Gravitation


  1. A geostationary satellite is orbiting the earth at a height of 5R above that surface of the earth, R being the radius of the earth. The time period of another satellite in hours at a height of 2R from the surface of the earth is :









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    ​According to Kelpner’s law of period T2 ∝ R3

    T12
    =
    R13
    =
    (6R)3
    = 8
    T22R23(3R)3

    24 × 24
    = 8
    T22

    T22 =
    24 × 24
    = 72 = 36 × 2
    8

    T2 = 6 √2

    Correct Option: C

    ​According to Kelpner’s law of period T2 ∝ R3

    T12
    =
    R13
    =
    (6R)3
    = 8
    T22R23(3R)3

    24 × 24
    = 8
    T22

    T22 =
    24 × 24
    = 72 = 36 × 2
    8

    T2 = 6 √2


  1. A particle of mass ‘m’ is kept at rest at a height 3R from the surface of earth, where ‘R’ is radius of earth and ‘M’ is mass of earth. The minimum speed with which it should be projected, so that it does not return back, is (g is acceleration due to gravity on the surface of earth)









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    As we know, the minimum speed with which a body is projected so that it does not return back is called escape speed.

    =
    GM
    1 / 2 (∵ h = 3R)
    6400

    Correct Option: B

    As we know, the minimum speed with which a body is projected so that it does not return back is called escape speed.

    =
    GM
    1 / 2 (∵ h = 3R)
    6400



  1. The radius of a planet is twice the radius of earth. Both have almost equal average mass-densities. If VP and VE are escape velocities of the planet and the earth, respectively, then









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    Escape velocity, Ve = R √(8 / 3) π GP

    ⇒ Ve ∝ R ⇒
    VP
    =
    RP
    = 2
    VERE

    ⇒ VP = 2 VE

    Correct Option: C

    Escape velocity, Ve = R √(8 / 3) π GP

    ⇒ Ve ∝ R ⇒
    VP
    =
    RP
    = 2
    VERE

    ⇒ VP = 2 VE


  1. A remote - sensing satellite of earth revolves in a circular orbit at a height of 0.25 × 106 m above the surface of earth. If earth's radius is 6.38 × 1066 m and g = 9.8 ms–2, then the orbital speed of the satellite is :​​​









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    Given : Height of the satellite from the earth's surface h = 0.25 × 106m ​
    Radius of the earth R = 6.38 × 106m ​
    Acceleration due to gravity g = 9.8 m/s2
    Orbital velocity, Vo = ?

    = 7.76 km/s ∵
    GM
    = g
    R2

    Correct Option: D

    Given : Height of the satellite from the earth's surface h = 0.25 × 106m ​
    Radius of the earth R = 6.38 × 106m ​
    Acceleration due to gravity g = 9.8 m/s2
    Orbital velocity, Vo = ?

    = 7.76 km/s ∵
    GM
    = g
    R2



  1. A satellite S is moving in an elliptical orbit around the earth. The mass of the satellite is very small compared to the mass of the earth. Then,​​​









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    The gravitational force on the satellite will be aiming towards the centre of the earth so acceleration of the satellite will also be aiming towards the centre of the earth.

    Correct Option: C

    The gravitational force on the satellite will be aiming towards the centre of the earth so acceleration of the satellite will also be aiming towards the centre of the earth.