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) |
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Zdroj: | Combustion, Explosion, & Shock Waves. Mar2020, Vol. 56 Issue 2, p172-180. 9p. |
Databáze: | Academic Search Ultimate |
Externí odkaz: |