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
https://doi.org/10.15407/knit2017.05.021
Мова публікації: Russian
Анотація: 
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).
References: 
1. Volkov E. B. Siritsin T. A. Static and dynamics of rocket motors: in 2 volumes, v. 2, p. 219—224 (Mechani-calengineering, Moskow,1987) [in Russian].
2. Sorkin R. E. Theory of internal ballistics of SRM, p. 85—87 ( Science, Moskow, 1964) [in Russian].