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
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
Author Details
Белоконов, И. 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
Selecting the conditions of nanosatellite separation from the upper stage of the arrier-rocket "Soyuz" in undirected flight
(Rus)
Vol 12, No 4 (2013)
ISSUE WITHOUT SECTION
Analysis of the influence of low-orbit nanosatellite uncontrolled motion on the possibility of solving navigation and communication problems after its separation from the «Soyuz» carrier rocket upper-stage
(Rus)
Vol 6, No 1 (2007)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Space vehicle attitude control recovery procedure combining magnetometric and padionavigation measurements
(Rus)
Vol 3, No 1 (2004)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Estimation of efficiency of controlling scientific experiments at autonomous microgravitational space platforms
(Rus)
Vol 5, No 1 (2006)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Problems of relational navigation in load transporation on helicopter external hanger
(Rus)
Vol 6, No 1 (2007)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Modelling the interaction of micrometeoroid and technogenous particles with a space vehicle
(Rus)
Vol 9, No 2 (2010): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent
(Rus)
Vol 11, No 4 (2012)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Analysis of uncontrolled motion of the “ Soyuz “ carrier rocket orbital stage after payload separation
(Rus)
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