Understanding Orbital Motion: Comparing Satellite Weights in Different Orbits

AI Thread Summary
The discussion focuses on calculating the acceleration of the Moon towards Earth and comparing the weights of two satellites in different orbits. The acceleration of the Moon can be derived from gravitational force equations, specifically using F_g = -GMm/r². For the two satellites, X and Y, which have equal mass but orbit at different radii, the weight ratio can be determined by applying gravitational force principles for each orbit. There is some clarification on the use of the negative sign in gravitational equations, emphasizing that it pertains to potential energy rather than force. Understanding these concepts is crucial for accurately analyzing orbital motion and satellite dynamics.
rachael
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q1. what is the acceleration of the moon towards the earth?
q2. Two satellites,X and Y, of equal mass are orbiting the Earth in orbits of radii r and 3r respectively. Find the ratios:
a. weight of satellite X/ weigh of satellite Y

thank you
 
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a1: I'm assuming you're modeling the orbits as circular motion, either way, try writing the forces acting on the two bodies (earth and the moon), and draw a figure that should help.

a2: similar to q1, except you have to do it twice, one for each satellite. now you'll have two equations and with the relationships of the radii given, you may solve for the masses.
hope this helps, sincerely, x
 
i don't get it
 
It might help you to know that
F_g= -\frac{GMm}{r^2}[/itex]<br /> where G is the universal gravitational constant, M and m are the masses of the objects and r is the distance between their centers.
 
I don't think it is F=-(GMm)/r²
there should'nt be a minus sign there.
You might have confused it with gravitational potential energy? U=-(GMm)/r
 
no, HallsofIvy's equation is correct.
 
my bad, without the minus sign is only a convention haha
 
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