Specifics of generating explosively formed projectiles of variable shape from metal liners
Authors: Kruglov P.V., Kolpakov V.I., Bolotina I.A.
Issue: #12 (96)
DOI 10.18698/2308-6033-2019-12
Mechanics
Experimental verification of the algorithm for calculating the shell of an elasto-screw propulsion unit
Authors: Popkov M.V., Sorokin F.D., Briede S.A.
Procedure of training artificial neural network of elastic-damping characteristic control system of shock absorber landing gear struts of ground-based aircraft
Authors: Brusov V.A., Merzlikin Yu.Yu., Menshikov A.S.
Experimental study of the nature of the load distribution on the turns of the thread of the planetary roller-screw mechanism
Authors: Ryakhovskiy O.A., Marokhin A.S., Vorobyev A.N., Khachirova O.A.
Aviation and Rocket-Space Engineering
Experimental estimation of residual propellant in the fuel tanks with innertank capillary devices for spacecraft propulsion systems
Authors: Sapozhnikov V.B., Polyanskiy A.R., Korolkov A.V., Konstantinov S.B., Alexandrov L.G.
Analysing options of reducing power consumption of thermal condition maintenance processes in spacecraft at launch pads
Authors: Matveeva O.P., Romanyak A.Yu., Udovik I.S.
Calculating the periods of radio signal transmission between two spacecrafts through the Venus atmosphere in the problem of studying its composition
Authors: Fedyaev K.S., Noname , Bober S.A., Zubko V.A., Belyaev A.A.
Analytical construction of relay dynamic system point mappings taking into account delays
Authors: Simonyants R.P., Bulavkin V.N.