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
Spacecraft
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 национальный исследовательский университет имени академика С.П. Королёва, Russian Federation
Issue
Section
Title
File
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)
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