write the expression for centripetal
acceleration.
a = v^2/r
Where v is the velocity of the satellite and r is the
radius of the orbit.
Since we are near the surface we can take the altitude of
the satellite to be 0 so the radius of it's orbit will be the same
as the radius of the moon.
Circumference = 2*pi*r = 2*pi*1.74x10^6 = 1.093x10^7
m
Period = 110 minutes = 6600 seconds
v = C/Period = 1.093x10^7/6600 = 1.656x10^3
m/s
a = (1.656x10^3)^2/1.74x10^6 = 1.57 m/s^2
So the acceleration at the moon's surface would be
approximately 1.57 m/s^2
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