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
Крамлих, А. В.
Issue
Section
Title
File
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
Software and algorithmic support for the ground-based complex for small spacecraft attitude determination
(Rus)
Vol 6, No 1 (2007)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Space vehicle attitude control recovery procedure combining magnetometric and padionavigation measurements
(Rus)
Vol 11, No 4 (2012)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Adaptive algorithm of determining low altitude spacecraft orientation on the basis of processing instant diverse-type measurements
(Rus)
Vol 15, No 2 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
On-board algorithm for SamSat-218D nanosatellite orientation and stabilization system
(Rus)
Vol 18, No 2 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Determining the dynamics of spacecraft rotational motion with the use of information provided by global navigation satellite systems
(Rus)
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