If the escape velocity from the surface of the earth 11.2km/s find the critical velocity of the body orbiting close to the surface from the earth
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Hello dear,
◆ Answer -
vo = 7.92 km/s
● Explanation -
For satellite orbiting very close to the earth,
vo = √(gR)
Rearranging,
vo = √(2gR) / √2
As we know, ve = √(2gR), so now
vo = ve / √2
vo = 11.2 / √2
vo = 7.92 km/s
Therefore, the critical velocity of the body orbiting close to the surface from the earth is 7.92 km/s.
Thanks dear...
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