The radii of circular orbits of two satellites A and B of the earth, are 4R and R, respectively. If the speed of satellite A is 3V, then the speed of satellite B will be
- 3V4
- 6V
- 12V
- 3V2
Answer
(2) 6V
Solution
Orbital speed: v = GMr
v 1 r
vBvA = rArB = 4RR = 2
vB = 2 3V = 6V
Answer: (2)