/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 34 In March 2006 , two small satell... [FREE SOLUTION] | 91Ó°ÊÓ

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In March 2006 , two small satellites were discovered orbiting Pluto, one at a distance of \(48,000 \mathrm{km}\) and the other at \(64,000 \mathrm{km}\) . Pluto already was known to have a large satellite Charon, orbiting at \(19,600 \mathrm{km}\) with an orbital period of 6.39 days. Assuming that the satellites do not affect each other, find the orbital periods of the two small satellites without using the mass of Pluto.

Short Answer

Expert verified
The orbital periods are approximately 16.45 days and 25.57 days.

Step by step solution

01

Understand Kepler's Third Law

Kepler's Third Law states that the square of the orbital period \(T\) of a planet is directly proportional to the cube of the semi-major axis \(r\) of its orbit, i.e., \( T^2 \propto r^3 \). Since these satellites orbit the same planet, Pluto, we can express this as \( \frac{T_1^2}{r_1^3} = \frac{T_2^2}{r_2^3} \).
02

Gather Known Values

We know the orbital radius \(r_1\) and period \(T_1\) of Charon are \(19,600\text{ km}\) and 6.39 days, respectively. The distances for the other two satellites are \(r_2 = 48,000\text{ km}\) and \(r_3 = 64,000\text{ km}\).
03

Set Proportions for First Satellite

First, we find the period \(T_2\) of the satellite at \(48,000\text{ km}\). Using \(\frac{T_2^2}{48000^3} = \frac{6.39^2}{19600^3}\), solve for \(T_2\).
04

Calculate Period for First Satellite

We find \(T_2\) by evaluating: \[ T_2 = \sqrt{6.39^2 \times \left(\frac{48000}{19600}\right)^3} \approx 16.45 \text{ days} \]
05

Set Proportions for Second Satellite

Now, we find the period \(T_3\) of the satellite at \(64,000\text{ km}\). Using \(\frac{T_3^2}{64000^3} = \frac{6.39^2}{19600^3}\), solve for \(T_3\).
06

Calculate Period for Second Satellite

We find \(T_3\) by evaluating: \[ T_3 = \sqrt{6.39^2 \times \left(\frac{64000}{19600}\right)^3} \approx 25.57 \text{ days} \]

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Key Concepts

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

Orbital Period
The term "orbital period" refers to the time it takes a satellite or any celestial body to complete one full orbit around another body, like a planet or star. It is a crucial concept in understanding the dynamic nature of satellite orbits. Orbital periods can vary greatly depending on the object's distance from the celestial body it orbits.
Kepler’s Third Law provides a direct connection between the orbital period and the semi-major axis of the orbit: if you know the semi-major axis, you can determine the orbital period and vice versa. For any satellites of Pluto, such as Charon or the recently discovered ones, their orbital period is influenced by the semi-major axis, affecting how quickly or slowly they revolve around Pluto.
Satellite Orbits
Satellite orbits are the paths that these objects take around planets or stars, defined by specific parameters like size, shape, and distance from the object they orbit. These orbits can be circular or elliptical, and their characteristics are described by properties such as the semi-major axis.
In the case of Pluto’s satellites, each follows a unique orbit. Their distance helps determine the speed at which they travel around Pluto. The behavior of their orbits can be precisely predicted using Kepler’s laws, which relate these orbits to the gravitational pull of Pluto, ensuring a stable path and predictable orbital period.
Pluto Satellites
Pluto, once considered the ninth planet, has several satellites, with Charon being the largest and most well-known. Beyond Charon, the smaller satellites discovered, such as those at distances of 48,000 km and 64,000 km, add intrigue to Pluto's system.
  • Charon: The largest satellite, having a known orbital period of 6.39 days.
  • Newly Discovered Satellites: These satellites’ periods can be calculated using existing data from Charon's orbit due to their shared central body – Pluto.
The dynamics of these satellites, including their orbital periods, are governed by the same gravitational forces allowing us to predict their movements through calculations involving distances and periods.
Proportional Relationship
The concept of a proportional relationship is essential when dealing with celestial mechanics, especially in regard to Kepler’s Third Law. For satellites orbiting the same body, the relationship between the square of their orbital periods and the cube of their semi-major axes follows a simple proportional rule.
This means that if you have data on one satellite, like Charon, you can determine the orbital periods of other satellites by using the proportional relationship: \[ \frac{T_1^2}{r_1^3} = \frac{T_2^2}{r_2^3} = \frac{T_3^2}{r_3^3} \] Such equations allow scientists to predict satellite behaviors without directly measuring every single parameter for each. Instead, they analyze one known orbit and apply the proportions to find others.
Semi-Major Axis
The semi-major axis is half of the longest diameter of an elliptical orbit, serving as a critical component when describing satellite orbits. It essentially measures the size of the orbit and impacts both the orbital path and speed.
  • Defining Orbits: The semi-major axis helps define the unique characteristics of each satellite’s path around Pluto.
  • Influence on Period: The larger the semi-major axis, the longer the orbital period, given the relationship established by Kepler's laws.
Understanding the semi-major axis helps not only in calculating the satellite's position but also in predicting its orbital period. This makes it a key factor when studying orbits in the Pluto satellite system.

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Most popular questions from this chapter

Exploring Europa. There is strong evidence that Europa, a satellite of Jupiter, has a liquid ocean beneath its icy surface. Many scientists think we should land a vehicle there to search for life. Before launching it, we would want to test such a lander under the gravity conditions at the surface of Europa. One way to do this is to put the lander at the end of a rotating arm in an orbiting earth satellite. If the arm is \(4.25 \mathrm{~m}\) long and pivots about one end, at what angular speed (in rpm) should it spin so that the acceleration of the lander is the same as the acceleration due to gravity at the surface of Europa? The mass of Europa is \(4.8 \times 10^{22} \mathrm{~kg}\) and its diameter is \(3138 \mathrm{~km}\).

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A particle of mass 3\(m\) is located 1.00 \(\mathrm{m}\) from a particle of mass \(m .\) (a) Where should you put a third mass \(M\) so that the net gravitational force on \(M\) due to the two masses is exactly zero? (b) Is the equilibrium of \(M\) at this point stable or unstable (i) for points along the line connecting \(m\) and \(3 m,\) and (ii) for points along the line passing through \(M\) and perpendicular to the line connecting \(m\) and 3\(m ?\)

(a) Suppose you are at the earth's equator and observe a satellite passing directly overhead and moving from west to east in the sky. Exactly 12.0 hours later, you again observe this satellite to be directly overhead. How far above the earth's surface is the satellite's orbit? (b) You observe another satellite directly overhead and traveling east to west. This satellite is again overhead in 12.0 hours. How far is this satellite's orbit above the surface of the earth?

An experiment is performed in deep space with two uni- form spheres, one with mass 25.0 \(\mathrm{kg}\) and the other with mass 100.0 \(\mathrm{kg}\) . They have equal radii, \(r=0.20 \mathrm{m}\) . The spheres are released from rest with their centers 40.0 \(\mathrm{m}\) apart. They accelerate toward each other because of their mutual gravitational attraction. You can ignore all gravitational forces other than that between the two spheres. (a) Explain why linear momentum is conserved. (b) When their centers are 20.0 \(\mathrm{m}\) apart, find (i) the speed of each sphere and (ii) the magnitude of the relative velocity with which one sphere is approaching the other. (c) How far from the initial position of the center of the \(25.0-\mathrm{kg}\) sphere do the surfaces of the two spheres collide?

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