Oxamide (OXA) and azodicarbonamide (ADA) are among the known burning rate suppressants used in composite solid rocket propellants. Much research has been carried out to understand mechanism of suppression but literature about the action of OXA and ADA on the combustion characteristics of propellant is still scarce. Here. a systematic study on coolant-based propellants has been underta... https://thebanyantreers.shop/product-category/decorative-trays/