A spaceship is launched into a circular orbit of radius R close to the surface of the earth. The additional velocity to be imparted to the spaceship in the orbit to overcome the earth’s gravitational pull is (g → acceleration due to gravity)
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a
b
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d
answer is D.
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Detailed Solution
Escape velocity at a radial distance R from the cenre of earth.V0 = Orbital speed = Additional velocity = Ve - V0 ⇒ (√2 - 1)V0 =