On the Effectiveness of Using the Real Law of Solid Propellant Burning Rate As a Function of Solid Rocket Motor Pressure.

Autor: Lipanov, A. M.1,2 (AUTHOR) aml35@yandex.ru, Kolesnikova, L. N.2 (AUTHOR), Leshchev, A. Yu.3 (AUTHOR)
Zdroj: Combustion, Explosion, & Shock Waves. Mar2020, Vol. 56 Issue 2, p172-180. 9p.
Databáze: Academic Search Ultimate