Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

A planet with a mass of \(7.00 \cdot 10^{21} \mathrm{~kg}\) is in a circular orbit around a star with a mass of \(2.00 \cdot 10^{30} \mathrm{~kg} .\) The planet has an orbital radius of \(3.00 \cdot 10^{10} \mathrm{~m}\). a) What is the linear orbital velocity of the planet? b) What is the period of the planet's orbit? c) What is the total mechanical energy of the planet?

Short Answer

Expert verified
Question: A planet with mass m_p orbits around a star with mass m_s. The distance between the planet and the star is r. Find the linear orbital velocity (v), the period of the planet's orbit (T), and the total mechanical energy (E) of the planet. Answer: To find the linear orbital velocity (v), the period of the planet's orbit (T), and the total mechanical energy (E) of the planet, follow these steps: 1. Find the gravitational force between the planet and the star using Newton's law of universal gravitation: \(F = G\frac{m_pm_s}{r^2}\) 2. Determine the centripetal force keeping the planet in a circular orbit: \(F_c = m_pv^2/r\) 3. Set the equations from steps 1 and 2 equal to each other and solve for v: \(v=\sqrt{\frac{Gm_s}{r}}\) 4. Calculate the period of the planet's orbit (T): \(T=\frac{2\pi r}{v}\) 5. Calculate the total mechanical energy of the planet (E): \(E=KE + PE = \frac{1}{2}m_pv^2 - G\frac{m_pm_s}{r}\) Using the given values for m_p, m_s, and r, along with the gravitational constant G, calculate the linear orbital velocity, the period of the planet's orbit, and the total mechanical energy of the planet.

Step by step solution

01

Gravitational force

First, we want to find the gravitational force between the planet and the star. This can be done using Newton's law of universal gravitation: \(F = G\frac{m_pm_s}{r^2}\) Where \(F\) is the gravitational force, \(G\) is the gravitational constant (\(6.67 \cdot 10^{-11} \mathrm{N(m/kg)^2}\)), \(m_p\) is the mass of the planet, \(m_s\) is the mass of the star, and \(r\) is the distance between them.
02

Centripetal force

The centripetal force keeping the planet in a circular orbit is equal in magnitude to the gravitational force. The centripetal force can be expressed as: \(F_c = m_pv^2/r\) Where \(F_c\) is the centripetal force, \(m_p\) is the mass of the planet, \(v\) is the linear velocity, and \(r\) is the orbital radius.
03

Solve for linear orbital velocity

Since the gravitational force and centripetal force are equal, we can set the equations from steps 1 and 2 equal to each other and solve for \(v\): \(G\frac{m_pm_s}{r^2}=m_pv^2/r \Rightarrow v=\sqrt{\frac{Gm_s}{r}}\) Now, plug in the given values for \(G\), \(m_s\), and \(r\) to find the linear orbital velocity, \(v\).
04

Calculate the period of the planet's orbit

To find the period of the planet's orbit, we need to find the time it takes for the planet to travel around the circumference of its orbit, \(2\pi r\). We can find the period, \(T\), by dividing this distance by the linear orbital velocity, \(v\): \(T=\frac{2\pi r}{v}\) Using the linear orbital velocity found in step 3, calculate the period of the planet's orbit.
05

Calculate total mechanical energy

The total mechanical energy of the planet is the sum of its kinetic energy and gravitational potential energy. The kinetic energy, \(KE\), can be calculated as: \(KE=\frac{1}{2}m_pv^2\) The gravitational potential energy, \(PE\), can be calculated as: \(PE=-G\frac{m_pm_s}{r}\) The total mechanical energy, \(E\), is the sum of the kinetic energy and potential energy: \(E=KE + PE\) Calculate the kinetic energy and potential energy using the values found in step 3 and the given masses. Then, add the kinetic and potential energies together to find the total mechanical energy.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

Key Concepts

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

Gravitational Force
In the realm of orbital mechanics, the concept of gravitational force is fundamental. In our case, we look at the gravitational force as the attraction between a planet and a star. This force is calculated using Newton’s law of universal gravitation, which states: \[F = G \frac{m_p m_s}{r^2}\]where:
  • \(F\) is the gravitational force,

  • \(G\) is the gravitational constant \(6.67 \cdot 10^{-11} \mathrm{N(m/kg)^2}\),

  • \(m_p\) is the mass of the planet,

  • \(m_s\) is the mass of the star, and

  • \(r\) is the distance between the two celestial bodies.
This force is what holds the planet in orbit. The greater the masses or the closer they are, the stronger the gravitational pull. This force provides the necessary centripetal force to maintain the circular orbital path of the planet.
Centripetal Force
To keep a planet in a circular orbit, a centripetal force is required. This is the force that keeps the planet moving in a circle rather than flying off into space. In this context, the centripetal force is provided by the gravitational pull between the planet and the star. We can express it as:\[F_c = m_p \frac{v^2}{r}\]where:
  • \(F_c\) is the centripetal force,

  • \(v\) is the orbital velocity,

  • \(r\) is the radius of the orbit, and

  • \(m_p\) is the mass of the planet.
The crucial point here is that the gravitational force is equal in magnitude to the centripetal force required for circular motion. By setting \[G\frac{m_pm_s}{r^2} = m_p\frac{v^2}{r}\]we can relate these quantities, allowing us to solve for unknowns like orbital speed (\(v\)) and orbital period.
Kinetic Energy
Kinetic energy is the energy of motion. For a planet revolving around a star, this energy is a function of its speed in orbit. The expression for kinetic energy is:\[KE = \frac{1}{2} m_p v^2\]where:
  • \(KE\) is kinetic energy,

  • \(m_p\) is the mass of the planet, and

  • \(v\) is the linear velocity of the planet.
In a stable orbit, the planet's kinetic energy arises from the gravitational force acting as a centripetal force. Higher velocities mean more kinetic energy. This energy is balanced against the planet’s gravitational potential energy to maintain a stable orbit.
Potential Energy
In orbital mechanics, gravitational potential energy is significant. It is the energy stored by the virtue of the position of the planet. The formula for potential energy in the context of a planet orbiting a star is given by:\[PE = -G \frac{m_p m_s}{r}\]The negative sign indicates that the potential energy is lower when the planet is closer to the star, reflecting the attractive nature of gravity. Here:
  • \(PE\) is the potential energy,

  • \(G\) is the gravitational constant,

  • \(m_p\) the mass of the planet,

  • \(m_s\) is the mass of the star, and

  • \(r\) is the orbital radius.
This form of energy counteracts kinetic energy to influence the planet's motion. The total mechanical energy of the planet is the sum of its kinetic and potential energies, which remains conserved unless external forces work on the system.

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

Standing on the surface of a small spherical moon whose radius is \(6.30 \cdot 10^{4} \mathrm{~m}\) and whose mass is \(8.00 \cdot 10^{18} \mathrm{~kg}\) an astronaut throws a rock of mass 2.00 kg straight upward with an initial speed \(40.0 \mathrm{~m} / \mathrm{s}\). (This moon is too small to have an atmosphere.) What maximum height above the surface of the moon will the rock reach?

In a binary star system consisting of two stars of equal mass, where is the gravitational potential equal to zero? a) exactly halfway between the stars b) along a line bisecting the line connecting the stars c) infinitely far from the stars d) none of the above

You have been sent in a small spacecraft to rendezvous with a space station that is in a circular orbit of radius \(2.5000 \cdot 10^{4} \mathrm{~km}\) from the Earth's center. Due to a mishandling of units by a technician, you find yourself in the same orbit as the station but exactly halfway around the orbit from it! You do not apply forward thrust in an attempt to chase the station; that would be fatal folly. Instead, you apply a brief braking force against the direction of your motion, to put you into an elliptical orbit, whose highest point is your present position, and whose period is half that of your present orbit. Thus, you will return to your present position when the space station has come halfway around the circle to meet you. Is the minimum radius from the Earth's center-the low point \(-\) of your new elliptical orbit greater than the radius of the Earth \((6370 \mathrm{~km})\), or have you botched your last physics problem?

Suppose a new extrasolar planet is discovered. Its mass is double the mass of the Earth, but it has the same density and spherical shape as the Earth. How would the weight of an object at the new planet's surface differ from its weight on Earth?

With the usual assumption that the gravitational potential energy goes to zero at infinite distance, the gravitational potential energy due to the Earth at the center of Earth is a) positive. b) negative. c) zero. d) undetermined.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free