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Investigation of Liquid Breakup Process Solid Rocket Motor Part A: Horizontal Converging–Diverging Nozzle
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents a solid rocket motor (SRM), both experiment and simulation of alumina molten flow patterns using the cold flow case. The combustion of aluminum composite propellants in SRM chambers causes high-temperature ...
Investigation of Liquid Breakup Process Solid Rocket Motor Part B: Vertical C-D Nozzle
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Aluminized propellants are frequently used in solid rocket motors (SRMs) to increase specific impulse. However, as the propellant combusts, the aluminum is oxidized into aluminum oxide (Al2O3), it agglomerates into molten ...