Scientific articles \ Applied sciences. Medicine. Technology \ Engineering. Technology in general

Transport vehicle engineering - 629

Scientific articles

In section "Transport vehicle engineering"
Approach to select of universal vibratory system
Semenova L.A., Lysenko E.A., Lysenko K.E.
Increase of efficiency of gas distribution in the accelerating channel of an electrojet engine
Gopanchuk V.V., Zhasan V.S., Potapenko M. Yu.
Use of methods of nondestructive test for exposure of corrosion damage of the airframe structure with account of corrosive damage criteria
Katsura A.V.
Complex systems reliability calculation task solution method with variable aggregates breakdown stream parameters
Shaymardanov L.G., Boyko O.G.
Theoretical bases of compositing technique of light streams from separate sources of radiation for SC land working off
Krat S.A.
Solution of a problem of support of the decision to be made by a crew team when an emergency situation occurs wile in flight
Lukasov V.V., Nikushkin N.V.
Dynamic synthesis of DC load with energy recuperation into power network of spacecraft power supply system test complex
Mizrakh E.A., Lobanov D.K.
Determination of the adhesive-bonded joint parameters durian honeycomb panels manufacturing
Mikhnev M.M., Ishenina N.N., Nagovitsin V.N.
Perfection of technology of application of sheetings on frames of SC by microarc oxidation
Mikheev A.E., Girn A.V., Khartov V.V., Vakhteev Е.В., Evkin I.V.
Electroarc hardening of titanic alloys
Mikheev A.E., Girn A.V., Ivasev S.S., Kudymov V.I.
Calculating and analytical method of choosing envelopes of metal for processing power-generating set components by stock removal
Kraev V.V., Krushenko G.G.
Problems of optimization of software of on-board radio-electronic equipment
Zharikov V.N., Pichkalev A.V.
Experimental study of radiotransparent thermal control coating for application in sunshields antennas
Chernyatina A.A., Kharlamov V.A., Ermolaev R.A., Parshin A.S., Alexandrova G.A.
Development of the methodology of electric thermal vacuum testing for temperature control of small spacecraft Jubelee-2 (MIR)
Vshivkov A. Yu., Golovenkin E.N., Krat S.A., Ganenko S.A.
Features of experimental definition of composite materials durability against erosive impact of stationary plasma thrusters
Nadiradze A.B., Rachmatullin R.R., Kochura S.G., Maksimov I.A., Smirnov V.А.
Method and criterion of selective assembly of wave gear drives of solar batteries of space vehicles
Prudnikov O.P., Tyulevin S.V., Nazarov D.V.
Flight safety risk analysis statistical method
Shaymardanov L.G., Boyko O.G., Lyubimcev A.V.
Mathematical modeling of gas-liquid flow in microchannels of various geometry under chemical reactions, friction and heat exchange
Yakutin A.V., Kolomentsev A.I.
Methods for high-accuracy measurements of precision structures for mobile automatic spacecraft in thermal vacuum conditions
Dvirniy G.V.
Distinctive features of maintenance of flawlessness of nonreusable mechanical devices functioning on space vehicles
Pokhabov Yu. P.
Theoretical justification of algorithm of determination of aircraft rotating mass moments
Ushakov N.U.
Method of reliability estimation of complicated systems, calculation of which cannot be reduced to a serial-parallel element connection scheme
Furmanova E.A., Boyko O.G., Shaimardanov L.G.
Analysis of software for automatic performance of spacecraft tests
Khasanova R.A.
About domestic system of space monitoring of emergencies
Testoedov N.A., Dvirnyj V.V., Nosenkov A.A., Elfimova M.V.
Calibration of measuring path for ECM test of navigation equipment of customers of satellite radio navigation systems
Tyapkin V.N., Fateev Y.L., Dmitriev D.D., Konnov V.G.
Technique for calculation and selection of spacecraft electric heaters parameters under uncertainty conditions
Chebotarev V.E., Zvonar V.D., Fatkulin R.F., Dmitriev G.B.
Experimental research of loading device of recuperation type
Lobanov D.K., Mizrakh E.A.
Loading device of recuperation type with improved dynamic characteristics
Mizrakh E.A., Lobanov D.K.
Development and thermal vacuum tests of heat shields for protection of mechanical electric drive unit from effect of “solar trap”
Vshivkov A. Yu., Tanasienko F.V., Golovenkin E.N., Yurtaev E.V.
Methodological bases of estimation of systemic action of additional payload on spacecraft functioning
Kislitskiy M.I.
Influence of calendar time on fatigue resistance of bolt-riveted joints of aircrafts
Katsura A.V., Krushenko G.G.
Estimation of the form of a large-sized transformed reflector surface for a spacecraft
Goldobin N.N.
Questions of development of a standard program of certified tests of electric radio products of foreign manufacture applied in domestic spacecrafts of long functioning
Matyushev R.A., Patraev V. Yu.
Rate making and development of spacecraft onboard equipment to mechanical environment
Orlov S.A., Kopytov V.I.
Airplanes functional systems reliability calculation method
Furmanova E.A., Boyko O.G.
Dynamical workbench for signature analysis and operating conditions of flywheel engine group of pointing and attitude control systems of spacecrafts
Synitskiy D.E., Murygin A.V.
Simulation modeling of the main components of motion control system of the satellite
Yelubayev S.A., Jamalov N.K., Alipbayev K.A., Sukhenko A.S., Bopeyev T.M.
Bus-modular system for test of onboard radioelectronic equipment
Krasnenko S.S., Nedorezov D.A., Kashkin V.B., Pichkalev A.V.
About the accuracy of systems reliability definition with statistic methods
Furmanova E.A., Boyko O.G.
Analysis of the dynamic performance of the pointing and attitude control subsystem of the resilient spacecraft with power gyroscopic unit on the basis of GD 02-150 gyrodyne
Yakimov E.N., Raevskiy V.A., Lukyanenko M.V.
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