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Urgent help needed, please! Circular motion
Suppose the surface (radius = r) of the space station is rotating at 42.7 m/s. What must be the value of r for the astronauts to weigh one-half of their Earth weight?
My soln: Let // represent square root
V = // (GMe/r)
I divided Me by 2 and made r the subject
r = GMe/V^2
but i got the anser wrong
Suppose the surface (radius = r) of the space station is rotating at 42.7 m/s. What must be the value of r for the astronauts to weigh one-half of their Earth weight?
My soln: Let // represent square root
V = // (GMe/r)
I divided Me by 2 and made r the subject
r = GMe/V^2
but i got the anser wrong