On contribution of the shaped charge jet tail elements in penetrating a target
Authors: Fedorov S.V.
Issue: #12 (132)
DOI 10.18698/2308-6033-2022-12
Mechanics
Mathematical modeling of loss of stability of local delaminations caused by high-speed impact
Authors: Bokhoeva L.A., Baldanov A.B., Rogov V.E.
Optimal use of supports in interposing a pipeline into the submerged crossing well. Part 1
Authors: Ovchinnikov N.T.
Semi-empirical analysis of the initial stage of the growth of the deception point beyond the shock wave front
Authors: Andreev S.G.
Aviation and Rocket-Space Engineering
Study of the aircraft aerodynamic characteristics at entering the clear-air turbulence zone and the flight safety issues
Authors: Vyshinsky V.V., Zoan K.T.
Influence of the design of a separable junction between the grid composite adapter and the spacecraft hull on their natural oscillation frequencies
Authors: Eremenko A.A., Azarov A.V.
Product thermal regime determination on the Moon surface taking into account the specular-diffuse reflection
Authors: Borschev N.O., Deniskina A.R., Emelyanov A.Yu.
Development of a method for temperature calculation of the multi-fuel nozzle inner wall based on heat flux
Authors: Altunin K.V.
Scientific Conferences
Ballistic evaluation of the Apollo missions to the Moon
Authors: Kazakov G.V., Ponomarev S.A., Seleznev K.V.