Solid rocket motor design using a surrogate model


Tola C., Nikbay M.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.90, ss.1104-1127, 2018 (SCI İndekslerine Giren Dergi) identifier

  • Cilt numarası: 90 Konu: 7
  • Basım Tarihi: 2018
  • Doi Numarası: 10.1108/aeat-01-2017-0045
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Sayfa Sayıları: ss.1104-1127

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.