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Which mechanism ultimately limits maximum efficiency in solid rocket propellant grain design?

A)Phase transition induced volume fracture
B)Thermal expansion induced nozzle erosion
C)Crystallization induced gas flow turbulence
D)Oxidation induced ablative material loss

💡 Explanation

Phase transition volume fracture limits efficiency because solid propellant grains undergo significant phase changes near the ignition temperature, rather than ablative losses. Therefore, volumetric expansion causes internal stresses that promote cracking; this shortens burn time.

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