Innovative device for low-trauma installation and extraction of the monospiral esophageal stent
Authors: Sayapin S.N.
Issue: #10 (166)
DOI 10.18698/2308-6033-2025-10
Mechanics
Aviation and Rocket-Space Engineering
Analyzing design parameters of the foreign small-lift launch vehicles
Authors: Bechasnov P.M.
Study of a rotating tethered space system depending on the tether tension force
Authors: Ekimovskaya A.A., Ermakov V.Yu., Tufan A.
Methodology to determine the rational integrity level in design and development of the helicopter airframe assembly constructed using polymer composite materials
Authors: Kisin I.D., Zavalov O.A.
Numerical simulation in determining parameters of the model of damage accumulation in the composite material monolayer
Authors: Akulin P.V., Turbin N.V., Dudchenko A.A.
Methodology for comparative assessment of the mixer efficiency in the model channels
Authors: Novoselov K.I., Zakharov V.S.
Development of the automated tools for registering the fuel ignition and flameout moments using the visual analysis methods
Authors: Yanuk A.V., Tarasenko A.N., Panov E.N.
Experimental study results of the electrostatic fields influence on sedimentation process in the MS-20 aviation motor oil under conditions of its forced convection in the annular channel
Authors: Altunin V.A., Lvov M.V., Altunin K.V., Yusupov A.A., Shchigolev A.A., Yanovskaya M.L.