Problem 1
Question
Find the centrifugal acceleration at the equator of the planet Jupiter and of the Sun. In each case, express your answer also as a fraction of the surface gravity. (The rotation periods are 10 hours and 27 days, respectively, the radii \(7.1 \times 10^{4} \mathrm{~km}\) and \(7.0 \times 10^{5} \mathrm{~km}\), and the masses \(1.9 \times 10^{27} \mathrm{~kg}\) and \(\left.2.0 \times 10^{30} \mathrm{~kg} .\right)\)
Step-by-Step Solution
Verified Answer
Question: Calculate the centrifugal acceleration at the equator of Jupiter and the Sun, and express the answer as a fraction of the surface gravity for both.
Answer: The centrifugal acceleration at the equator of Jupiter is approximately \(4.30\mathrm{~m/s^2}\), or \(0.173\) times the surface gravity. The centrifugal acceleration at the equator of the Sun is approximately \(5.82 \times 10^{-3}\mathrm{~m/s^2}\), or \(2.12 \times 10^{-5}\) times the surface gravity.
1Step 1: Calculate linear velocity
First, we will calculate the linear velocity of Jupiter and the Sun using the formula \(v = \frac{2 \pi R}{T}\). We have \(R_J=7.1 \times 10^4 \mathrm{~km}\), \(T_J=10\mathrm{~hours}\) for Jupiter, and \(R_\odot=7.0 \times 10^5 \mathrm{~km}\), \(T_\odot=27\mathrm{~days}\) for the Sun.
For Jupiter:
\(v_J = \frac{2 \pi (7.1 \times 10^7\mathrm{~m})}{10\mathrm{~hours} \times 3600\mathrm{~s/hour}} \approx 1.75 \times 10^4\mathrm{~m/s}\)
For the Sun:
\(v_\odot = \frac{2 \pi (7.0 \times 10^8\mathrm{~m})}{27\mathrm{~days} \times 24\mathrm{~hours/day} \times 3600\mathrm{~s/hour}} \approx 2.02 \times 10^3\mathrm{~m/s}\)
2Step 2: Calculate centrifugal acceleration
Now, calculate the centrifugal acceleration using the formula \(a_c = \frac{v^2}{R}\).
For Jupiter:
\(a_{cJ} = \frac{(1.75 \times 10^4\mathrm{~m/s})^2}{7.1 \times 10^7\mathrm{~m}} \approx 4.30 \times 10^0\mathrm{~m/s^2}\)
For the Sun:
\(a_{c\odot} = \frac{(2.02 \times 10^3\mathrm{~m/s})^2}{7.0 \times 10^8\mathrm{~m}} \approx 5.82 \times 10^{-3}\mathrm{~m/s^2}\)
3Step 3: Calculate surface gravity
Calculate the surface gravity using the formula \(g = \frac{GM}{R^2}\). We have \(M_J=1.9 \times 10^{27} \mathrm{~kg}\) for Jupiter, and \(M_\odot=2.0 \times 10^{30}\mathrm{~kg}\) for the Sun. The gravitational constant is \(G = 6.674 \times 10^{-11}\mathrm{~m^3/kg~s^2}\).
For Jupiter:
\(g_J = \frac{(6.674 \times 10^{-11}\mathrm{~m^3/kg~s^2})(1.9 \times 10^{27}\mathrm{~kg})}{(7.1 \times 10^7\mathrm{~m})^2} \approx 24.79\mathrm{~m/s^2}\)
For the Sun:
\(g_\odot = \frac{(6.674 \times 10^{-11}\mathrm{~m^3/kg~s^2})(2.0 \times 10^{30}\mathrm{~kg})}{(7.0 \times 10^8\mathrm{~m})^2} \approx 274.07\mathrm{~m/s^2}\)
4Step 4: Express centrifugal acceleration as a fraction of surface gravity
Divide the calculated centrifugal acceleration by the surface gravity to express the centrifugal acceleration as a fraction of the surface gravity.
For Jupiter:
\(\frac{a_{cJ}}{g_J} = \frac{4.30 \times 10^0\mathrm{~m/s^2}}{24.79\mathrm{~m/s^2}} \approx 0.173\)
For the Sun:
\(\frac{a_{c\odot}}{g_\odot} = \frac{5.82 \times 10^{-3}\mathrm{~m/s^2}}{274.07\mathrm{~m/s^2}} \approx 2.12 \times 10^{-5}\)
The centrifugal acceleration at the equator of Jupiter is approximately \(4.30\mathrm{~m/s^2}\), or \(0.173\) times the surface gravity. The centrifugal acceleration at the equator of the Sun is approximately \(5.82 \times 10^{-3}\mathrm{~m/s^2}\), or \(2.12 \times 10^{-5}\) times the surface gravity.
Key Concepts
Linear VelocitySurface GravityRotation Periods of Celestial Bodies
Linear Velocity
Understanding linear velocity is essential when examining the movement of celestial bodies. Let's start with its definition. Linear velocity, symbolized as 'v', is the rate at which an object covers distance in a particular direction, and it is a vector quantity having both magnitude and direction. In the context of a rotating planet or the Sun, the linear velocity at the equator can be determined by the formula:
\( v = \frac{2 \times \pi \times R}{T} \)
Here, \( R \) is the radius of the celestial body and \( T \) is the rotation period. The rotation period is the time it takes for the celestial body to complete one full rotation on its axis. It's expressed in seconds, minutes, or hours.
\( v = \frac{2 \times \pi \times R}{T} \)
Here, \( R \) is the radius of the celestial body and \( T \) is the rotation period. The rotation period is the time it takes for the celestial body to complete one full rotation on its axis. It's expressed in seconds, minutes, or hours.
- For Jupiter with a radius of 7.1 x 104 km and rotation period of 10 hours, the linear velocity is high due to the short rotation period.
- For the Sun with a much larger radius of 7.0 x 105 km but a longer rotation period of 27 days, the linear velocity is considerably lower.
Surface Gravity
Surface gravity, often represented by 'g', is the gravitational acceleration experienced by an object on the surface of a celestial body. It is determined by the mass of the body and the distance from its center, calculated using the formula:
\( g = \frac{GM}{R^2} \)
where \( G \) is the gravitational constant, \( M \) is the mass of the celestial body, and \( R \) is its radius. Surface gravity gives us an understanding of how strong a body’s gravitational pull is at its surface.
\( g = \frac{GM}{R^2} \)
where \( G \) is the gravitational constant, \( M \) is the mass of the celestial body, and \( R \) is its radius. Surface gravity gives us an understanding of how strong a body’s gravitational pull is at its surface.
- For example, Jupiter has a much lower surface gravity than the Sun due to its smaller mass relative to its radius.
- Surface gravity influences an object's weight and the escape velocity needed for it to leave the surface of the celestial body.
Rotation Periods of Celestial Bodies
The rotation period of a celestial body is the time it takes to complete one full spin around its axis. This spin determines the length of a day on the body, affecting the life cycles of potential inhabitants and influencing the planet's climate and weather patterns.
- Shorter rotation periods, like Jupiter's 10 hours, can lead to a more pronounced bulging at the equator, increased centrifugal force, and potentially stronger atmospheric dynamics.
- Longer rotation periods, such as the Sun's 27-day cycle, result in less bulging and relatively weaker centrifugal forces.
Other exercises in this chapter
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