Comparative estimation of the accuracy of methods of autonomous navigation of small spacecraft in formation flying
Golyakov A.D., Richnyak A.M., Kalabin P.V.
Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing
Parovay E.F.
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.
Comparison of heat generation estimation methods for angular contact ball bearings
Petrov N.I., Lavrentyev Y.L.
Dynamic construction of the educational process in an integrated learning system
Grinberg G.M.
Theory and methods of designing machines with reduced vibroloading
Vasilyev A.V., Gleyzer A.I., Dmitriyev V.N., Prasolov S.G.
Quantitative ways of estimating the regional innovative potential
Tsapenko M.V.
Conceptually logical model of an integrated data system (software & hardware) for the control of individual and small-scale production of aviation components
Prilepsky I.V.
About elaboration diagnostic methods of elements the pneumohydrosystem productions
1 1., 1 1., 1 1.
Design of experiments for verification of computational life prediction methods
Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.
Statistical physics and cycles of operation of heat engines
Mikheenkov E.L.
Choice of design parameters of universal platforms of small space vehicles
Volotsuev V.V., Tkachenko I.S., Safronov S.L.
Realization of the multichannel cnc machining methods
1 1., 1 1.
Enhancement of efficiency of casting processes in production of parts of aircraft engines by way of action of pulse-magnetic field on melt
Chernikov D.G., Glouschenkov V.A., Igolkin A.J.
Common properties of hydrocarbon combustion products and Brayton cycle
Mikheenkov E.L.
Increasing process efficiency in the production of casting parts of aircraft engines by the action of pulsed magnetic field on the melt
Chernikov D.G., Glouschenkov V.A., Igolkin A.J., Nikitin K.V., Akishin S.A.
Solving the polynomial approximation problem with use of the iterative kachmazh method
Ivanov A.A.
Enhancement of efficiency of casting processes in production of parts of aircraft engines by way of action of pulse-magnetic field on melt
Chernikov D.G., Glouschenkov V.A., Igolkin A.J.
Stand for testing turbocharger rotor
Antipov V.A., Lazutkin G.V., Andrianov S.V., Velmin S.A.
Approaches to the evaluation of fuels for hypersonic engines
Sergeev S.M., Petrukhin N.V.
Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II
Salmin V.V., Vassiliev V.V., Ishkov S.A., Romanenko V.A., Sokolov V.O., Starinova O.L., Yurin V.V.
Experimental methods of carbon-based structures of nanotubs materials
Motova E.A., Moskvichev A.N.
Procedure of calculating efforts of blank stretching without corrugation in stretch forming
Dementyev S.G.
Features computer simulation cluster charactiristics electromagnetic converters
Merkulov A.I., Lavrov A.Y., Burkov D.S.
Automated restoration of gas turbine engine characteristics by experimental data
Botchkaryov S.K., Mosoulin V.V.
Use of ultra-small space vehicles for studying near-Earth plasma by radiophysical methods
Chugunin D.V., Chernyshov A.A., Mogilevsky M.M., Moiseenko I.L., Petrukovich A.A.
Assessment of changes in the sound-proof ability of the rocket fairing with layers of sound-proof materials varying in thickness
Popov P.A.
Method of reducing design aerodynamic characteristics to the results of drain tests of a transport category aircraft model
Bondar Y.I.
Identification of a gas turbine engine mathematical model by the ressults of testing
Botchkaryov S.K., Dmitriyev A.Y.
State of the art of theory and technology of incremental forming
Grechnikov F.V., Surudin S.V., Erisov Y.A., De Alvarenga R.
Convective current experiments using Dakon-P equipment onboard “Progress” cargo spacecraft
Ayukaeva D.M., Babushkin I.A., Belyaev M.Y., Zilberman Y.A., Matveeva T.V., Sidorov A.S.
On a method of practical training fulfillment for course of studies “Design of Main Units and Systems of Engine”
Borisov V.A., Zhizhkin A.M.
Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust
1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.
Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics
Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.
1 - 34 of 34 Items

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