Computational Investigation of Combustion Efficiency in LOX-HTPB Hybrid Rocket Motors. Acceleron Aerospace Journal, [S. l.], v. 5, n. 2, p. 1350–1361, 2025. DOI: 10.61359/11.2106-2546. Disponível em: https://acceleron.org.in/index.php/aaj/article/view/261. Acesso em: 6 mar. 2026.