Question

A body attains a height equal to the radius of the earth. The velocity of the body with which it was projected is

A. $$\sqrt {\frac{{GM}}{R}} $$  
B. $$\sqrt {\frac{{2GM}}{R}} $$
C. $$\sqrt {\frac{5}{4}\frac{{GM}}{R}} $$
D. $$\sqrt {\frac{{3GM}}{R}} $$
Answer :   $$\sqrt {\frac{{GM}}{R}} $$
Solution :
Energy at surface of the earth = energy at maximum height
or $$\left( {K + U} \right)$$  at the earth's surface $$= \left( {K + U} \right)$$   at maximum height
$$\therefore \frac{1}{2}m{u^2} - \frac{{GMm}}{R} = \frac{1}{2}m \times {\left( 0 \right)^2} - \frac{{GMm}}{{R + h}}$$
At maximum height it has only potential energy
or $$\frac{1}{2}m{u^2} = \frac{{GMm}}{R} - \frac{{GMm}}{{R + R}}\,\,\left( {\because h = R} \right)$$
$$\eqalign{ & {\text{or}}\,\,{u^2} = \frac{{2GM}}{R} - \frac{{2GM}}{{2R}} \cr & {\text{or}}\,\,{u^2} = \frac{{GM}}{R} \cr & \therefore u = \sqrt {\frac{{GM}}{R}} \cr} $$
Alternative
The expression for the speed with which a body should be projected so as to reach a height $$h$$ is $$u = \sqrt {\frac{{2gh}}{{1 + \left( {\frac{h}{R}} \right)}}} $$
Here, $$h = R$$  (given)
$$u = \sqrt {\frac{{2gR}}{{1 + \left( {\frac{R}{R}} \right)}}} = \sqrt {\frac{{2 \times \frac{{GM}}{{{R^2}}} \times R}}{2}} = \sqrt {\frac{{GM}}{R}} $$

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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