Author Details

Salmin, V. V.

Issue Section Title File
Vol 12, No 4 (2013) ISSUE WITHOUT SECTION Spacecraft preset orbital parameters control by means of thrusters PDF
(Rus)
Vol 6, No 1 (2007) AIRCRAFT AND SPACE ROCKET ENGINEERING Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part I PDF
(Rus)
Vol 7, No 1 (2008) AIRCRAFT AND SPACE ROCKET ENGINEERING Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II PDF
(Rus)
Vol 14, No 2 (2015) AIRCRAFT AND SPACE ROCKET ENGINEERING Computational algorithm of forming program motion in a scheduled turn of small spacecraft PDF
(Rus)
Vol 14, No 4 (2015) AIRCRAFT AND SPACE ROCKET ENGINEERING Flight development tests and attempted operation of «AIST» small satellites PDF
(Rus)
Vol 14, No 4 (2015) AIRCRAFT AND SPACE ROCKET ENGINEERING Control of in-plane orbit parameters of a geostationary low-thrust satellite PDF
(Rus)
Vol 17, No 3 (2018) AIRCRAFT AND SPACE ROCKET ENGINEERING Refinement of operable state recovery algorithms for “AIST” small satellites on the basis of telemetric information PDF
(Rus)
Vol 17, No 4 (2018) AIRCRAFT AND SPACE ROCKET ENGINEERING Development of methods for ensuring energy balance for the operation of mission equipment of “AIST”-series small satellites under conditions of power limitations PDF
(Rus)
Vol 19, No 4 (2020) AIRCRAFT AND SPACE ROCKET ENGINEERING Choice of mission trajectory plans and conceptual design of electrical propulsion module for launching payloads into circumterrestrial orbits PDF
(Rus)
Vol 20, No 3 (2021) AIRCRAFT AND SPACE ROCKET ENGINEERING Analysis of characteristics of electric propulsion systems intended for carrying out maneuvers of maintenance of low Earth working orbit of small satellites PDF
(Rus)
Vol 21, No 4 (2022) AIRCRAFT AND SPACE ROCKET ENGINEERING Methodology of designing a space transport system including a “DM” chemical upper stage and an electric rocket transport module PDF
(Rus)

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