[1]
Kulkarni, A.R., Bhat, V.K., Phadke, S.P. and Nair, R. 2013. Simplified Burn-Rate Model for CMDB Propellants. Defence Science Journal. 40, 3 (Jan. 2013), 255–262. DOI:https://doi.org/10.14429/dsj.40.4467.