A satellite moves in a circular orbit of radius 4R round the earth. The acceleration of the satellite in terms of g is
A
\(\frac{g}{16}\)
B
\(\frac{g}{4}\)
C
\(\frac{4}{g}\)
D
\(\frac{16}{g}\)
Verified Correct Answer: A.
Physical Principles & Numerical Solution
\(\frac{g}{R^2}\) = \(\frac{g}{4^2}\) = \(\frac{g}{16}\)
Source: Myschool Past Questions Archive (Record #44663)