A method for selecting design parameters of a small spacecraft de-orbiting system
Authors: Krestina A.V., Tkachenko I.S.
Issue: #8 (104)
Aviation and Rocket-Space Engineering
Parametric study of ramjet engine thrust characteristics
Authors: Voronetskiy A.V., Smolyaga V.I., Abramov M.A., Miroshnichenko S.A.
An experimental space-purpose solar cell with a carbon fiber honeycomb frame: features of development and test results
Authors: Naumova A.A., Lebedev A.A., Vagapova N.T., Kagan M.B., Sineva M.V.
A method for selecting parameters of drives for lifting erectors and transportation and installation units for space rockets
Authors: Igritsky V.A., Igritskaya A.Yu., Zverev V.A.
An algorithm for controlling the spatial motion of a spacecraft with an imperfectly reflecting solar sail based on the laws of locally optimal control for Earth — Mars heliocentric flight
Authors: Khabibullin R.M., Starinova O.L.
Ensuring non-collision and safe distancing of a large number of spacecraft when launched by the Fregat upper stage
Authors: Simonov A.V., Morskoy I.M., Gordienko E.S., Vorobyov A.L., Paul V.G.
A modern approach to the design of foreign landing parachute systems
Authors: Ploskov S.Yu.
Methods of substantiating the quantitative composition and estimating the values of reliability indicators of technical objects of aircraft computer network
Authors: Zhurbin S.A., Kazakov G.V., Koryanov V.V.
Analysis of the performance of electrodynamic tethers with autonomous electron generation
Authors: Bechasnov P.M.
Metallurgy and Science of Materials
Acoustic emission as an information factor of dissipative processes in metal cutting
Authors: Yakubov Ch.F., Kim V.A., Bashkov O.V., Komkova T.Yu.