The nozzle of an experimental rocket motor is fabricated from $5 \mathrm{~mm}$-thick alloy steel. The combustion gases are at $2100 \mathrm{~K}$, and the effective heat transfer coefficient is $6000 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K}$. If the nozzle is initially at $300 \mathrm{~K}$ and the maximum allowable operating temperature for the steel is specified as $1300 \mathrm{~K}$, what is the allowable duration of firing? To obtain a conservative estimate, neglect the heat loss from the outer surface of the nozzle. Take $k=43 \mathrm{~W} / \mathrm{m} \mathrm{K}, \alpha=12.0 \times 10^{-6}$ $\mathrm{m}^{2} / \mathrm{s}$ for the steel.