23. The critical orbital speed of
satellite in a near-Earth orbit is about
[R = 6400 km]
O 250 m/s
O
8 km/s
O
11 km/s
O 250 km/s
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Answer:
Given: velocity of satellite = vc = 6.8 km/s = 6.8 x 103 m/s, R = 6400 km = 6.4 x 106 m, g = 9.8 m/s2.
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