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The temperature at the surface of the Sun is approximately 5 700 K, and the temperature at the surface of the Earth is approximately 290 K. What entropy change occurs when 1 000 J of energy is transferred by radiation from the Sun to the Earth?

Short Answer

Expert verified
The entropy change for the Sun is approximately -0.175 J/K, for the Earth approximately 3.448 J/K, and the total entropy change is approximately 3.273 J/K.

Step by step solution

01

Understanding the Concept of Entropy Change Due to Heat Transfer

The entropy change \( \Delta S \) for a system when an amount of heat \( Q \) is transferred at a constant temperature \( T \) is given by the equation \( \Delta S = \frac{Q}{T} \). When heat is transferred from one system to another, the total entropy change is the sum of the entropy changes of the individual systems.
02

Calculating the Entropy Change for the Sun

Calculate the entropy change for the Sun as the energy leaves it by using the formula: \( \Delta S_{\text{Sun}} = -\frac{Q_{\text{Sun}}}{T_{\text{Sun}}} \) where \( Q_{\text{Sun}} \) is the amount of energy transferred and \( T_{\text{Sun}} \) is the temperature of the Sun. We use a negative sign because the Sun is losing energy. Plug in the values to get \( \Delta S_{\text{Sun}} = -\frac{1000 \, \text{J}}{5700 \, \text{K}} \) and calculate the result.
03

Calculating the Entropy Change for the Earth

Calculate the entropy change for the Earth as it receives energy by using the formula: \( \Delta S_{\text{Earth}} = \frac{Q_{\text{Earth}}}{T_{\text{Earth}}} \) where \( Q_{\text{Earth}} \) is the amount of energy transferred and \( T_{\text{Earth}} \) is the temperature of the Earth. Plug in the values to get \( \Delta S_{\text{Earth}} = \frac{1000 \, \text{J}}{290 \, \text{K}} \) and calculate the result.
04

Calculating the Total Entropy Change

To find the total entropy change \( \Delta S_{\text{total}} \) due to the energy transfer, sum the entropy changes of the Sun and the Earth using the formula: \( \Delta S_{\text{total}} = \Delta S_{\text{Sun}} + \Delta S_{\text{Earth}} \) and substitute the calculated values for \( \Delta S_{\text{Sun}} \) and \( \Delta S_{\text{Earth}} \) from the previous steps to obtain the total change in entropy.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Heat Transfer
Heat transfer is a fundamental concept in thermodynamics that involves the movement of thermal energy from one place to another. It can occur through three primary mechanisms: conduction, convection, and radiation.

In our exercise, the heat transfer takes place by radiation from the Sun to the Earth. Radiation is unique among the three mechanisms as it does not require a medium to travel through; it can occur through a vacuum. This is how the Sun's energy reaches Earth, traveling across the empty space between them.

When we consider the transfer of 1,000 joules of energy from the Sun to the Earth, we are observing the flow of heat due to a temperature difference. The second law of thermodynamics states that heat naturally flows from a hotter object to a cooler one until thermal equilibrium is reached—if not impeded by work or other energy interactions.
System Thermodynamics
In system thermodynamics, we analyze the properties and energy exchanges of systems to understand how processes like heat transfer affect them. A 'system' in thermodynamics is simply the part of the universe we are focusing on, while the surroundings are everything else.

During the heat transfer from the Sun (system) to the Earth (another system), there are changes in the properties of both systems. An important property in this context is entropy, a measure of a system's disorder or randomness. For a given amount of energy transfer, a higher temperature system will experience a smaller increase in entropy compared to a lower temperature system receiving the same amount of energy.

By applying the entropy change formula, we note that as the Sun loses energy, its entropy decreases, while the Earth's entropy increases as it receives energy. The overall change in the universe's entropy, however, will be positive, which is consistent with the second law of thermodynamics.
Temperature
Temperature is a measure of the average kinetic energy of the particles in a substance. In other words, it's an indicator of how hot or cold an object is and determines the direction of heat transfer.

The Sun's surface temperature of approximately 5,700 K is significantly higher than the Earth's surface temperature of approximately 290 K. This drastic difference in temperatures drives the flow of heat from the Sun to the Earth. As heat is transferred, the temperatures of the two bodies influence how much the entropy changes within each system.

For instance, in our exercise, when 1,000 J of energy is transferred from the Sun to the Earth, the resultant change in entropy for each system is inversely proportional to their respective temperatures. The Earth's lower temperature leads to a larger gain in entropy compared to the Sun's higher temperature leading to a smaller loss in entropy. This is reflective of the idea that entropy is also a measure of energy dispersal at a specific temperature.

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Most popular questions from this chapter

A gasoline engine has a compression ratio of 6.00 and uses a gas for which \(\gamma=1.40 .\) (a) What is the efficiency of the engine if it operates in an idealized Otto cycle? (b) What If ? If the actual efficiency is 15.0%, what fraction of the fuel is wasted as a result of friction and energy losses by heat that could by avoided in a reversible engine? (Assume complete combustion of the air–fuel mixture.)

An ideal refrigerator or ideal heat pump is equivalent to a Carnot engine running in reverse. That is, energy \(Q_{c}\) is taken in from a cold reservoir and energy \(Q_{h}\) is rejected to a hot reservoir. (a) Show that the work that must be supplied to run the refrigerator or heat pump is $$W=\frac{T_{h}-T_{c}}{T_{c}} Q_{c}$$ (b) Show that the coefficient of performance of the ideal refrigerator is $$\operatorname{COP}=\frac{T_{c}}{T_{h}-T_{c}}$$

Here is a clever idea. Suppose you build a two-engine device such that the exhaust energy output from one heat engine is the input energy for a second heat engine. We say that the two engines are running in series. Let \(e_{1}\) and \(e_{2}\) represent the efficiencies of the two engines. (a) The overall efficiency of the two-engine device is defined as the total work output divided by the energy put into the first engine by heat. Show that the overall efficiency is given by $$e=e_{1}+e_{2}-e_{1} e_{2}$$ (b) What If? Assume the two engines are Carnot engines. Engine 1 operates between temperatures \(T_{h}\) and \(T_{i} .\) The gas in engine 2 varies in temperature between \(T_{i}\) and \(T_{c} .\) In terms of the temperatures, what is the efficiency of the combination engine? (c) What value of the intermedone by temperature \(T_{i}\) will result in equal work being done by each of the two engines in series? (d) What value of \(T_{i}\) will result in each of the two engines in series having the same efficiency?

A Carnot engine has a power output of 150 \(\mathrm{kW}\) . The engine operates between two reservoirs at \(20.0^{\circ} \mathrm{C}\) and \(500^{\circ} \mathrm{C}\). (a) How much energy does it take in per hour? (b) How much energy is lost per hour in its exhaust?

A heat engine performs 200 J of work in each cycle and has an efficiency of 30.0%. For each cycle, how much energy is (a) taken in and (b) expelled by heat?

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