VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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Combustion chamber
Gas turbine engine
Mathematical model
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algorithm
blade
combustion chamber
design
efficiency
experiment
finite element method
gas turbine engine
mathematical model
mathematical modeling
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
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)
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