Satellite following circular orbit.

Click For Summary

Homework Help Overview

The discussion revolves around a satellite in circular orbits around Earth, specifically analyzing gravitational potential energy and related calculations as the satellite transitions between two orbits with different radii.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning, Assumption checking

Approaches and Questions Raised

  • Participants explore the interpretation of orbital radius and its implications for gravitational potential energy calculations. Questions arise regarding whether to include the radius of Earth in the calculations and the distinction between gravitational potential energy and kinetic energy in the context of the problem.

Discussion Status

Some participants have provided clarifications on the definitions of radius and altitude, while others question the original poster's assumptions about the calculations. There is a recognition that the relationship between gravitational potential energy and kinetic energy needs to be considered, particularly in relation to the work done in moving the satellite.

Contextual Notes

Participants note the importance of understanding the definitions of radius and altitude in the context of orbital mechanics. There is also a mention of potential expectations from the instructor regarding the presentation of solutions.

dator
Messages
5
Reaction score
0

Homework Statement


A satellite with a mass of 5.00 x 10^2kg is in a circular orbit, whose radius is 2r_e, around earth. Then it is moved to a circular orbit with a radius of 3r_e.

a) Determine the satellite's gravitational potential energy from the first orbit to the second orbit.
b) Determine the change in gravitational potential energy from the first orbit to the second orbit.
c) Determine the work done in moving the satellite from the first orbit to the second orbit. Apply energy conservation.
d) Calculate the speed it would need in order to maintain its new orbit.
e) Calculate the escape velocity for the satellite if it is on the Earth's surface.


Homework Equations


E_p = -1(G*m_1*m_2)/r
(delta)E_p = -((G*m_1*m_2)/r) - (-((G*m_1*m_2)/r))
v = sqrt((G*m_planet)/r)
v_escape = sqrt((2*G*m_planet)/r)


The Attempt at a Solution


I worked out all the questions but I am wondering about the wording and if I should have considered a few things.

Questions a+b:
For the radius it lists 2r_e that is basically 2*(Radius of earth) correct?
And when calculating the potential gravitational energy, E_p will the radius be (2r_e+Radius of earth)? The question says "whose radius is 2r_e, around Earth" implying that you would add the radius of Earth on top of the multiplication.

So E_p_i = -(G*m_earth*m_satellite)/(2*r_e+r_e)

Question c:
Isn't this just the result of question b?

d+e:
no problems here just plug into the eqn and solve.

Thanks in advance!
 
Physics news on Phys.org
Radius means distance from the center. Altitude means height above the surface.
 
D H said:
Radius means distance from the center. Altitude means height above the surface.

Thank you!
 
an orbital radius is typically measured from the center of the object that it is orbiting. if the orbital radius is 2r_e then use 2*(radius of earth) not 3*. I understand your interpretation, but I think it's incorrect.

question c: looks like it to me. your teacher probably wants some statement or equation as proof though.
 
dator said:
Question c:
Isn't this just the result of question b?
No. Question (b) is about gravitational potential energy only. There is also kinetic energy to consider.
 

Similar threads

  • · Replies 16 ·
Replies
16
Views
3K
Replies
5
Views
3K
Replies
5
Views
3K
Replies
1
Views
2K
  • · Replies 3 ·
Replies
3
Views
2K
  • · Replies 3 ·
Replies
3
Views
3K
Replies
5
Views
3K
  • · Replies 6 ·
Replies
6
Views
3K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 15 ·
Replies
15
Views
2K