Urazbakhtin Ф. А. and Korenev А. А. (2012) “Mathematical Model of Critical Situations According to Properties Intensity of Solid Propellant Rocket Engine”, Intellekt. Sist. Proizv, 7(1), pp. 60–72. Available at: https://izdat.istu.ru/index.php/ISM/article/view/1402 (Accessed: 7 April 2025).