Author Details

Салмин, В. В., Самарский государственный аэрокосмический университет имени академика С.П. Королёва (национальный исследовательский университет), Russian Federation

Issue	Section	Title	File
Vol 12, No 4 (2013)	ISSUE WITHOUT SECTION	Spacecraft preset orbital parameters control by means of thrusters	(Rus)
Vol 5, No 1 (2006)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Simulating thermal fields of complex closed structure aboard research space laboratory	(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 9, No 2 (2010): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	The design shape and basic performances of small satellite of SSAU and SRP SRC “TSSKB-Progress”	(Rus)
Vol 9, No 2 (2010): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust	(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)