Development of mathematical models and programs (in MathCad)‚ carrying out computations of following problems: thermal condition of liquid propellant (kerosene) in first- and second stage fuel tanks at the launch pad; thermal condition of air in payload unit; thermal condition of air in launch vehicle units; determine of required parameters of thermostating air (temperature‚ flow rate‚ humidity); determine of thermal stratification of propellant in fuel tanks‚ determine of thermal resistance of the fairing. Development of sections of preliminary design review and critical design review; contact with foreign partners; take part in teleconference with foreign partners. Take part in technical inspection of military facilities.
Образование
Основное — высшее
Dnepropetrovsk State University, Dnepropetrovsk, Ukraine, Mechanics and mathematics faculty (высшее), с 2000 по 2008
Специальность:
“Hydro and Aerodynamics”
Dynamics of gases and fluids; engineering approach and numerical methods.
