KISHORE, K.; SUNITHA, M. R. Effect of Oxidizer Particle Size on Burning Rate and Thermal Decomposition of Composite Solid Propellants. Defence Science Journal, [S. l.], v. 32, n. 3, p. 251–257, 2014. DOI: 10.14429/dsj.32.6307. Disponível em: https://publications.drdo.gov.in/ojs/index.php/dsj/article/view/6307. Acesso em: 16 jun. 2025.