When the total energy of a satellite-planet system is positive,the satellite will .......

  • A
    Move around the planet in a circular orbit
  • B
    Move around the planet in an elliptical orbit
  • C
    Escape out with minimum speed
  • D
    Escape out with a speed greater than the escape velocity

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Similar Questions

Match Column-$I$ with Column-$II$.
Column-$I$ Column-$II$
$(1)$ Value of escape velocity on the surface of the Earth $(a)$ $2.38 \, km \, s^{-1}$
$(2)$ Value of escape velocity on the surface of the Moon $(b)$ $7.92 \, km \, s^{-1}$
$(c)$ $11.2 \, km \, s^{-1}$

The escape velocity of a rocket launched from the surface of the earth:

$A$ body is projected vertically upwards from the surface of a planet of radius $R$ with a velocity equal to half the escape velocity of that planet. Then,the maximum height attained by the body is

The masses and radii of the earth and moon are $(M_1, R_1)$ and $(M_2, R_2)$ respectively. Their centers are at a distance $r$ apart. Find the minimum escape velocity for a particle of mass $m$ to be projected from the midpoint between these two masses.

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