If ve is escape velocity and vo is orbital velocity of a satellite for orbit close to the earth's surface, then these are related by
- vo = 2ve
- vo = ve
- ve = 2vo
- ve = 2 vo
Answer
(4) ve = 2 vo
Solution
Orbital velocity close to the earth's surface: vo = gR
Escape velocity: ve = 2gR
ve = 2 vo
Answer: (4)