Gravitation
- A ball is dropped from a satellite revolving around the earth at a height of 120 km. The ball will
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The orbital speed of satellite is independent of mass of satellite, so the ball will behave as a satellite and will continue to move with the same speed in the original orbit.
Correct Option: B
The orbital speed of satellite is independent of mass of satellite, so the ball will behave as a satellite and will continue to move with the same speed in the original orbit.
- The escape velocity of a body on the surface of the earth is 11.2 km/s. If the earth’s mass increases to twice its present value and the radius of the earth becomes half, the escape velocity would become
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Escape velcocity
Given Me' = 2 Me and Re' = Re 2
= √4 = 2
ve' = 2 ve = × 11.2 = 22.4 km/sCorrect Option: B
Escape velcocity
Given Me' = 2 Me and Re' = Re 2
= √4 = 2
ve' = 2 ve = × 11.2 = 22.4 km/s
- The escape velocity of a sphere of mass m is given by (G = Universal gravitational constant; M = Mass of the earth and Re = Radius of the earth)
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Escape velocity is the minimum velocity with which a body is projected to escape from earth's gravitational field
1 mve2 = GMm mve2 ⇒ ve = √2GM / Re 2 Re Correct Option: B
Escape velocity is the minimum velocity with which a body is projected to escape from earth's gravitational field
1 mve2 = GMm mve2 ⇒ ve = √2GM / Re 2 Re
- The escape velocity on the surface of earth is 11.2 km/s. What would be the escape velocity on the surface of another planet of the same mass but 1/4 times the radius of the earth?
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vearth = √2GMe / Re
∴ vplanet = 2 × vearth = 2 × 11.2 = 22.4 km/sCorrect Option: A
vearth = √2GMe / Re
∴ vplanet = 2 × vearth = 2 × 11.2 = 22.4 km/s
- For a satellite moving in an orbit around the earth, the ratio of kinetic energy to potential energy is
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K.E. of satellite moving in an orbit around the earth is
K = 1 mv2 = 1 m √GM / r 2 = GMm 2 2 2r
P.E. of satellite and earth system isU = GMm ⇒ K = GMm 2r = 1 r U GMm 2 r
Correct Option: A
K.E. of satellite moving in an orbit around the earth is
K = 1 mv2 = 1 m √GM / r 2 = GMm 2 2 2r
P.E. of satellite and earth system isU = GMm ⇒ K = GMm 2r = 1 r U GMm 2 r