The mean distance of Mars from the Sun is1.52times that of Earth from the Sun. From Kepler’s law of periods, calculate the number of years required for Mars to make one revolution around the Sun; compare your answer with the value given in Appendix C.

Short Answer

Expert verified

The number of years required for Mars to make one revolution around the sun is 1.87 years.

Step by step solution

01

Step 1: Given

The mean distance of Mars from the sun is 1.52 times that of Earth from the sun.

02

Determining the concept

Using Kepler’s law of period, find thenumber of years required for Mars to make one revolution around the sun and compare the answer with the given value in Appendix C. According to Kepler’s third law, the squares of the orbital periods of the planets are directly proportional to the cubes of the semi major axes of their orbits.

Formula is as follow :

TMTE2=rMrE3

where, T is corresponding time and ris corresponding radius.

03

Determining the number of years required for mars to make one revolution around the sun and to compare the answer with the given value in appendix c 

Now,

TMTE2=rMrE3

As,

rM=1.52rEandTE=1year

TM=1.87years

Hence, thenumber of years required for Mars to make one revolution around the sun is1.87 years.

The given value in the appendix is 1.88 years which is quite close to the obtained answer.

Therefore, using Kepler’s law of period, the time of revolution of the mars around the sun can be found.

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!

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

Zero, a hypothetical planet, has amass of5.0×1023kg, a radius of3.0×106m ,and no atmosphere. A10kg space probe is to be launched vertically from its surface. (a) If the probe is launched with an initial energy of 5.0×107J, what will be its kinetic energy when it is4.0×106m from the center of Zero? (b) If the probe is to achieve a maximum distance of 8.0×106mfrom the center of Zero, with what initial kinetic energy must it be launched from the surface of Zero?

In Fig. 13-23, a central particle is surrounded by two circular rings of particles, at radii rand R , withR > r. All the particles have mass m . What are the magnitude and direction of the net gravitational force on the central particle due to the particles in the rings?

The presence of an unseen planet orbiting a distant star can sometimes be inferred from the motion of the star as we see it. As the star and planet orbit, the center of mass of the star-planet system, the star moves toward and away from us with what is called the line of sight velocity, a motion that can be detected. Figure 13-49 shows a graph of the line of sight velocity versus time for the star 14  Herculis. The star’s mass is believed to be 0.90 of the mass of our Sun. Assume that only one planet orbits the star and that our view is along the plane of the orbit. Then approximate (a) the planet’s mass in terms of Jupiter’s mass mJand

(b) the planet’s orbital radius in terms of Earth’s orbital radiusrE .

What are (a) the speed and (b) the period of a220kgsatellite in an approximately circular orbit 640kmabove the surface of Earth? Suppose the satellite loses mechanical energy at the average rate of 1.4×105Jper orbital revolution. Adopting the reasonable approximation that the satellite’s orbit becomes a “circle of slowly diminishing radius,” determine the satellite’s

(c) altitude,(d) speed, and(e) period at the end of its 1500th revolution.

(f) What is the magnitude of the average retarding force on the satellite? Is angular momentum around Earth’s center conserved for (g) the satellite and(h) the satellite–Earth system (assuming that system is isolated)?

(a) What is the gravitational potential energy of the two-particle system in Problem 3? If you triple the separation between theparticles, how much work is done (b) by the gravitational force between the particles and (c) by you?

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