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

Transport vehicle engineering - 629

Scientific articles

In section "Transport vehicle engineering"
The Nuclear Icebreaker Fleet and Its Role in the Economic Development of the Northern Sea Route
Aleksushin G.V.
Аpplication of the propulsion subsystem on the base of SPT-100V plasmic thruster to orbit raising and orbit control of the Express-80 and Express-103 spacecraft
Ermoshkin Yu.M., Vnukov A.A., Volkov D.V., Kochev Yu.V., Simanov R.S., Yakimov E.N., Grikhin G.S.
Flow model in the impeller of a centrifugal pump
Nazarov V.P., Chernenko V.V., Chernenko D.V.
Development of workspace and algorithms for testing SpaceWire onboard equipment
Maksyutin A.S., Myrygin A.V., Ivlenkov D.V., Dymov D.V.
Development of a model for detecting malfunctions during the maintenance of aircraft units and systems
Gusev E.V., Rodchenko V.V.
Alternative method of solar simulation for thermal vacuum tests of spacecraft
Shevchuk A.A.
Actuator made of a material with a shape memory effect for transformable space structures
Zimin V.N., Krylov A.V., Filippov V.S., Shakhverdov A.O.
Methodological principles of space vehicle design for the maximum energy supply of the payload
Chebotarev V.E., Fatkulin R.F., Vorontsova E.O., Shangina E.A., Balandina T.N.
Development of a methodology for testing SpaceWire network switches
Maksyutin A.S., Kazaykin D.S., Dymov D.V., Ivlenkov D.V.
Pressure measurement inside non-sealed equipment bay of the geostationary spacecraft
Mordovskiy S.A., Maksimov I.A., Ivanov V.V., Sitnikova N.N., Trofimchuk D.A.
The choice of the energy parameters of an oxygen-hydrogen propellant expander cycle rocket engine
Belyakov V.A.
Design of the fastening assembly of the guys on the power spokes reflector
Kolga V.V., Lykum A.I., Marchuk M.E., Filipson G.U.
The concept of an educational and scientific experiment for conducting on-orbit testing of any types of photovoltaic cell
Lukyanov M.M., Prokhorov G.P., Kutsenko V.S., Karpov E.S., Parshin A.S., Zuev D.M.
Methodological principles for the formation of a number of unified space communication satellite platforms
Chebotarev V.E., Zimin I.I., Vnukov A.A., Shangina E.A.
On the issue of hydrodynamic braking efficiency dur-ing high-velocity tests on a rocket-rail track
Astakhov S.A., Biryukov V.I., Kataev A.V.
Increasing the specific impulse of an oxygen-hydrogen liquid rocket engine by in-creasing heat transfer in the combustion chamber
Vasilevsky D.O.
Testing of spacecraft orientation and stabilization systems using starry sky simulators
Gorelko M.G., Murigin A.V.
Specialized LED assembly for out-atmospheric solar simulator
A. A. Shevchuk, V. V. Dvirnyi, M. S. Maybakh, S. A. San'ko, A. A. Pavlova
Experimental determination of vibration conductivity by rocket sled structural elements in high-speed track tests of aircraft equipment
Astakhov S.A., Biryukov V.I., Kataev A.V.
Studying static stability of a model rocket
Bordachev V.A., Kolga V.V., Rozhkova E.A.
Ground control system for distant space vehicle
А.O. Zhukov, K.A. Ivanov, M.K. Bondareva, M.N. Bondarev, D.S. Gorovoy
Evaluation of force-deformation characteristics of an actuator made of material with a shape memory effect for transformable space structures
Zimin V.N., Krylov A.V., Filippov V.S., Shakhverdov A.O.
The main provisions of the methodology for ensuring the resistance of the onboard equipment of spacecraft to the effects of the radiation effects of outer space
Maksimov I.A., Kochura S.G., Avdyushkin S.A.
The aircraft hydraulic system units and pipelines heat exchange parameters study
Nikolaev V.N.
Development of the CYCLOPS CubeSat payload
Sotnikova N.V., Kadadova A.V., Kadochnikov D.M., Utkin V.V.
Parametric analysis of the strength of a solid propellant rocket engine nozzle
Dogadkin V.A., Kolga V.V., Trukhin V.R.
Formation of an approach to modeling orbital operations assembly of a reconfigurable spacecraft on geostationary orbit
Y.L. Koroleva, A.I. Khokhlov, D.A. Nikolaev, N.V. Borisova, M.G. Matylenko
Ensuring the thermal regime of spacecraft structures
Shatrov A.K., Fisenko E.N., Rabetskaya O.I.
Evaluation of the main parameters of ReshUCube-1 telemetry over a period of 10 months in orbit
O.E. Shimova, D.M. Zuev, D.D. Velikanov, M.M. Luk'yanov, K.A. Mel'chukov
Calculation of the parameters and characteristics of a rotating lunar jet penetrator
E.V. Gusev, V.A. Zagovorchev, V.V. Rodchenko, E.R. Sadretdinova, E.A. Shipnevskaya
Features of reaching limiting speed values of track tests of ballistic type aircraft
Astakhov S.A.
Verification of thermodynamic parameters of a mixture of generator gas on oxygen-hydrogen fuel with an excess of one of the fuel components
V.A. Belyakov, D.O. Vasilevsky, D.V. Maslov, A.A. Kuleshov, R.V. Romashko
Study of the payload extraction trajectory heavy class carrier rocket
Bordachev V.A., Kolga V.V.
Ensuring durability and reliability of contact rings of current collection devices when working in elastic-plastic state
Grishin A.А.
Research of the motion parameters of a spaceplane entry of into the atmosphere
Kolga V.V., Runda N.S.
The birth of Siberian satellite construction
Akbulatov E.S.
Innovative technical solutions developed under the leadership of M. F. Reshetnev in the creation of the first Siberian launcher “Cosmos-3M”
Nazarov V.P., Golovenkin E.N., Piunov V.Yu.
Increasing the capabilities of a test ballistic missile to separate test objects
Minyaev S.I.
Development of an experimental unit and methodology for groundbased experimental testing of two-phase thermoregulation systems for spacecrafts
Khodenkov A.A., Delkov A.V.
Classification of defects of aviation display units
Antishin V.G., Kiselev S.К., Razumov I.А., Shorina D.S.
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