Change in momentum for a satellite in circular orbit

In summary, a satellite with mass 2200kg and orbit height 870km above Earth's surface is in a circular orbit passing over the North and South poles. The change in momentum from when it passes over the equator heading North to when it next passes over the equator can be calculated using the equations for centripetal force, period, and conservation of angular momentum. Despite the speed being constant in a circular orbit, the direction of the velocity changes, resulting in a quantifiable change in momentum.
  • #1
Peter Coe
3
0

Homework Statement



A satellite is in a circular orbit passing over the North and South geographical poles as it orbits the Earth. It has a mass of 2200kg and its orbit height is 870km above the Earth's surface. What is the change in momentum of the satellite from when it passes over the equator heading North, to when it next passes over the equator?[/B]

Homework Equations



m (satellite) = 2.2 x 10^3 kg
M (Earth) = 5.98 x 10^24 kg
R = r(earth) + h(satellite) = 6.37 x 10^6 m + 8.7 x 10^5 m = 7.24 x 10^6 m
G = 6.673 x 10^-11 m^3 kg^-1 s^-2

v = SQR (G)(M)/R
a = v^2/R
F(centripetal) = (m(satellite) x v^2)/r
T = (2pi x R)/v

m(1)v(1)r(1) = m(2)v(2)r(2) due to conservation of angular momentum.

The Attempt at a Solution



So v = 7.424 x 10^3 m/s and a = 7.61 m/s. T = 6.127 x 10^3 s or 1.7 hours. Centripetal force = 1.67 x 10^16 N

And here is where I got stuck. Isn't velocity constant in circular orbit? So why is there a change in momentum? Many thanks in advance.
 
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  • #2
Peter Coe said:
Isn't velocity constant in circular orbit? So why is there a change in momentum?
Is velocity a vector or a scalar?
 
  • #3
Peter Coe said:
Isn't velocity constant in circular orbit?
No, speed is constant, but velocity amd momentum are vectors.
There is also the subtlety that the Earth is orbiting the sun, so the satellite's orbit is not a simple circle, but I doubt the question intends you to worry about that.
 
  • #4
So I'd be wrong to say that the magnitude of the relative velocity does not change in circular orbit? I'm aware the nature of the direction does, and that velocity is a vector quantity - but how does that produce a quantifiable change in momentum?
 
  • #5
Peter Coe said:
I'm aware the nature of the direction does, and that velocity is a vector quantity - but how does that produce a quantifiable change in momentum?
Say you have a billiards ball moving to the right with velocity V. It hits another ball, and as a result ends up moving to the left with the same magnitude of velocity, but opposite direction.
Do you think there was a change in momentum in this case or not?
 
  • #6
Peter Coe said:
So I'd be wrong to say that the magnitude of the relative velocity does not change
No, you'd be right to say that, but the magnitude is the speed, and there is more to velocity than just speed.
Peter Coe said:
velocity is a vector quantity - but how does that produce a quantifiable change in momentum?
Suppose a particle starts with velocity ##\vec v##, and this consists of speed |v| in the +x direction. If it later still has speed |v| but is now traveling in the -x direction, what has been the change in velocity?
 
  • #7
haruspex said:
No, you'd be right to say that, but the magnitude is the speed, and there is more to velocity than just speed.

Suppose a particle starts with velocity ##\vec v##, and this consists of speed |v| in the +x direction. If it later still has speed |v| but is now traveling in the -x direction, what has been the change in velocity?
Bandersnatch said:
Say you have a billiards ball moving to the right with velocity V. It hits another ball, and as a result ends up moving to the left with the same magnitude of velocity, but opposite direction.
Do you think there was a change in momentum in this case or not?

Well the change in velocity/momentum would be a negative value relative to its original position. Ahhh, I see.. assign +ve and -ve.. Thanks
 

1. What is meant by "change in momentum" for a satellite in circular orbit?

Change in momentum refers to the change in the magnitude and direction of the satellite's momentum as a result of external forces acting on it. This can include changes in velocity, direction, or a combination of both.

2. How is the change in momentum for a satellite in circular orbit calculated?

The change in momentum for a satellite in circular orbit can be calculated using the formula Δp = mΔv, where Δp is the change in momentum, m is the mass of the satellite, and Δv is the change in velocity.

3. What causes a change in momentum for a satellite in circular orbit?

A change in momentum for a satellite in circular orbit can be caused by external forces such as gravitational pull from other objects, atmospheric drag, or thrust from the satellite's own propulsion system.

4. How does a change in momentum affect a satellite in circular orbit?

A change in momentum can affect a satellite in circular orbit by altering its trajectory, speed, and overall motion. This can lead to changes in the satellite's orbit and potentially impact its ability to perform its intended tasks.

5. Can a satellite in circular orbit maintain a constant change in momentum?

No, a satellite in circular orbit cannot maintain a constant change in momentum. This is because external forces acting on the satellite will continuously cause changes in momentum, which must be accounted for in order to maintain a stable orbit.

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