Question

The escape velocity from the surface of the earth is $${v_e}.$$ The escape velocity from the surface of a planet whose mass and radius are three times those of the earth, will be

A. $${v_e}$$  
B. $$3{v_e}$$
C. $$9{v_e}$$
D. $$\frac{1}{{3{v_e}}}$$
Answer :   $${v_e}$$
Solution :
Escape velocity on surface of the earth is given by
$${v_e} = \sqrt {2g{R_e}} = \sqrt {\frac{{2G{M_e}}}{{{R_e}}}} \,\,\left( {\because g = \frac{{G{M_e}}}{{R_e^2}}} \right)$$
where, $${M_e} =$$  mass of earth
$${R_e} =$$  radius of the earth
$$G =$$  gravitational constant
$$\therefore {v_e} \propto \sqrt {\frac{{{M_e}}}{{{R_e}}}} $$
If $${v_p}$$ is escape velocity from the surface of the planet, then $$\frac{{{v_e}}}{{{v_p}}} = \sqrt {\frac{{{M_e}}}{{{R_e}}}} \times \sqrt {\frac{{{R_p}}}{{{M_p}}}} $$
where, $${M_p}$$ is mass of the planet and $${R_p}$$ is radius of the planet.
but $${R_p} = 3{R_e}\,\,\left( {{\text{given}}} \right)$$
and $${M_p} = 3{M_e}$$
$$\eqalign{ & \therefore \frac{{{v_e}}}{{{v_p}}} = \sqrt {\frac{{{M_e}}}{{{R_e}}}} \times \sqrt {\frac{{3{R_e}}}{{3{M_e}}}} = \frac{1}{1} = 1 \cr & {\text{or}}\,\,{v_p} = {v_e} \cr} $$

Releted MCQ Question on
Basic Physics >> Gravitation

Releted Question 1

If the radius of the earth were to shrink by one percent, its mass remaining the same, the acceleration due to gravity on the earth’s surface would-

A. Decrease
B. Remain unchanged
C. Increase
D. Be zero
Releted Question 2

If $$g$$ is the acceleration due to gravity on the earth’s surface, the gain in the potential energy of an object of mass $$m$$ raised from the surface of the earth to a height equal to the radius $$R$$ of the earth, is-

A. $$\frac{1}{2}\,mgR$$
B. $$2\,mgR$$
C. $$mgR$$
D. $$\frac{1}{4}mgR$$
Releted Question 3

If the distance between the earth and the sun were half its present value, the number of days in a year would have been-

A. $$64.5$$
B. $$129$$
C. $$182.5$$
D. $$730$$
Releted Question 4

A geo-stationary satellite orbits around the earth in a circular orbit of radius $$36,000 \,km.$$   Then, the time period of a spy satellite orbiting a few hundred km above the earth's surface $$\left( {{R_{earth}} = 6400\,km} \right)$$    will approximately be-

A. $$\frac{1}{2}\,hr$$
B. $$1 \,hr$$
C. $$2 \,hr$$
D. $$4 \,hr$$

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Gravitation


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