On-board algorithm for SamSat-218D nanosatellite orientation and stabilization system - PDF (Russian)
Copyright (c) 2016 VESTNIK of the Samara State Aerospace University
Copyright (c) 2016 VESTNIK of the Samara State Aerospace University
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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Keywords
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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Keywords
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
Copyright (c) 2016 VESTNIK of the Samara State Aerospace University