Experimental and computational determination of dynamic parameters of stretchable cables
Authors: Reshetnikov D.E., Kozhevnikov A.N., Matveev K.A.
Issue: #6 (162)
Mechanics
Aviation and Rocket-Space Engineering
Weight efficiency of the anisogrid circular cylindrical shells exposed to transverse bending and internal pressure
Authors: Zheleznov L.P.
Random response analysis of preloaded metal designs using the MSC Nastran software package. Part 1
Authors: Shulga A.A., Alikin N.A., Barysheva D.V.
Modeling the working process in the chamber and calculating the characteristics of a low-thrust rocket engine working on the oxygen-methane gaseous propellant components with the 50 N thrust
Authors: Vorozheeva O.A., Koptev I.I., Yagodnikov D.A.
Computational study of the thermal state of a low-thrust rocket engine chamber operating on the gaseous propellant components taking into account the axial heat leaks along the combustion chamber fire wall
Authors: Novikov A.V., Andreev E.A., Bardakova E.I.
Studying the influence of the low-thrust spacecraft launch date on energy costs in the Earth–Moon system transfer
Authors: Kuvshinova E.Yu.
Motion dynamics of a satellite with the inflatable braking device during its descent from the low-Earth orbit
Authors: Khalyavka N.S., Prosuntsov P.V.