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	(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	(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	(Rus)
Vol 14, No 2 (2015)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Computational algorithm of forming program motion in a scheduled turn of small spacecraft	(Rus)
Vol 14, No 4 (2015)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Flight development tests and attempted operation of «AIST» small satellites	(Rus)
Vol 14, No 4 (2015)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Control of in-plane orbit parameters of a geostationary low-thrust satellite	(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	(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	(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	(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	(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	(Rus)
Vol 23, No 3 (2024)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Selection of design parameters of a spacecraft electric propulsion engine ensuring the geostationary orbit raising mission	(Rus)

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