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Vol 23, No 3 (2024)

Methodical and algorithmic aspects of mathematical modeling of a screw aircraft power plant

Zinenkov Y.V.

(Rus)

Vol 22, No 3 (2023)

Comparison of quasi-three-dimensional and full three-dimensional formulations of thrust bearing operation

Sokolov N.V., Khadiev M.B., Fedotov P.E., Fedotov E.M.

(Rus)

Vol 22, No 3 (2023)

Digital model of the drag force of the Earth’s upper atmosphere for the design of low-orbit spacecraft

Volotsuev V.V.

(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 23, No 3 (2024)

Development and research testing of a low thrust on gaseous-propellant rocket engine chamber

Musteikis A.I., Levikhin A.A., Kolosenok S.V.

(Rus)

Vol 23, No 2 (2024)

Comparative results of computational and theoretical study of the annular nozzle with a flat central body

Kirshina A.A., Levikhin A.A., Kirshin A.Y.

(Rus)

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

Firing test stand pulse detonation low-thrust engines

Govorenkho G.S., Teterin D.P., Kotelnikhov D.S., Aliluev A.V., Aliluev S.V., Fedorets V.N.

(Rus)

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

Ageenko Y.I., Bubnova A.S.

(Rus)

Vol 23, No 1 (2024)

Optimization of trajectory motion of the first stage of an aerospace system

Khramov A.A.

(Rus)

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

Design procedure of fundamental parameters of the direct-flow detonation pulsing engine

Porshnev V.A.

(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 8, No 4 (2009)

Elastic metal-plastic thrust bearings for combined hydraulic units of pumped storage hydroelectric power stations

Baiborodov Y.I.

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

The numerical modelling of processes in combustion chambers of low thrust rocket engines

Salich V.L.

(Rus)

Vol 14, No 4 (2015)

Control of in-plane orbit parameters of a geostationary low-thrust satellite

Salmin V.V., Chetverikov A.S.

(Rus)

Vol 8, No 4 (2009)

Full-scale tests of superloaded thrust bearings for hydraulicturbine generators of Sibir hydroelectric power stations of the new generation with unit power of 1 million kw

Baiborodov Y.I.

(Rus)

Vol 12, No 2 (2013)

Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200

Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.A.

(Rus)

Vol 20, No 3 (2021)

Three-dimensional periodic thermoelastichydrodynamic modeling of hydrodynamic processes of a thrust bearing

Sokolov N.V., Khadiev M.B., Fedotov P.E., Fedotov E.M.

(Rus)

Vol 14, No 3-1 (2015): Special Issue

Method of investigating the elastohydrodynamic contact in slide bearings with compressible and incompressible lubrication

Temis M.J.

(Rus)

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

Development of advanced low thrust rocket engines with ecologically friendly propellants

1 1., 1 1., 1 1.

(Rus)

Vol 12, No 4 (2013)

The usage of high power supply capacity transport spacecraft

Ivanovich S.N.

(Rus)

Vol 18, No 4 (2019)

Optimal control of spacecraft motion in the vicinity of Eros 433 asteroid

Shornikov A.Y.

(Rus)

Vol 17, No 4 (2018)

Programs of time-optimal control in the problem of rendezvous transfer of spacecraft with low transversal thrust

Ishkov S.A., Filippov G.A., Fadeenkov P.V.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage

Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.

(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 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 17, No 4 (2018)

Оptimization of gas turbine aircraft engine control throughout the engine service life

Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.

(Rus)

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

Numerical modeling on dynamic process of injection in supersonic part of the nozzle

Yakovchuk M.S.

(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 10, No 3-4 (2011): Special Issue

Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber

Silyutin M.V., Shustov S.A.

(Rus)

Vol 17, No 3 (2018)

Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(Rus)

Vol 10, No 2 (2011)

Optimum programs of correction of quasielliptical and circular orbits of spacecraft with the limited-thrust engine

Khramov A.A.

(Rus)

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

Research of the possibility of thermal conditions LREST using an infrared thermal imaging system

Ryzhkov V.V., Silyutin M.V.

(Rus)

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

Philippov G.A.

(Rus)

Vol 10, No 1 (2011)

Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits

Fadeenkov P.V., Ishkov S.A.

(Rus)

Vol 7, No 1 (2008)

System of artificial intellect support of low-thrust spacecraft interplanetary mission optimization

Starinova O.L.

(Rus)

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

Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants

Silyutin M.V., Shustov S.A.

(Rus)

Vol 16, No 3 (2017)

Locally optimal control of space tug motion between the libration points of the Earth-Moon system

Starinova O.L., Fain M.K.

(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)

1 - 40 of 40 Items

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