VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
Menu
Archives
Home
About the Journal
Editorial Team
Editorial Policies
Author Guidelines
About the Journal
Issues
Search
Current
Articles in press
Retracted articles
Archives
Contact
Subscriptions
All Journals
User
Username
Password
Remember me
Forgot password?
Register
Search
Search
Search Scope
All
Authors
Title
Abstract
Index terms
Full Text
Browse
By Issue
By Author
By Title
By Sections
Other Journals
Keywords
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
×
User
Username
Password
Remember me
Forgot password?
Register
Search
Search
Search Scope
All
Authors
Title
Abstract
Index terms
Full Text
Browse
By Issue
By Author
By Title
By Sections
Other Journals
Keywords
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
Home
>
Search
>
Author Details
Author Details
Belokonov, I. V.
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 6, No 1 (2007)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Modelling the interaction of micrometeoroid and technogenous particles with a space vehicle
(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 1, No 1 (2002)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Dynamics and motion control of aerospace and space-rocket systems
(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)
Vol 18, No 3 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Selection of project structure for nanosatellite propulsion system
(Rus)
Vol 18, No 4 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Analysis of SamSat-218D nanosatelite motion acording to trajectory measurements
(Rus)
Vol 20, No 1 (2021)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy
(Rus)
This website uses cookies
You consent to our cookies if you continue to use our website.
About Cookies
TOP