A) \[{{M}_{e}}\]
B) \[{{M}_{e}}\] only
C) \[\mu ,{{\mu }_{e}},V\]
D) \[{{M}_{e}},{{R}_{e}}\]and \[r\]
Correct Answer: D
Solution :
Orbital velocity \[({{v}_{0}})\] of a satellite orbiting in a circular orbit of radius r is given by \[{{v}_{0}}=\sqrt{\frac{G{{M}_{e}}}{r}}\] Hence, orbital velocity depends on \[{{M}_{e}},\,{{R}_{e}}\] and r.
You need to login to perform this action.
You will be redirected in
3 sec
