Underwater barrier deformation and destruction in the high-explosive and shaped charges blast
Authors: Ladov S.V.
Issue: #6 (138)
Mechanics
Wing model modal analysis in the airflow in conservative formulation
Authors: Naumov A.M., Domnina O.A.
Aviation and Rocket-Space Engineering
Membrane and vapor compression technologies use in the two-stage dehumidifying scheme of the rocket launch complex thermal regulation system
Authors: Barmin I.V., Kozlov V.V., Krylov P.V., Mikhaylova I.P.
Prospects for introducing propulsion system based on the flash evaporation in the rocket and space technology
Authors: Bechasnov P.M.
Weak links design for the main landing gear leg mount
Authors: Titov E.I., Serebryanskiy S.A.
Simulation of the aircraft landing gear legs with the plastically deformable shock absorbers
Authors: Sumerin A.A., Shcheglov G.A.
Results of experimental study of the thermal processes at forced convection of the MS-20 engine aviation oil
Authors: Altunin V.A., Lvov M.V., Yusupov A.A., Shchigolev A.A., Pukachev I.R., Yanovskaya M.L.
Overview of the distributed computational technologies used in construction of the advanced small spacecraft orbital constellations and ensuring their fail-safe and fault-tolerant operation
Authors: Asharina I.V., Grishin V.Yu., Sirenko V.G.