1.

How many times is escape velocity \[({{V}_{e}})\], of orbital velocity \[({{V}_{0}})\] for a satellite revolving near earth       [RPMT 2000]

A.             \[\sqrt{2}\] times
B.               2 times
C.             3 times
D.               4 times
Answer» B.               2 times


Discussion

No Comment Found

Related MCQs