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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.
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.
Experimental research of thermal yet influence of staff LTRE upon the construction models of airspace devices
Shustov S.A.
Simulation of ultrashort pulse transmission in a chain of fused silica microspheres
Kozlova E.S.
Creation of the database for electrochemical processing with the purpose of optimization of process of the choice of electrolit
Smelov V.G., Shitarev I.L., Smirnov G.V.
Method for determining the energy of jets vibration waves
Limanova N.I., Levkin Y.S.
Evaluation of the possibility of using combustion promoters in hydrocarbon fuels for perspective jet engines
Petrukhin N.V., Sergeev S.M., Prokopenko O.A., Grek M.O.
Unit impulse input tests of a system of the «Frigate» upper-stage rocket
Mikhalenkov N.A., Yermakov V.Y., Utkina Y.I.
Increase of welded joints strength at welding nickel-based alloys by pulse laser influence
Murzin S.P., Tregub V.I., Nikiforov A.M.
Experimental researches of possible low-thrust rocket adaptation developed by FSUE R&DIME for bipropellant MON-3+MMH providing tolerable thermal state thrusters
Beshenev Y.A., Buldashev S.A., Kazankin F.A., Lemskiy N.V., Semkin Y.V.
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.
Diagnostics of state gas-fluid of flows in the field of cross vibration
Limanova N.I., Levkin U.S.
Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets
Ivanov I., Kryukov I., Shustov S.
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.
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Defining the specific impulse of mixed solid propellants
1 1., 1 1.
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.
Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft
Kurenkov V.I., Kucherov A.S., Yakishik A.A.
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.
Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Theoretical basis of directed energy transmission pulses in stationary and moving media
Skvortsov B.V., Skvortsov D.B., Malysheva–Strojkova A.N.
Hydrogenium saturation research for finishing pulsed electrochemical machining of titan alloy (BT9) TJ blades
Smirnov G.V.
1 - 22 of 22 Items

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