Solid rocket motor design using a surrogate model

Tola C., Nikbay M.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.90, no.7, pp.1104-1127, 2018 (SCI-Expanded) identifier


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.