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Development and research testing of a low thrust on gaseous-propellant rocket engine chamber
Musteikis A.I., Levikhin A.A., Kolosenok S.V.
Research of laws of interaction of components in a liquid phase self-igniting liquid rocket fuel
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.
Residual stresses distribution regularities in the smallest section of hardened hollow cylindrical detail with circular cut
Sazanov V.P., Larionova Y.S., Kolychev S.A.
Developing an electronic reference book on thermogasodynamic properties of rocket engine fuel combustion products taking into account non-ideal character of the working process
Silyutin M.V.
Peculiarities of the working process of low-thrust hypergolic-propellant liquid rocket engines with a thrust of less than 1 N
Nigodjuk V.E., Sulinov A.V.
Study of residual strained state components distribution in the smallest section of superficial hardened part with a circular cut by finite-elements modeling method
Sazanov V.P.
The phase characteristic of force cutting and its role in occurrence and development of self-oscillations at sharpening not rigid details of aviation engines
Burmistrov E.V., Basyrov M.N., GiniyatuIIin R.R.
Prospects of application of additive technologies to develop parts and components of gas turbine engines and ramjets
Magerramova L.A., Nozhnitsky Y.A., Volkov S.A., Volkov M.E., Chepurnov V.Z., Belov S.V., Verbanov I.S., Zaikin S.V.
FPGA using in systems of automated frequency distribution
Grushin P.I., Loginov V.I., Yampurin N.P.
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.
Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components
Shustov S.A.
Mistakes analysis of multicoordinate processing on the machine tools with the numerical control by program
Ismaylova E.Y.
Procedure of creating three-dimensional solid models of tool electrodes for electrochemical pulse machining of gas turbine engine parts in CAD-systems with their parametric coupling with software module profiling
Nekhoroshev M.V., Pronichev N.D., Smirnov G.V.
The interactive system for collecting data of technical condition of aircraft components
Blagorazumov A.K., Kirpichev I.G.
Working process of gaseous fuel metallizator
Pervyshin A.N., Ryazanov A.I.
Forecasting and optimization of supplies in case of demand fluctuations
Gorlach B.A., Saveliev G.L.
Impulse noise of digital-to-analog converters and its influence on the purity of the spectrum of digital synthesizers
Izmaylova Y.A.
Test bench for investigation of thrusters intra-chamber working processes
Pervyshin A.N., Ryazanov A.I.
Functional components of the model of pedagogical activity of a distance learning teacher
Belousov A.I., Gromova T.V.
Design build process for the accuracy of eligibility
Grechnikov F.V., Tlustenko S.F.
Automated profiling of tool electrode in electrochemical pulse machining
Nekhoroshev M.V., Pronichev N.D., Smirnov G.V.
The analysis of influence of parameters of the spectrum of maxima on efficiency of allocation modulating components of vibration of gas turbine engine
Sundukov A.E., Sundukov E.V., Nikolaev V.A.
Increasing the energy efficiency of liquid rocket engine of small thrust (0,1-1,0) N with jet scheme of mixing
Nigodjuk V.E., Sulinov A.V.
Fracture resistance criteria implementation while securing reliability of airplanes structural components during design stage
Tarasov Y.L.
Influence of width of the filter on characteristics of discrete components of the spectrum of vibration of gas turbine engine
Sundukov A.E., Nikolaev V.A., Sundukov E.V.
1 - 26 of 26 Items

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