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Complex of algorithms for fast determination of the parameters of motion of high-speed vessels in the digital signal processing system of a space synthetic aperture radar
Gusev S.N., Moroz A.V.
Experimental research of the closed-type gas-dynamic mixer
Lepeshinsky I.A., Reshetnikov V.A., Zarankevich I.A., Istomin E.A., Antonovsky I.V., Guzenko A.A.
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
Balakin V.L., Krikunov M.M.
Modeling orbital tether system deployment with limitations on the deployment speed
Ishkov S.A., Filippov G.A., Xiaoye X.
Resonant method of accelerating non-magnetic materials
Syomkin N.D., Piyakov A.V., Voronov K.Y., Sukhachev K.I.
Experimental simulation of registration of outer space objects
Baryshev Y.Y., Syomkin N.D., Voronov K.Y.
Process of coating the inner surface of an inclined pipe and its mathematical modeling
Skvortsov B.V., Zaretskaya M.I., Zaretskiy I.S., Zhivonosnovskiy P.A.
Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit
Ishkov S.A.
Analysis and ballistic design of a medium-caliber system with an attached camera of accelerating
Safronov A.I., Azovsky V.M., Zorkin V.A., Chirkunova N.V.
Flame propagation velocity and ionization in burning gasoline and methane with addition of hydrogen
Shaykin A.P., Ivashin P.V., Galiev I.R.
Numerical modeling and experimental research of a two-phase liquid- gas ejector with a profiled supersonic nozzle
Lepeshinsky I.A., Reshetnikov V.A., Zarankevich I.A.
Method and apparatus for evaluating the efficiency of energy transfer from combustion products to abrasive particles at the exit of a sand blaster nozzle
Kornilin D.V., Medvedev M.V.
Optimal distribution of turboprop engine free energy between the screw and the jet with mass characteristics taken into account
Grigoriev V.A., Prokaev A.S.
Conditions of compatibility of compressor and turbine used as part of a gas generator required to ensure turbine operability
Grigoriev A.V., Ilyushin M.Y., Mitrofanov V.A., Rassokhin V.A., Rudakov O.A., Solovieva A.V.
Dependence of methane laminar flame propagation speed on the pressure and initial temperature
Lukachev S.V., Matveev S.G., Zubrilin I.A., Sigidaev A.V.
The concept of matching the joint operation of the combustion chamber, the compressor and the turbine
Grigoriev A.V., Golubchikov P.P., YIlushin M.Y., Rudakov O.A., Solovieva A.V.
Experimental study of air flow in axisymmetric diffuser output section with rotating wall
Kurkin E.I., Ivchenko A.V.
Influence of fluctuation velocity on the electric conductivity of hydrocarbon flames
Shajkin A.P., Galiev I.R., Bobrovsky A.V.
Research of current and power interchange of swirled fluid streams in a hydraulic heat gentrator
Belozertsev V.N.
Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine
1 1., 1 1.
Gas-dynamic losses in the flow part of the channel charge of a solid-propellant rocket engine
A. N. Sabirzyanov A.N., Khamatnurova C.B., Kuzmin V.V.
Determination of the conditions of nanoporous structures formation in metal materials by pulse-periodic laser treatment
Murzin S.P.
Assessing weight efficiency of carrier rockets launched from dirigibles and airplanes
Kurenkov V.I.
System of differential equations of aircraft spatial motion dynamics with arbitrary tensor of inertia and center of gravity position
Vereshchikov D.V.
Procedure of estimating characteristics of angular velocity meter using the Kalman filter and Allan variance
Kutovoy D.A., Maslova O.I., Perepelkina S.Y., Tiunov Y.S., Fedotov A.A.
Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine
Ishkov S.A., Filippov G.A.
Numerical model of viscosity impact on flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with velocity slip
Shustov S.A.
Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
Ananenko V.M., Golyakov A.D., Kalabin P.V.
Analysis of the accuracy of Earth remote sensing satellite angular motion control and track guidance during route observation intervals
Galkina A.S., Platoshin I.V.
Theoretical basis of directed energy transmission pulses in stationary and moving media
Skvortsov B.V., Skvortsov D.B., Malysheva–Strojkova A.N.
Active noise control systems based on acoustic particle velocity measurements
Gasparov M.S., Kharitonov M.Y.
1 - 31 of 31 Items

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