Gravitation
- The ratio of escape velocity at earth (ve) to the escape velocity at a planet (vp) whose radius and mean density are twice as that of earth is :
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As we know, escape velocity,
⇒ Vc = Rc √ρc / 2ρc Vp 2Rc ∴ Ratio Vc = 1 : 2 √2 Vp Correct Option: B
As we know, escape velocity,
⇒ Vc = Rc √ρc / 2ρc Vp 2Rc ∴ Ratio Vc = 1 : 2 √2 Vp
- With what velocity should a particle be projected so that its height becomes equal to radius of earth?
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From conservation of energy
1 mu2 - GMm = 1 m × (0)2 - GMm 2 R 2 R + R ⇒ u2 = 2GM - 2GM = GM R 2R R
Correct Option: A
From conservation of energy
1 mu2 - GMm = 1 m × (0)2 - GMm 2 R 2 R + R ⇒ u2 = 2GM - 2GM = GM R 2R R
- The potential energy of a satellite, having mass m and rotating at a height of 6.4 × 106 m from the earth surface, is
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Mass of the satellite = m and height of satellite from earth (h) = 6.4 × 106 m.
We know that gravitational potential energy of the satellite at heighth = - G Me m = - gRe2 m (Re + h) 2Re = - gRem = -0.5 mgRe 2
(where, GMe = gRe2 and h = Re)Correct Option: C
Mass of the satellite = m and height of satellite from earth (h) = 6.4 × 106 m.
We know that gravitational potential energy of the satellite at heighth = - G Me m = - gRe2 m (Re + h) 2Re = - gRem = -0.5 mgRe 2
(where, GMe = gRe2 and h = Re)
- Assuming the radius of the earth as R, the change in gravitational potential energy of a body of mass m, when it is taken from the earth's surface to a height 3R above its surface, is
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Gravitational potential energy (GPE) on the surface of earth,
E1 = - G M m R GPE at 3R, E2 = - G M m = - G M m (R + 3R) 4R ∴ Change in GPE = E2 - E1 = - GMm + GMm = 3GMm 4R R 4R = 3g R2m ∵ g = GM 4R R2 = 3 mg R 4 Correct Option: B
Gravitational potential energy (GPE) on the surface of earth,
E1 = - G M m R GPE at 3R, E2 = - G M m = - G M m (R + 3R) 4R ∴ Change in GPE = E2 - E1 = - GMm + GMm = 3GMm 4R R 4R = 3g R2m ∵ g = GM 4R R2 = 3 mg R 4