MCQOPTIONS
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| 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 | |