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Which consequence results when the gunpowder reaction rate increases within a Congreve rocket?

A)Increased rocket trajectory stability
B)Decreased burning time efficiency
C)Elevated nozzle ablation risks
D)Minimized rocket payload capacity

💡 Explanation

Increased gunpowder reaction raises temperature via increased kinetic energy therefore accelerating nozzle material degradation arising from thermal stress, rather than payload reduction because temperature is dominant.

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