In order to make the effective acceleration due to gravity equal to zero at the equator, the angular velocity of rotation of the earth about its axis should be $(g = 10\,m{s^{ - 2}}$ and radius of earth is $6400 \,kms)$
$0\,\;rad\,{\sec ^{ - 1}}$
$\frac{1}{{800}}rad\,se{c^{ - 1}}$
$\frac{1}{{80}}rad\,se{c^{ - 1}}$
$\frac{1}{8}rad\,se{c^{ - 1}}$
When a body is taken from pole to the equator its weight
Two masses $m_1$ and $m_2$ start to move towards each other due to mutual gravitational force. If distance covered by $m_1$ is $x$, then the distance covered by $m_2$ is
A body of mass $m$ is situated at a distance equal to $2R$ ($R-$ radius of earth) from earth's surface. The minimum energy required to be given to the body so that it may escape out of earth's gravitational field will be
In a satellite if the time of revolution is $T$, then $K.E.$ is proportional to
Masses and radii of earth and moon are $M_1,\, M_2$ and $R_1,\, R_2$ respectively. The distance between their centre is $'d'$ . The minimum velocity given to mass $'M'$ from the mid point of line joining their centre so that it will escape