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Authors
Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments
Popov P.A., Sindyukov A.A., Malykhina O.I.
Designing an active electronically scanned array as part of onboard equipment of a high-speed radio communication channel
Zhdanov E.R., Slavyanskiy A.O., Kharina O.S., Shpack A.V.
Methodology of designing a space transport system including a “DM” chemical upper stage and an electric rocket transport module
Russkikh A.S., Salmin V.V.
Issues of evolution of rotor piston engines’ subject abroad and in Russia
Kocherov E.P., Kononov V.A., Okorochkov V.V., Okorochkova V.M., Ivanova K.P.
Model of the main worm of milling cutters for gear cutting
Androsov S.P., Brailov I.G., Vizigin D.V.
Modeling external thermal influence of infrared radiation sources during tests of rocket and space equipment in VK-600/300
Dobritsa D.B., Ushakova A.A., Shabarchin A.F., Yashchenko B.Y.
Computer simulation of forming operations of the magnetic-pulse processing of metals
Grechnikov F.V., Chernikov D.G.
The design shape and basic performances of small satellite of SSAU and SRP SRC “TSSKB-Progress”
1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.
Increasing the efficiency of rotary piston engines by the use of the diesel cycle
Okorochkov V.V., Okorochkova V.M., Ravodin A.I.
Operate reliability enhancement of thermogenerator modules for heat engine with acoustic emission method
1 1.
Method of accelerated test research soldered joints surface mount devices
Nasedkin A.V.
Module of storing information: combining the functions of authorizing access and transfer of information within the control system equipment
Hanevsky D.A., Solovieva N.V., Ananyin A.S., Shchepochkin I.N.
Significance and directions of development of rotary piston area of research
Okorochkov V.V., Okorochkova V.M., Shafranov V.V.
Two-channel optimal discrete law of control of spacecraft with aerodynamic and inertial asymmetry during descent in Mars atmosphere
Lyubimov V.V., Bakry I.
Development of automated software module for modelling of forming part of electrochemical GTE
Nekhoroshev M.V., Pronichev N.D.
Choice of mission trajectory plans and conceptual design of electrical propulsion module for launching payloads into circumterrestrial orbits
Salmin V.V., Kvetkin A.A., Russkikh A.S.
Working conditions analysis of rotor supports bearings in aviation gas turbine engines and energetic units structure
Zrelov V.A., Makarchuk V.V., Prodanov M.E., Sudarev A.A.
1 - 17 of 17 Items

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