Specific features of mathematical modeling of ceramic plates destruction under the influence of high-speed impactors
Authors: Petukov A.V., Grin K.A.
Issue: #12 (120)
DOI 10.18698/2308-6033-2021-12
Mechanics
Aviation and Rocket-Space Engineering
A method of forming a spacecraft adapter layout to meet the requirements of dynamic compatibility by topological and parametric optimization methods
Authors: Borovikov A.A., Tushev O.N.
Low-orbit spacecraft for highly detailed observation with a long lifetime in working orbits with an altitude below four hundred kilometers
Authors: Volotsuev V.V.
Feasibility evaluation of using additive technologies in aerospace products
Authors: Shemonaeva E.S., Goncharov A.V., Andreev V.D.
Analysis of temperature measuring error in high-temperature ceramic samples with various methods of thermocouple fixing
Authors: Nikonova V.D., Yuldashev Z.N., Denisov O.V., Denisova L.V.
On the S-25 anti-aircraft missile system. Part 1
Authors: Metelsky A.O., Markov V.A., Pusev V.I.
Numerical study of the influence of the physicochemical liquid fuel properties on the efficiency of the low-thrust rocket engine working process
Authors: Novikov A.V., Andreev E.A., Bardakova E.I.
Analysis of the trajectory of spacecraft return from the lunar surface to a given region of the Earth
Authors: Konstantinov M.S., Nikolichev I.A., Thant Aung Myo
Investigation of UWB RF signal technology for solving indoor positioning problem
Authors: Novichkov A.R., Goncharov I.K., Egorushkin A.Yu., Faschevsky N.N.