At the nose of a missile in flight, the pressure and temperature are (5.6 mathrm{~atm}) and (850^{circ}

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At the nose of a missile in flight, the pressure and temperature are \(5.6 \mathrm{~atm}\) and \(850^{\circ} \mathrm{R}\), respectively. Calculate the density and specific volume.  \(1 \mathrm{~atm}=2116 \mathrm{lb} / \mathrm{ft}^{2}\).

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