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QJEEM13Phac04: JEE Main 2013 Physics - Class 11 JEEM13Phac04 Solution: What is the minimum energy required to launch a satellite of…

What is the minimum energy required to launch a satellite of mass mm from the surface of a planet of mass MM and radius RR in a circular orbit at an altitude of 2R2R ?

Multiple Choice Options

  • A 5GmM6R{{5GmM} \over {6R}}
  • B 2GmM3R{{2GmM} \over {3R}}
  • C GmM2R{{GmM} \over {2R}}
  • D GmM3R{{GmM} \over {3R}}

Step-by-Step Verified Solution

Energy of the satellite on the surface of the planet

Ei = K.E + P.E = 0 + (−GMmR)\left( { - {{GMm} \over R}} \right) = −GMmR{ - {{GMm} \over R}}

Energy of the satellite at 2R distance from the surface of the planet while moving with velocity v

Ef = 12mv2{1 \over 2}m{v^2} + (−GMmR+2R)\left( { - {{GMm} \over {R + 2R}}} \right)

In the orbital of planet, the centripetal force is provided by the gravitational force

∴\therefore mv2R+2R=GMm(R+2R)2{{m{v^2}} \over {R + 2R}} = {{GMm} \over {{{\left( {R + 2R} \right)}^2}}}

⇒v2=GM3R\Rightarrow {v^2} = {{GM} \over {3R}}

∴\therefore Ef = 12mv2{1 \over 2}m{v^2} + (−GMmR+2R)\left( { - {{GMm} \over {R + 2R}}} \right)

=12mGM3R−GMm3R= {1 \over 2}m{{GM} \over {3R}} - {{GMm} \over {3R}}

= −GMm6R- {{GMm} \over {6R}}

∴\therefore Minimum energy required required to launch the satellite

= Ef - Ei

= −GMm6R- {{GMm} \over {6R}} - (−GMmR)\left( { - {{GMm} \over R}} \right)

= 5GMm6R{{5GMm} \over {6R}}

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