Question

what is the velocity of Pluto on elliptical and circular orbit. calculate it and compare it

what is the velocity of Pluto on elliptical and circular orbit. calculate it and compare it

Homework Answers

Answer #1

Accoring to the concept of the gravitation

velocity of the elliptical orbit Ve={GM(2/r-1/a)}^1/2

the velocity of the circular orbit Vr={GM/r)^1/2

Given that

mass of the sun M=1.989*10^30 kg

gravitational constant G=6.67*10^-11 N.m^2/kg^2

distance b/w sun to pluto r=150*10^9 m

semi major axis [a=39.5 AU=59.1*10^11 m]

now we find the velocity of the circular orbit

velocity Vc=(6.67*10^-11*1.989*10^30/150*10^9}^1/2=2.974*10^4 m/s

now we find the velocity of the elliptical orbit

Ve={6.67*10^-11*1.989*10^30[(2/150*10^9)-(1/59.1*10^11)}^1/2

={6.67*1.989*10^19[1.33*10^-11-0.02*10^-11]}^1/2

=4.2*10^4/2.974*10^4=1.41

Ve=1.41Vc

Ve/Vc=4.2*10^4/

Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
When installing a communication satellite, which type of orbit is preferred? Elliptical or circular? Why?
When installing a communication satellite, which type of orbit is preferred? Elliptical or circular? Why?
The existence of the dwarf planet Pluto was proposed based on irregularities in Neptune's orbit. Pluto...
The existence of the dwarf planet Pluto was proposed based on irregularities in Neptune's orbit. Pluto was subsequently discovered near its predicted position. But it now appears that the discovery was fortuitous, because Pluto is small and the irregularities in Neptune's orbit were not well known. To illustrate that Pluto has a minor effect on the orbit of Neptune compared with the closest planet to Neptune, answer the following questions. (a) Calculate the acceleration (in m/s2) due to gravity at...
An Apollo spacecraft describes a circular orbit with a 2414 km radius around the moon with...
An Apollo spacecraft describes a circular orbit with a 2414 km radius around the moon with a velocity of 5133 km/h. In order to transfer it to a smaller circular orbit with a 1930 km radius, the spacecraft is first placed on an elliptical path AB by reducing its velocity to 4827 km/h as it passes through A. Determine (a) the velocity of the spacecraft as it approaches B on the elliptic path, (b) the value to which its velocity...
What velocity is needed to launch a satellite into a circular orbit at an altitude of...
What velocity is needed to launch a satellite into a circular orbit at an altitude of 800 km above the surface of the Earth?
For an elliptical orbit, calculate the angular momentum L in terms of G, m1, m2, a...
For an elliptical orbit, calculate the angular momentum L in terms of G, m1, m2, a and e.
At a certain point in its elliptical orbit about the Sun, a planet receives a small...
At a certain point in its elliptical orbit about the Sun, a planet receives a small tangential impulse so that its velocity changes from v to v + δv, Find the resultant small changes in a, the semimajor axis. (Hint: You may find it helpful to approximate the planet’s orbits as nearly circular.)
A satellite, moving in an elliptical orbit, is 360 km above Earth’s surface at its farthest...
A satellite, moving in an elliptical orbit, is 360 km above Earth’s surface at its farthest point and 180 km above at its closest point. Calculate (a) the semimajor axis and (b) the eccentricity of the orbit. c.) period of the orbit, d.) the mechanical energy of the orbiting satellite e.) the velocity of the satellite at the closest point
Classical Mechanics problem: Assume Earth’s orbit is circular (a good approximation) and that the Sun’s mass...
Classical Mechanics problem: Assume Earth’s orbit is circular (a good approximation) and that the Sun’s mass suddenly decreases by half. Yikes! Will Earth escape the solar system and what type of orbit (circular, elliptical, parabolic or hyperbolic) will it have? Show your work
Consider a 1000 kg communication satellite that needs to be boosted from an orbit 330 km...
Consider a 1000 kg communication satellite that needs to be boosted from an orbit 330 km above the earth to a geosynchronous orbit 35,900 km above the earth. c) How much work must the rocket motor do to transfer the satellite from the circular orbit to the elliptical orbit? e) Now find the velocity v2 of the outer circular orbit. f) How much work must the rocket motor do to transfer the satellite from the elliptical orbit to the outer...
A satellite orbits the Earth uniformly in a circular orbit with a velocity of magnitude 4.00...
A satellite orbits the Earth uniformly in a circular orbit with a velocity of magnitude 4.00 km/s. Use Newton's gravitation force as the force in Newton's Law of Acceleration, using also the centripetal acceleration . Solve for radius r of the satellite's orbit in terms of v . (a) Find then the altitude of the satellite above the surface of the Earth. Earth's mass and radius are 5.9810 kg and 6.3810 km. (b) Find the time it takes the satellite...