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The study investigates the combustion performance of aluminum-lithium alloy (Al–Li alloy) in solid rocket propellants, specifically AP/RDX/Al/HTPB formulations. Experimental results indicate that increasing Al–Li alloy content enhances burning rates and combustion efficiency while reducing the size of condensed combustion products. The findings suggest that Al–2.5Li alloy powder is a promising fuel for improving the performance of solid propellants.

Author

pikachufly02

Language

EN