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
$\sqrt {\frac{{4G\left( {{M_1} + {M_2}} \right)}}{d}} $
$\sqrt {\frac{{4G}}{d}\frac{{{M_1}{M_2}}}{{({M_1} + {M_2})}}} $
$\sqrt {\frac{{2G}}{d}\left( {\frac{{{M_1} + {M_2}}}{{{M_1}{M_2}}}} \right)} $
$\sqrt {\frac{{2G}}{d}\left( {{M_1} + {M_2}} \right)} $
A geostationary satellite is orbiting the earth at a height of $6\, R$ from the earth’s surface ($R$ is the earth’s radius ). What is the period of rotation of another satellite at a height of $2.5\, R$ from the earth’s surface
If the radius of earth shrinks by $1.5 \%$ (mass remaining same), then the value of gravitational acceleration changes by ......... $\%$
The mass of planet is $\frac{1}{9}$ of the mass of the earth and its radius is half that of the earth. If a body weight $9\,N$ on the earth. Its weight on the planet would be ........ $N$
The dependence of acceleration due to gravity $g$ on the distance $r$ from the centre of the earth assumed to be a sphere of radius $R$ of uniform density is as shown figure below
The correct figure is
The orbital angular momentum of a satellite revolving at a distance $r$ from the centre is $L.$ If the distance is increased to $4r$ then the new angular momentum will be