Satellite following circular orbit.

AI Thread Summary
A satellite with a mass of 500 kg orbits Earth at a radius of 2r_e and is later moved to a radius of 3r_e. The gravitational potential energy must be calculated using the correct radius, which is the distance from Earth's center, not just the altitude above the surface. The change in gravitational potential energy and the work done in moving the satellite are related but distinct, as they also involve kinetic energy considerations. The calculations for the satellite's speed in the new orbit and escape velocity from Earth's surface can be done using standard gravitational equations. Understanding the distinction between radius and altitude is crucial for accurate calculations.
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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!
 
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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.
 
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