What Is the Magnitude of Satellite Acceleration Due to Gravity?

AI Thread Summary
The discussion focuses on calculating the acceleration due to gravity for synchronous communications satellites orbiting 3.59 x 10^7 m above the Earth's surface. The gravitational force is derived using the formula F = (G*m1*m2)/(r^2), with the correct parameters leading to an acceleration of 0.233 m/s². A key point highlighted is that the distance (r) in Newton's law of gravity should be measured from the Earth's center, not from the surface. An initial miscalculation resulted in an incorrect value of 0.309 m/s². The correction emphasizes the importance of accurately determining the radius in gravitational calculations.
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Homework Statement



Synchronus communications satellites are placed in a circular orbit that is 3.59 x 107 m above the Earth's surface. What is the magnitude of the acceleration due to gravity at this distance?

F=?
G=6.67259 x 10-11 N*m2/kg2
ME (Mass of Earth)= 5.98 x 1024 kg
r = 3.59 x107m

Homework Equations



F = (G*m1*m2)/(r2)
F = MA

The Attempt at a Solution



1) F = G * (ME2/r2) = 1.8514...N
2)F = MA --> (1.8514...N) = (5.98 x 1024)A
3) A = 0.309 m/s2

CORRECT ANSWER: 0.233 m/s2
 
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In Newton's law of gravity, r is the distance from the center of the earth, not the distance from the surface.
 
Doc Al said:
In Newton's law of gravity, r is the distance from the center of the earth, not the distance from the surface.

Ah, there's the problem. :P

Thanks. :D
 
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