Difference between potential energy on Earth and in orbit

In summary, the difference between potential on the surface of the Earth (R,M) and an object in orbit (r) about the Earth is GM/R-GM/r.
  • #1
Lorna
45
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Homework Statement



What is the difference between the potential on the surface of the Earth (R,M) and an object in orbit (r) about the earth.

Homework Equations





The Attempt at a Solution



potential on Earth = -GM/R
potential of object in orbit = -GM/r

diffrence = GM/R-GM/r

answer should be : GM/R-3GM/2r --- I don't understand where the 3/2 came from.

Thanks
 
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  • #2
Perhaps the 3/2 comes from the potential energy due to the Sun?
 
  • #3
The question should be - "where does the 1/2 GM/r come from?".

For an object "in orbit" it must be revolving, i.e. it has to have kinetic energy in addition to GPE, otherwise it would simply fall into the Mass providing the gravitational force.

For an object to be in orbit, mg = mv2/r, means g = v2/r or v2 = gr, and that object has kinetic energy 1/2 mv2 or 1/2 mgr.

g = GM/r2, so

KE = 1/2 m (GM/r2) r = 1/2 GMm/r

Also, check the form of the GPE

http://hyperphysics.phy-astr.gsu.edu/hbase/gpot.html#ui
 
  • #4
But they're not talking about the total energy, just the difference between the potential on the south pole of Earth and from distance r from the center of Earth.
 
  • #5
Where does the South Pole come into this. At the polls the effect of gravity is greater because one does not have the rotation of the Earth to offset some of the gravitational force.
 
  • #6
Hello,

Lorna said:
But they're not talking about the total energy, just the difference between the potential on the south pole of Earth and from distance r from the center of Earth.

The two are the same. Take a look at the problem statement again:

Lorna said:
What is the difference between the potential on the surface of the Earth (R,M) and an object in orbit (r) about the earth.

The "in orbit" is key. Gravitational potential is defined as the work required to move a mass from one point to another. Here, you want to move the object to a point on the surface of the earth. Since the object is in orbit, ie moving, you can't just drop it to the surface of the earth; there's going to be work required to slow it down to a stop, and this needs to be accounted for. Hence the kinetic term.

Hope this helps.
 
  • #7
I still don't know how they got the 3/2. Let me give you the exact question:

A satellite is in circular orbit of radius r about the Earth (Radius R, mass M). Astandard clock C on the satellite is compared with an identical clock C0 at the south pole on Earth. Show that the ratio of the rate of the orbiting clock to that of the clock on Earth is approximately:

1+(GM/Rc^2)-(3GM/2rc^2).

Note that the orbiting clock is faster only if r > 3/2 R, ir if r-R>3184 km.

--------------

The formula to find the rate is : 1+delta (potential)/c^2
so I have to find the diffrence between the potential
 
  • #8
Hello,

I'm not sure this is still an introductory physics problem :-)

Here's my take:

According to GR, the further into the gravitational well you get, the slower the clocks run. So if it were simply a matter of position in the well (gravitational potential), the Earth clock would -always- run more slowly (its deeper).

Now the hint states (and the answer shows) that the orbiting clock is faster only if [itex] r > \frac{3}{2}R[/itex], so there is an orbit where the clock is actually slower, counter to GR.

The formula you quote for the rate, that has to do with the potential, I suspect is only useful in finding the dilation due to the gravitational field. You still would need to apply the SR time dilations due to differing velocities, and I expect this will produce your 3/2 factor. If you re-read the problem, it simply asks for the the rate of the orbiting clock to the clock on earth, and doesn't specify which effects to ignore and which to include-- so you should probably address both of them.

So, again, I think ignoring the kinetic part is sinking you. I invite someone else to comment, as I'm not as up on this stuff as some others are.
 
  • #9
Thanks so much, but the formula is the I mensioned is correct according to my book because that's what it finds, the rate. I'll try posting the problem in advanced physics and see if anybody has an idea, because my instructor will probably put it in the final exam.
 

1. What is potential energy?

Potential energy is the energy that an object possesses due to its position or configuration. It is the energy that an object has the potential to convert into other forms of energy.

2. How does potential energy on Earth differ from potential energy in orbit?

Potential energy on Earth is the energy an object has due to its position relative to the Earth's surface and the force of gravity. In orbit, potential energy is the energy an object has due to its position relative to the center of mass of the planet or celestial body it is orbiting.

3. Why does potential energy increase as an object moves further from the Earth's surface?

This is because the force of gravity decreases as the distance between the object and the Earth's surface increases. As a result, the object has to do work against a smaller force to move away from the Earth, resulting in an increase in potential energy.

4. How does potential energy affect an object's motion in orbit?

In orbit, an object's potential energy is converted into kinetic energy as it moves towards the center of mass of the planet or celestial body it is orbiting. This kinetic energy then allows the object to maintain its orbit.

5. Can potential energy be converted into other forms of energy in orbit?

Yes, potential energy can be converted into kinetic energy in orbit, as well as other forms of energy such as thermal energy or electromagnetic energy. This can occur through various processes such as friction or collisions with other objects in orbit.

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