Consider a spherical shell satellite with outer diameter of \(4 \mathrm{~m}\)
and shell thickness of \(10 \mathrm{~mm}\) is reentering the atmosphere. The
shell satellite is made of stainless steel with properties of \(\rho=8238
\mathrm{~kg} / \mathrm{m}^{3}, c_{p}=468 \mathrm{~J} / \mathrm{kg} \cdot
\mathrm{K}\), and \(k=13.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). During
the reentry, the effective atmosphere temperature surrounding the satellite is
\(1250^{\circ} \mathrm{C}\) with convection heat transfer coefficient of \(130
\mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). If the initial temperature of
the shell is \(10^{\circ} \mathrm{C}\), determine the shell temperature after 5
minutes of reentry. Assume heat transfer occurs only on the satellite shell.