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

6×1024kgA planet of mass orbits a star in a highly elliptical orbit. At a particular instant the velocity of the planet is (4.5×104,-1.7×104,0)m/s, and the force on the planet by the star is (1.5×1022,1.9×1023,0)N. FindFandF

Short Answer

Expert verified

-4.95×1022,1.87×1022,0Nand6.45×1022,1.71×1023,0N

Step by step solution

01

Identification of the given data 

The given data is listed below as,

  • The velocity of the planet is,v=(4.5×104,-1.7×104,0)m/s
  • The mass of the planet is,m=6×1024kg
  • The force exerted by the star is,F=(1.5×1022,1.9×1023,0)N
02

Significance of the parallel force

The parallel force mainly acts in the same or the opposite direction at some points of an object.

From the momentum principle, the equation of the parallel component of the force is expressed as,

F=|F|cosθp^

Here,F is the parallel force,|F| is the absolute value of the gravitational force, p^is the unit vector, andθ is the angle between the momentum and gravitational force.

03

Determination of the parallel and the perpendicular force of the planet

The momentum of the planet is expressed as,

p=mv

Here, mis the mass and vis the velocity.

For m=6×1024kgandv=4.5×104,-1.7×104,0m/s.

p=6×1024kg×4.5×104,-1.7×104,0m/s=2.7×1029,-1.02×1029,0kg·m/s

The magnitude of the momentum of the planet can be expressed as,

p=px2+py2+pz2

Here role="math" localid="1658048840021" px,pyandpzand are the momentum at the , x,yand zdirection respectively.

For px=2.7×1029kg·m/s,py=-1.02×1029kg·m/sandpz=0

p=2.7×1029kg·m/s2+-1.02×1029kg·m/s+(0)2=2.886×1029kg·m/s

Write the expression for the unit vector p^.

p^=pp

Here, p^is the momentum of the planet and pis the magnitude of the momentum.

For p=2.7×1029,-1.02×1029,0kg·m/sandp=2.886×1029kg·m/s,

p^=p=2.7×1029,-1.02×1029,0kg·m/s2.886×1029kg·m/s=(0.9355,-0.353,0)

Rewriting equation (1).

F11=(F·p^)p^

For F=1.5×1022,1.9×1023,0Nandp^=(0.9355,-0.353,0)

F=1.5×1022,1.9×1023,0N×(0.9355,-0.353,0)×(0.9355,-0.353,0)=1.4×1022N-6.7×1022N×(0.9355,-0.353,0)=-5.3×1022N×(0.9355,-0.353,0)=-4.95×1022,1.87×1022,0N

04

Determination of the perpendicular force of the planet

The equation of force for the planet can be expressed as,

Fnet=F+FF=Fnat-F

For F=1.5×1022,1.9×1023,0NandF=-4.95×1022,1.87×1022,0N,

F=1.5×1022,1.9×1023,0N--4.95×1022,1.87×1022,0N=6.45×1022,1.71×1023,0N

Thus, the values of FandFare-4.95×1022,1.87×1022,0Nand

6.45×1022,1.71×1023,0N respectively.

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

P49 The Ferris wheel in Figure 5.80is a vertical, circular amusement ride with radius 10m . Riders sit on seats that swivel to remain horizontal. The Ferris wheel rotates at a constant rate, going around once in 10.5s. Consider a rider whose mass is 56kg .

(a) At the bottom of the ride, what is the rate of change of the rider's momentum? (b) At the bottom of the ride, what is the vector gravitational force exerted by the Earth on the rider?

(c) At the bottom of the ride, what is the vector force exerted by the seat on the rider?

(d) Next consider the situation at the top of the ride. At the top of the ride, what is the rate of change of the rider's momentum?

(e) At the top of the ride, what is the vector gravitational force exerted by the Earth on the rider?

(f) At the top of the ride, what is the vector force exerted by the seat on the rider?

A rider feels heavier if the electric, interatomic contact force of the seat on the rider is larger than the rider's weight mg (and the rider sinks more deeply into the seat cushion). A rider feels lighter if the contact force of the seat is smaller than the rider's weight (and the rider does not sink as far into the seat cushion).

(g) Does a rider feel heavier or lighter at the bottom of a Ferris wheel ride?

(h) Does a rider feel heavier or lighter at the top of a Ferris wheel ride?

(a) Many communication satellites are placed in a circular orbit around the Earth at a radius where the period (the time to go around the Earth once) is\(24\;{\rm{h}}\). If the satellite is above some point on the equator, it stays above that point as the Earth rotates, so that as viewed from the rotating Earth the satellite appears to be motionless. That is why you see dish antennas pointing at a fixed point in space. Calculate the radius of the orbit of such a "synchronous" satellite. Explain your calculation in detail.

(b) Electromagnetic radiation including light and radio waves travels at a speed of\(3 \times {10^8}\;{\rm{m}}/{\rm{s}}\). If a phone call is routed through a synchronous satellite to someone not very far from you on the ground, what is the minimum delay between saying something and getting a response? Explain. Include in your explanation a diagram of the situation.

(c) Some human-made satellites are placed in "near-Earth" orbit, just high enough to be above almost all of the atmosphere. Calculate how long it takes for such a satellite to go around the Earth once, and explain any approximations you make.

(d) Calculate the orbital speed for a near-Earth orbit, which must be provided by the launch rocket. (The advantages of near-Earth communications satellites include making the signal delay unnoticeable, but with the disadvantage of having to track the satellites actively and having to use many satellites to ensure that at least one is always visible over a particular region.)

(e) When the first two astronauts landed on the Moon, a third astronaut remained in an orbiter in circular orbit near the Moon's surface. During half of every complete orbit, the orbiter was behind the Moon and out of radio contact with the Earth. On each orbit, how long was the time when radio contact was lost?

A proton moving in a magnetic field follows the curving path shown in Figure. The dashed circle is the kissing circle tangent to the path when the proton is at location A. The proton is traveling at a constant speed of 7.0 x 105 m/s, and the radius of the kissing circle is 0.08m . The mass of a proton is 1.7 x 10-27kg . Refer to the directional arrows shown at the right in Figure when answering the questions below.

(a) When the proton is at location A, what are the magnitude and direction of (dp/dt)p^ , the parallel component of (dp/dt)?

(b) When the proton is at location A, what are the magnitude and direction of |p|p^/dl , the perpendicular component of(dp/dt) ?

The planets in our Solar System have orbits around the Sun that are nearly circular, and v<<c.Calculate the period T(a year-the time required to go around the Sun once) for a planet whose orbit radius is r. This is the relationship discovered by Kepler and explained by Newton. (It can be shown by advanced techniques that this result also applies to elliptical orbits if you replaceby the semi major axis, which is half the longer, major axis of the ellipse.) Use this analytical solution for circular motion to predict the Earth's orbital speed, using the data for Sun and Earth on the inside back cover of the textbook.

The radius of a merry-go round is 11m, and it takes 12s to go around one. What is the speed of an atom in the outer rim?

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