Gravitational potential energy: derive expression for energy

AI Thread Summary
The discussion focuses on deriving expressions for gravitational potential energy needed to launch an object from Earth's surface to a height h and to achieve orbit at that height. The initial attempt at the solution incorrectly simplified the energy difference, leading to confusion about the role of Earth's radius in the calculations. After feedback, the correct approach involves careful algebra to find a common denominator when subtracting potential energy terms. For part B, it is clarified that additional energy is required not only to reach the orbital radius but also to achieve the necessary velocity for orbit, which involves kinetic energy considerations. The conversation emphasizes the importance of accurate algebraic manipulation in deriving the correct expressions.
MaryCate22
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Homework Statement


Part A:
Derive an expression for the energy needed to launch an object from the surface of Earth to a height h above the surface.

Part B:
Ignoring Earth's rotation, how much energy is needed to get the same object into orbit at height h?

Express your answer in terms of some or all of the variables h, mass of the object m, mass of Earth mE, its radius RE, and gravitational constant G.

Homework Equations


U=-GmmE/RE+h

The Attempt at a Solution


I figured that the energy you would need to bring the object to height h above the surface would equal the difference between the energy at the surface and the energy at h. I assume the object is at rest and the only energy it has is gravitational potential.

E=-GmmE/RE-(-GmmE/RE+h)...E=GmmE/h

This is not correct. Feedback I got was that the answer depends on RE. I've no idea how to go about part B.
 
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MaryCate22 said:

The Attempt at a Solution


I figured that the energy you would need to bring the object to height h above the surface would equal the difference between the energy at the surface and the energy at h. I assume the object is at rest and the only energy it has is gravitational potential.

E=-GmmE/RE-(-GmmE/RE+h)...E=GmmE/h

From this line, how did you reach the right side?

U = -\frac{Gmm_E}{R_E} - \left( - \frac{Gmm_E}{R_E +h} \right)

Your denominators don't cancel out.
 
MaryCate22 said:

Homework Statement


Part A:
Derive an expression for the energy needed to launch an object from the surface of Earth to a height h above the surface.

Part B:
Ignoring Earth's rotation, how much energy is needed to get the same object into orbit at height h?

Express your answer in terms of some or all of the variables h, mass of the object m, mass of Earth mE, its radius RE, and gravitational constant G.

Homework Equations


U=-GmmE/RE+h

The Attempt at a Solution


I figured that the energy you would need to bring the object to height h above the surface would equal the difference between the energy at the surface and the energy at h. I assume the object is at rest and the only energy it has is gravitational potential.

E=-GmmE/RE-(-GmmE/RE+h)...E=GmmE/h

This is not correct. Feedback I got was that the answer depends on RE. I've no idea how to go about part B.

U=-G*m*mE/(RE+h). Review your algebra about subtracting fractions! You are doing it wrong.
 
rock.freak667 said:
From this line, how did you reach the right side?

U = -\frac{Gmm_E}{R_E} - \left( - \frac{Gmm_E}{R_E +h} \right)

Your denominators don't cancel out.

E=(-GmmE/Re)+(GmmE/Re)+(GmmE/h) First two terms cancel? I may have forgotten basic algebra.
 
MaryCate22 said:
E=(-GmmE/Re)+(GmmE/Re)+(GmmE/h) First two terms cancel? I may have forgotten basic algebra.

Yes, forgotten basic algebra. a/(b+c) is not the same as a/b+a/c. Find a common denominator etc.
 
E=(-GmmE+h/Re+h)+(GmmE/Re+h)

Can't believe I did that. Can I add +h to the numerator and denominator of the first term? Is that finding a common denominator? Then I get E=h/(Re+h).
 
MaryCate22 said:
E=(-GmmE+h/Re+h)+(GmmE/Re+h)

Can't believe I did that. Can I add +h to the numerator and denominator of the first term? Is that finding a common denominator?

No, that's equally bad. a/b-c/d. Find common denominator, bd. Multiply first term by d/d, second by b/b getting ad/bd-bc/bd. Now you have a common denominator bd so you get (ad-bc)/bd. I hope this sounds familiar.
 
Dick said:
No, that's equally bad. a/b-c/d. Find common denominator, bd. Multiply first term by d/d, second by b/b getting ad/bd-bc/bd. Now you have a common denominator bd so you get (ad-bc)/bd. I hope this sounds familiar.

Reworked and got E= [-GmmE(Re+h)+Re(GmmE)]/Re(Re+h)=GmmEh/Re(Re+h)

Doing the algebra correctly, is the answer right? Is my reasoning sound? Sorry for forgetting elementary school, and thanks for your help.
 
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MaryCate22 said:
Reworked and got E= [-GmmE(Re+h)+Re(GmmE)]/Re(Re+h)=GmmEh/Re(Re+h)

Doing the algebra correctly, is the answer right? Is my reasoning sound? Sorry for forgetting elementary school, and thanks for your help.

Yes, that looks much better. For part B you need enough energy to reach the radius of the orbit and then more energy to get to the correct velocity to maintain that orbit.
 
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  • #10
Dick said:
Yes, that looks much better. For part B you need enough energy to reach the radius of the orbit and then more energy to get to the correct velocity to maintain that orbit.

Very helpful. I got to the right answer. Thank you!
 
  • #11
For part B, the energy that is extra and used to get the correct velocity, would that be kinetic or gravitational potential?
 
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