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
deformation
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
structure
turbine
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Author Details
Author Details
Стратилатов, Н. Р.
Issue
Section
Title
File
Vol 12, No 4 (2013)
ISSUE WITHOUT SECTION
Choosing the place for the installation of navigation system aerials on the ERS spacecraft body
(Rus)
Vol 12, No 4 (2013)
ISSUE WITHOUT SECTION
Design of a dimensionally stable space telescope body adaptive to temperature gradients
(Rus)
Vol 12, No 4 (2013)
ISSUE WITHOUT SECTION
Influence of the reliability of Earth remote sensing spacecraft onboard systems on the monitoring of imaging periodicity
(Rus)
Vol 7, No 1 (2008)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Orbital tether system motion equations considering space vehicle vibrations
(Rus)
Vol 9, No 2 (2010): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Development of load – bearing frames of space telescopes with invariable dimensions adaptive to temperature gradients
(Rus)
Vol 11, No 4 (2012)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Selection of sites and angles for placing star coordinators of remote sensing satellites
(Rus)
Vol 15, No 2 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Metodological basis of the development of a problem-oriented system for selecting design parameters of space vehicles
(Rus)
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