RAHIM, Muhammad Fadhli Hairi; ARIFFIN, Ahmad Hamdan. Design and Analysis of Nozzle Exit Area for Science Technology Engineering and Mathematics (STEM) Based Solid Rocket Propellant. Progress in Aerospace and Aviation Technology, [S. l.], v. 5, n. 2, p. 8–16, 2025. Disponível em: https://penerbit.uthm.edu.my/ojs/index.php/paat/article/view/18365. Acesso em: 11 mar. 2026.