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A solar flux of \(1400 \mathrm{~W} / \mathrm{m}^{2}\) directly strikes a spacevehicle surface which has a solar absortivity of \(0.4\) and thermal emissivity of \(0.6\). The equilibrium temperature of this surface in space at \(0 \mathrm{~K}\) is (a) \(300 \mathrm{~K}\) (b) \(360 \mathrm{~K}\) (c) \(410 \mathrm{~K}\) (d) \(467 \mathrm{~K}\) (e) \(510 \mathrm{~K}\)

Short Answer

Expert verified
The equilibrium temperature of the space vehicle's surface in space at 0 K is approximately 410 K.

Step by step solution

01

Understand the equilibrium condition

In equilibrium, the energy absorbed by the surface is equal to the energy radiated by the surface. Therefore, we can express this condition as follows: $$\text{Absorbed Energy} = \text{Radiated Energy}$$
02

Calculate the absorbed energy

The energy absorbed by the surface can be calculated using the solar flux and the solar absorptivity. The formula for this is: $$\text{Absorbed Energy} = \text{Solar Flux} * \text{Solar Absorptivity}$$ Substitute the given values: $$\text{Absorbed Energy} = (1400 \frac{\mathrm{W}}{\mathrm{m}^{2}}) * 0.4$$ Now, calculate the absorbed energy: $$\text{Absorbed Energy} = 560 \frac{\mathrm{W}}{\mathrm{m}^{2}}$$
03

Calculate the radiated energy

The energy radiated by the surface due to thermal radiation can be written as: $$\text{Radiated Energy} = \text{Emissivity} * \sigma * T^{4} * A$$ Where: - Emissivity is the thermal emissivity of the surface (0.6 in this case) - \(\sigma\) is the Stefan–Boltzmann constant (\(5.67 × 10^{-8} \frac{\mathrm{W}}{\mathrm{m}^{2}\mathrm{K}^{4}}\)) - T is the surface temperature in Kelvin, which we are trying to find - A is the surface area Since we are calculating the temperature and the question is asking the equilibrium surface temperature, we will consider the radiated and absorbed energy per unit area. Thus, A in both cases cancels out.
04

Equate absorbed and radiated energy and solve for T

Now, we can equate the absorbed and radiated energies: $$560 \frac{\mathrm{W}}{\mathrm{m}^{2}} = 0.6 * 5.67 × 10^{-8} \frac{\mathrm{W}}{\mathrm{m}^{2}\mathrm{K}^{4}} * T^{4}$$ Divide both sides by `\(0.6 * 5.67 × 10^{-8} \frac{\mathrm{W}}{\mathrm{m}^{2}\mathrm{K}^{4}}\)`: $$T^{4} = \frac{560 \frac{\mathrm{W}}{\mathrm{m}^{2}}}{0.6 * 5.67 × 10^{-8} \frac{\mathrm{W}}{\mathrm{m}^{2}\mathrm{K}^{4}}}$$ Calculate \(T^{4}\): $$T^{4} = 1.64 × 10^{8} \mathrm{K}^{4}$$ Now, take the fourth root on both sides: $$T = \sqrt[4]{1.64 × 10^{8}\mathrm{K}^{4}}$$ Calculate T: $$T = 410 \mathrm{K}$$ Thus, the answer is: **(c) \(410 \mathrm{~K}\)**

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Most popular questions from this chapter

Five identical thin aluminum sheets with emissivities of \(0.1\) on both sides are placed between two very large parallel plates, which are maintained at uniform temperatures of \(T_{1}=800 \mathrm{~K}\) and \(T_{2}=450 \mathrm{~K}\) and have emissivities of \(\varepsilon_{1}=\) \(\varepsilon_{2}=0.1\), respectively. Determine the net rate of radiation heat transfer between the two plates per unit surface area of the plates, and compare the result to that without the shield.

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Define the spectral emissivity of a medium of thickness \(L\) in terms of the spectral absorption coefficient.

A clothed or unclothed person feels comfortable when the skin temperature is about \(33^{\circ} \mathrm{C}\). Consider an average man wearing summer clothes whose thermal resistance is \(1.1\) clo. The man feels very comfortable while standing in a room maintained at \(20^{\circ} \mathrm{C}\). If this man were to stand in that room unclothed, determine the temperature at which the room must be maintained for him to feel thermally comfortable. Assume the latent heat loss from the person to remain the same. Answer: 27.8°C

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