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Vol 22, No 1 (2023)

The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review)

Alendar A.D., Lanshin A.I., Evstigneev A.A., Yakubovsky K.Y., Siluyanova M.V.

(Rus)

Vol 19, No 4 (2020)

Choice of mission trajectory plans and conceptual design of electrical propulsion module for launching payloads into circumterrestrial orbits

Salmin V.V., Kvetkin A.A., Russkikh A.S.

(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)

Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine

Kvetkin A.A., Kolesov A.V.

(Rus)

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

Salmin V.V., Volotsuev V.V., Nikitin A.V.

(Rus)

Vol 15, No 4 (2016)

Mathematical modelling of the working process of a hot gas pressure feed system

Salich V.L.

(Rus)

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

Problems development of nuclear electric propulsion

Belogurov A.I., Kolbaya T.C., Rachuk V.S.

(Rus)

Vol 20, No 1 (2021)

Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy

Sinitsin L.I., Belokonov I.V.

(Rus)

Vol 15, No 1 (2016)

Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit

Ishkov S.A.

(Rus)

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

Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS

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

(Rus)

Vol 10, No 6 (2011)

Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components

Titov B.A., Koltsov I.V.

(Rus)

Vol 12, No 1 (2013)

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

Bebyakov A.A.

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

Iodine as an alternative propellant for electrojet engines

Ostrovskiy V.G., Smolentsev A.A., Scherbina P.A.

(Rus)

Vol 12, No 2 (2013)

Adjustment of the pneumatic drive of a ground catapult to the permanent law of tractive force

Sereda V.A.

(Rus)

Vol 18, No 3 (2019)

Selection of project structure for nanosatellite propulsion system

Belokonov I.V., Ivliev A.V., Bogatyrev A.M., Kumarin A.A., Lomaka I.A., Simakov S.P.

(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 10, No 3-2 (2011): Special Issue

Prospects and problems of movement and power plants in powder metal fuel

Egorov A.G., Tizilov A.S.

(Rus)

Vol 13, No 5-3 (2014): Special Issue

Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft

Kurenkov V.I., Kucherov A.S., Yakishik A.A.

(Rus)

Vol 21, No 1 (2022)

On the efficiency of using the Navier-Stokes approximation in thermogasdynamic calculation of low-thrust liquid-propellant rocket engines at low Reynolds numbers

Maksimov A.D., Shustov S.A.

(Rus)

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

Ryzhkov V.V., Sulinov A.V.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

The use of electric engine to reduce the microaccelerations level of space lab

Sedelnikov A.V., Sygurova E.Y., Kireeva 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 16, No 4 (2017)

The use of gas-dynamic flame stabilization in afterburner combustion chambers of aircraft gas turbine engines

Kolesnikov A.S., Pakhol'chenko A.A.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

Comparative evaluation of the effectiveness of the application of perspective types of electric propulsion thrusters in the small spacecraft

Kulkov V.M., Obukhov V.A., Yegorov Y.G., Belik A.A., Krainov A.M.

(Rus)

1 - 25 of 25 Items

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