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Title
Authors
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.
Development and research testing of a low thrust on gaseous-propellant rocket engine chamber
Musteikis A.I., Levikhin A.A., Kolosenok S.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.
Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block
Ageenko Y.I., Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Mathematical model of small-thrust rocket engine with gaseous oxygen and hydrogen in pulse operation
1 1.
Research of the possibility of thermal conditions LREST using an infrared thermal imaging system
Ryzhkov V.V., Silyutin M.V.
Experimental research on the development of an “oxygen (gas) + kerosene” – fueled thruster
Salich V.L.
Method of transient simulation of combustion processes in a low-thrust rocket engine operating on gaseous hydrogen and oxygen
Zubanov V.M., Shabliy L.S., Stepanov D.V.
Working process of gaseous fuel metallizator
Pervyshin A.N., Ryazanov A.I.
Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits
Fadeenkov P.V., Ishkov S.A.
Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants
Silyutin M.V., Shustov S.A.
Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD
Ryzhkov V.V., Morozov I.I.
Locally optimal control of space tug motion between the libration points of the Earth-Moon system
Starinova O.L., Fain M.K.
Modeling of intrachamber processes in an oxygen-hydrogen thruster
Vaulin S.D., Salich V.L.
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.
Development of thruster chamber operating on oxygen-hydrogen fuel
Salich V.L.
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.
The numerical modelling of processes in combustion chambers of low thrust rocket engines
Salich V.L.
Research of liquid outflow from low-emission swirl injectors of a low-thrust liquid rocket engine
Semkin Y.V.
Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency
Ageenko Y.I., Ilyin R.V., Pegin I.V.
Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines
Ryzhkov V.V., Verjasov Y.N., Galperin R.N., Gulyaev Y.I., Ivashin Y.S.
The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies
Ryzhkov V.V.
Numerical simulation of low liquid flow in a mixer consisting of two centrifugal swirlers
Semkin E.V.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
1 - 25 of 25 Items

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