Calculate Satellite Velocity at 3600 km Above Earth

AI Thread Summary
To calculate the velocity of a satellite 3600 km above Earth's surface, it's essential to adjust for the change in gravitational acceleration at that altitude. The radius used in the circular motion equation should be the distance from the Earth's center, which is greater than 3600 km. The correct velocity is slightly higher than the initially calculated 5940 m/s. The formula v = √(GM/r) is recommended for accurate calculations, where G is the gravitational constant and M is the mass of the Earth. Accurate application of these principles is crucial for understanding satellite motion.
pb23me
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1. Homework Statement [/b]
calculate the velocity of a satellite 3600 km above the surface of the earth.


Homework Equations


Fnet= mg=ma
mg=ma
g=V2/r
r=3600000


The Attempt at a Solution

5940 m/s I am pretty sure this is correct just want to make sure.
 
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Looks good to me as long as you plugged in all the right values
 
Two things you need to include in your calculation:
1) at 3600 km above the surface of Earth, the acceleration due to gravity is not same as at the surface.
2) The radius in the circular motion equation is not 3600 km.
The correct value is a bit more than what you got.
 
Filip Larsen said:
Two things you need to include in your calculation:
1) at 3600 km above the surface of Earth, the acceleration due to gravity is not same as at the surface.
2) The radius in the circular motion equation is not 3600 km.
The correct value is a bit more than what you got.

You are right...but the equations are right, and as we all know that is all that matters once you start grad school :P haha
 
Just equate centripetal acceleration to the gravitational force at that height.
Better just remember the formula instead of deriving each time -

v = sq root (GM/r)

where G = grav constant, M= mass of earth, r = distance from centre of earth
 
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