Solid rocket motor design using a surrogate model


Tola C., Nikbay M.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.90, sa.7, ss.1104-1127, 2018 (SCI-Expanded) identifier

Özet

Purpose This study aims to determine the relationship between sectional geometric parameters of a slotted solid rocket propellant on structural integrity and internal ballistic performance of a rocket motor by using response surface method.