Experimental Approaches to Develop a High Thrust Ratio in a Single Chamber Dual Thrust Motor Using a Composite Propellant Formulation Based on HTPB/AP/Al
Ramesh Kurva, Sujeet Ukey, Milind Modgi, Mehilal
Słowa Kluczowe: dual thrust ratio, single chamber, composite propellant, high burning rate, burning surface area
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