Solid rocket motor design using a surrogate model

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Copy For Citation

Tola C., Nikbay M.

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

• Publication Type: Article / Article
• Volume: 90 Issue: 7
• Publication Date: 2018
• Doi Number: 10.1108/aeat-01-2017-0045
• Journal Name: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
• Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus
• Page Numbers: pp.1104-1127
• Istanbul Technical University Affiliated: Yes

Abstract

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.