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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.
Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine
Kvetkin A.A., Kolesov A.V.
Prospects and problems of movement and power plants in powder metal fuel
Egorov A.G., Tizilov A.S.
System-mathematical simulation of engine air hydraulic power supply
Goryunova N.R., Goryunov A.A.
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.
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.
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.
Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft
Kurenkov V.I., Kucherov A.S., Yakishik A.A.
Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy
Sinitsin L.I., Belokonov I.V.
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.
Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control
Shorikov A.F., Kalev V.I.
Forecasting the individual performance capabilities of the rocket engine powerplant units at the maintanance stage
Biryuk V.V., Bronshtein V.M., Presnyakova A.S., Shatilova M.Y., Dostovalova S.S.
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.
Problems development of nuclear electric propulsion
Belogurov A.I., Kolbaya T.C., Rachuk V.S.
Hard & soft complex for “Angara” family launch vehicles engine system development
Partola I.S.
Mathematical modelling of the working process of a hot gas pressure feed system
Salich V.L.
The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage
Ivanov V.P., Partola I.S.
1 - 17 of 17 Items

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