Mathematical modelling of introballistic characteristic of solid rocket engine with power-on emergency shutdown system

1Lytvynenko, VYe., 1Kalnysh, RV, 1Popov, VA
1Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
Space Sci.&Technol. 2017, 23 ;(5):21-24
Section: Space Energy, Power and Propulsion
Publication Language: Russian
We consider differential equations, which describe processes in combustion chamber of solid rocket engine (SRE). We describe our propositions, which are useful for calculation of introballistic characteristic (IBC). They allows 1) to take into account the more numbers of factors that have influence on the SRM’s work, 2) to include  the IBC calculations of engine with power-on emergency shutdown system (ESS).
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