

Shorikov A.F., Kalev V.I.

(Rus)

Vol 17, No 2 (2018)

Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method

Balakin V.L., Ishkov S.A., Khramov A.A.

(Rus)

Vol 15, No 1 (2016)

Technologies of reducing the technological environmental impact of space rocket launches

Shatrov J.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y., Sitnikov D.V., Lempert D.B.

(Rus)

Vol 11, No 4 (2012)

Peculiarities of solving three-dimensional problems of flow about a launch vehicle with large nose fairings using the ANSYS FLUENT software

Kharitonova A.N., Shakhov V.G.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Generation of control programes for disposable unmanned aircraft vehicle propulsion system by means of dynamic characteristic

Mikhailov A.Y., Akhmedzyanov D.A., Akhmetov Y.M., Mikhailova A.B.

(Rus)

Vol 9, No 2 (2010): Special Issue

Experimental determination of acoustic loads daunches of Strela LV and calculation of test modes for a spacecraft to be delivered by it to space

1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 7, No 1 (2008)

Orbital tether system motion equations considering space vehicle vibrations

Aslanov V.S., Stratilatov N.R.

(Rus)

Vol 18, No 4 (2019)

Application of differential evolution algorithm in the problem of aeroassisted orbital plane change maneuver

Elisov N.A., Ishkov S.A., Khramov A.A.

(Rus)

Vol 17, No 1 (2018)

Photoelectric converters in the power supply system of an atmospheric pseudo satellite

Kovalyov M.A., Zelensky V.A., Nazarov A.A., Оvаkimyan D.N., Мirzoev R.M.

(Rus)

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

Kuznetsov U.L., Ukraintsev D.S.

(Rus)

Vol 11, No 4 (2012)

Peculiarities of Earth observation space vehicle control in contingencies

Akhmetov R.N., Makarov V.P., Sollogub A.V.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Hard & soft complex for “Angara” family launch vehicles engine system development

Partola I.S.

(Rus)

Vol 8, No 4 (2009)

Vibration resistance problem for a space vehicle with single-degree-of-freedom powered gyroscopes

Filippov Y.I., Peresypkin K.V.

(Rus)

Vol 7, No 1 (2008)

Choosing the form of space vehicle designed for descent in the rarefied atmosphere of Mars

Aslanov V.S., Ledkov A.S.

(Rus)

Vol 21, No 3 (2022)

Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle

Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.

(Rus)

Vol 18, No 3 (2019)

Justification of the architecture of an interactive information model of the process of space-mission vehicle launch preparation

Privalov A.E., Bugaichenko P.Y.

(Rus)

Vol 17, No 1 (2018)

Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle

Balakin V.L., Ishkov S.A., Khramov A.A.

(Rus)

Vol 10, No 7 (2011)

The analysis of methods of protection of onboard equipment of space vehicles from influence of factors of the electrostatic discharge

Kostin A.V.

(Rus)

Vol 13, No 1 (2014)

Constructive actions for decreasing the acoustic pressure inside space-rocket products

Popov P.A., Sindyukov A.A.

(Rus)

Vol 8, No 4 (2009)

History of small space vehicle progress and development at Plesetsk cosmodrome. Current problems of further development

Korotkov V.V., Vinogradov A.V.

(Rus)

Vol 12, No 1 (2013)

Optimal control of the angle of attack of a hypersonic flight vehicle

Bebyakov A.A.

(Rus)

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

Tremkina O.V., Uglanov D.A., Urlapkin V.V., Korneev S.S., Komisar Y.V.

(Rus)

Vol 18, No 2 (2019)

Disturbed motion of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 16, No 3 (2017)

Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization

Balakin V.L., Ishkov S.A., Khramov A.A.

(Rus)

Vol 10, No 4 (2011)

Method for calculating shipping costs in transporting heterogeneous cargo

Saveliev G.L.

(Rus)

Vol 11, No 2 (2012)

Choice of design parameters of universal platforms of small space vehicles

Volotsuev V.V., Tkachenko I.S., Safronov S.L.

(Rus)

Vol 10, No 2 (2011)

Determination of mass-power propertions for parametric range of launch vehicle modifications

Baranov D.A., Yelenev V.D.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

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.

(Rus)

Vol 12, No 2 (2013)

Current state of the theory and practice of circuit wiring control and testing of the avionics of rocket fairings of middle-class launch vehicles

Koptev A.N., Gulyaev A.A.

(Rus)

Vol 20, No 3 (2021)

Laser-scanning rangefinder fixed on a gimbal with two degrees of freedom

Zelenskiy V.A., Kapalin M.V.

(Rus)

Vol 18, No 1 (2019)

Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle

Khramov A.A.

(Rus)

Vol 16, No 2 (2017)

Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments

Popov P.A., Sindyukov A.A., Malykhina O.I.

(Rus)

Vol 14, No 1 (2015)

Study of characteristics of the launch vehicle fuel line gas damper

Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.

(Rus)

Vol 11, No 2 (2012)

Principles of constructing systems and objects of a middle-class space rocket complex with increased load-carrying capacity

Baranov D.A., Yelenev V.D., Smorodin A.V.

(Rus)

Vol 10, No 1 (2011)

Definition of directions of developing methods, technical decisions and means of decreasing the technogenic influence on the environment for the omplementation on board of space launch vehicles

Shatrov Y.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

Use of the mathematical tool of hypervector ranging for selection energy-power plant of flight vehicles

Safronov V.V., Zhebrakov A.S.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

System of pressurization of the fuel tank of a launch vehicle using the heat of generator gas

Biryuk V.V., Smorodin A.V., Shepelev A.I., Onoprienko D.A.

(Rus)

1 - 70 of 70 Items

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