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Title
Authors
Experimental research of staff LTRE with hypergolic propellant under impulse engaging conditions
Shustov S.A.
Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets
Ivanov I., Kryukov I., Shustov S.
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.
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.
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.
Design procedure of fundamental parameters of the direct-flow detonation pulsing engine
Porshnev V.A.
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.
Possibility of using a bi-directional impulse turbine in a thermo-acoustic engine
Dovgjallo A.I., Shimanov A.A.
Influence of impulse generation mode on electro-erosion treatment
1 1., 1 1., 1 1., 1 1.
Optimizing the process of changing spacecraft orbital parameters by using a spinning electrodynamic tether sytem
Lu H., Wang C., Zabolotnov Y.M.
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.
Formation of the sliding surface mechanical seal different methods
Tarelnik V.B., Martsinkovskiy V.S., Antoshevskiy B.
Approbation of the numerical model of account of viscosity impact on the flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with sliding
Shustov S.A.
Experimental research of thermal yet influence of staff LTRE upon the construction models of airspace devices
Shustov S.A.
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.
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.
1 - 20 of 20 Items

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