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The mean radius of earth is R, its angular speed on its own axis is ω and the acceleration due to gravity at earth's surface is g. What will be the radius of the orbit of a geostationary satellite ?
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- (R2g / ω2)1 / 3
- (Rg / ω2)1 / 3
- (R2 ω2 / g)1 / 3
- (R2g / ω)1 / 3
- (R2g / ω2)1 / 3
Correct Option: A
T = | = | = | = | |||||
v0 | (gR2 / r)1 / 2 | (gR2)1 / 2 | ω |
Hence , r3 / 2 = | or r3 = | |||
ω | ω2 |
or r = (gR2 / ω2)1 / 3