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Two planets in circular orbits around a star have speeds of \(v\) and \(2 v\). (a) What is the ratio of the orbital radii of the planets? (b) What is the ratio of their periods?

Short Answer

Expert verified
The ratio of the orbital radii of the two planets is 4:1, and the ratio of their orbital periods is 8:1.

Step by step solution

01

Orbital speed formula

We'll start by using the formula for the orbital speed of a planet around a star: \(v^2 = G\frac{M}{r}\), where \(v\) is the orbital speed of the planet, \(G\) is the gravitational constant, \(M\) is the mass of the central body (the star), and \(r\) is the orbital radius of the planet. For our two planets, we have the following equations: \(v_1^2 = G\frac{M}{r_1}\) and \(v_2^2 = G\frac{M}{r_2}\), where \(v_1\) and \(v_2\) are their respective orbital speeds, and \(r_1\) and \(r_2\) are their respective orbital radii.
02

Setting up the ratio of orbital radii

The problem states that the orbital speeds of the two planets are related by \(v_2 = 2v_1\). Using the equations from Step 1, we can set up the ratio of orbital radii: \(\frac{r_1}{r_2} = \frac{G\frac{M}{v_1^2}}{G\frac{M}{v_2^2}} = \frac{v_2^2}{v_1^2} = \left(\frac{2v_1}{v_1}\right)^2 = 4\). So, the ratio of the orbital radii of the planets is 4:1.
03

Ratio of orbital periods

To find the ratio of the orbital periods, we'll use Kepler's third law, which states that the square of a planet's period is proportional to the cube of its orbital radius: \(T^2 \propto r^3\), where \(T\) is the orbital period, and \(r\) is the orbital radius. Setting up the ratio of periods for our two planets: \(\frac{T_1^2}{T_2^2} = \frac{r_1^3}{r_2^3}\). We know from Step 2 that the ratio of the orbital radii is 4:1. Hence, \(\frac{T_1^2}{T_2^2} = \left(\frac{4}{1}\right)^3 = 64\). Taking the square root of both sides gives: \(\frac{T_1}{T_2} = \sqrt{64} = 8\). So, the ratio of the orbital periods of the two planets is 8:1.

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Key Concepts

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

Orbital Speed
The orbital speed of a planet is a crucial aspect of its motion around a star. It determines how fast the planet travels along its circular path. This speed depends on several factors, including the gravitational pull of the star and the distance of the planet from it. The formula for calculating orbital speed is:
\[ v^2 = G\frac{M}{r} \]Here:
  • \(v\) is the orbital speed of the planet.
  • \(G\) is the gravitational constant.
  • \(M\) is the mass of the star.
  • \(r\) is the orbital radius, which is the distance between the planet and the star.
This formula highlights how the speed is inversely related to the orbital radius — meaning, the closer the planet is to the star, the faster it moves. Conversely, a greater distance implies a slower speed.
Orbital speed plays a fundamental role in determining the dynamics of a celestial body in space. By understanding it, one can derive other properties of a planetary system, such as the radius of orbit and the orbital period.
Kepler's Third Law
Kepler's Third Law is an essential principle in celestial mechanics that explains the relationship between a planet's orbital period and its orbital radius. Its formulation is:
\[ T^2 \propto r^3 \]This law means:
  • The square of the orbital period \( (T^2) \) of a planet is proportional to the cube of the semi-major axis of its orbit \( (r^3) \).
  • This concept simplifies to a constant relationship in a system where only one central massive body like the Sun is considered.
Thus, within our Solar System or any similar systems, if you know the orbital radius of a planet, you can easily calculate its orbital period and vice versa. It's important to note that this law only applies to objects in a stable, circular orbit. It is essential for computing celestial distances and understanding the orbital dynamics of planets and satellites.
Understanding Kepler's Third Law is vital for advancing comprehension in fields like astronomy, astrophysics, and even space navigation. It provides insight into the lasting mechanics that govern celestial motions.
Gravitational Constant
The gravitational constant, denoted by \(G\), is a key figure in the field of physics, especially in gravitational equations. It allows us to quantify the attractive force between two masses. In the context of celestial bodies, \(G\) becomes crucial when calculating gravitational forces between stars, planets, and other astronomical entities. The value of \(G\) is approximately \(6.674 \times 10^{-11} \text{m}^3\text{kg}^{-1}\text{s}^{-2}\).
In the formula for calculating orbital speed, \(G\) helps determine how the gravitational force of a massive body like a star influences the motion of planets revolving around it:
\[ v^2 = G\frac{M}{r} \]Here, \(G\) is coupled with the mass \(M\) of the star, influencing the speed \(v\) at which the planet orbits the star.
The constancy of \(G\) is a fundamental aspect of physics and remains unchanged regardless of the mass or location in the universe. Its role in space dynamics is indispensable and underpins foundational laws such as Newton's law of universal gravitation. Understanding \(G\) provides insight into how force, mass, and distance interact to orchestrate the movements of planets and stars.

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Most popular questions from this chapter

Circular orbits in Equation 13.10 for conic sections must have eccentricity zero. From this, and using Newton's second law applied to centripetal acceleration, show that the value of \(\alpha\) in Equation 13.10 is given by \(\alpha=\frac{L^{2}}{\mathrm{G} M m^{2}}\) where \(L\) is the angular momentum of the orbiting body. The value of \(\alpha\) is constant and given by this expression regardless of the type of orbit.

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