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Authors
Investigation of 11D428А-22 thruster operation dynamics with bellows flow stabilizer
Beshenev Y.A., Volkov A.V., Kazankin F.A.
Influence of complex loading of radial bearings of the oscillation groups of liquid propellant engine steering gear on the frictional moment
Balyakin V.B., Lavrin A.V., Dolgikh D.E.
Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing
Egorychev V.S.
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
Balakin V.L., Krikunov M.M.
Investigation of transformation of intermediate products of liquid-phase interaction propellant at the onset of combustion for rocket engine
Nigodjuk V.E., Sulinov A.V.
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.
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.
Optimal command control of flight paths of aerospace system hypersonic first stage in conditions of atmospheric disturbances
Krikunov M.M.
Mathematical modelling of the working process of a hot gas pressure feed system
Salich V.L.
Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent
1 1., 1 1., 1 1., 1 1.
Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control
Shorikov A.F., Kalev V.I.
Method of calculating the thickness of the combustion chamber of a liquid rocket engine made with the use of innovative technologies and materials
Krivonogov A.V.
Defining the specific impulse of mixed solid propellants
1 1., 1 1.
Disturbed motion of the hypersonic first stage of an aerospace system in climb
Balakin V.L., Krikunov M.M.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
Mathematical model of small-thrust rocket engine with gaseous oxygen and hydrogen in pulse operation
1 1.
Investigation of the kinetic properties of gas products of liquid-phase interaction hypergolic liquid rocket fuel
Nigodjuk V.E., Sulinov A.V.
Vortex cleaning of fuel tank pressurant gas
Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.
Мethod of design calculation of centrifugal emulsive duplex fuel nozzle
1 1.
Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing
Egorychev V.S.
Iodine as an alternative propellant for electrojet engines
Ostrovskiy V.G., Smolentsev A.A., Scherbina P.A.
1 - 21 of 21 Items

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