A spherical satellite of radius has an exterior surface with emissivity

PHYSICS · Single correct · CBSE · Physics · Thermal Properties of Matter · Thermal Properties of Matter

Problem

A spherical satellite of radius 1.0 m1.0\,\text{m} has an exterior surface with emissivity 0.600.60. If the satellite must radiate 2.0 kW2.0\,\text{kW} of thermal power into space, what surface temperature is required? (Stefan–Boltzmann constant σ=5.67×10−8 W m−2 K−4\sigma = 5.67\times10^{-8}\,\text{W}\,\text{m}^{-2}\,\text{K}^{-4}) (a) 230 K230\,\text{K} (b) 370 K370\,\text{K} (c) 260 K260\,\text{K} (d) 310 K310\,\text{K}

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