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
Тимбай, И. А.
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 12, No 4 (2013)
ISSUE WITHOUT SECTION
Determination of the maximum values of the spatial angle of attack of a nanosatellite in motion on lowcircular orbits
(Rus)
Vol 9, No 1 (2010)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Analysis of plane motion relative to the centre of mass of a descent capsule with the three-harmonic moment characteristics during its reentry
(Rus)
Vol 9, No 4 (2010)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Research of spatial motion of an uncontrolled spacecraft with the triharmonic moment characteristics around its center of mass during its reentry into atmosphere
(Rus)
Vol 9, No 4 (2010)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Deviation of reentry spacecraft from the estimated trajectory caused by transient modes of angular motion at the stage of entry into the atmosphere
(Rus)
Vol 9, No 4 (2010)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Research of planar motion of spacecraft around its center of mass under the influence of the gravitational and the aerodynamic moments during its descent from circular orbits
(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)
Vol 18, No 2 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Relative equilibria of dynamically symmetric CubeSat nanosatellite under the action of aerodynamic and gravitational torques
(Rus)
Vol 18, No 4 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Analysis of SamSat-218D nanosatelite motion acording to trajectory measurements
(Rus)
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