Математическое моделирование прогрева корпуса первой ступени ракеты РС-22 при инициированном воздействии
Date Issued
2012
Author(s)
Беляев, Н. Н.
Берлов, А. В.
Губин, А. И.
Abstract
The mathematical model of warming up of corps the first stage of the intercontinental strategic rocket RS-22 is built. A calculation is based on application of structural method for the decision of task of heat conductivity in component constructions. Time of warming up of corps rocket to the self-ignition of hard fuel is found.
