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QJEEM20Phcdd2: JEE Main 2020 Physics - Class 11 JEEM20Phcdd2 Solution: A satellite of mass m is launched vertically upwards with an…

A satellite of mass m is launched vertically upwards with an initial speed u from the surface of the earth. After it reaches height R (R = radius of the earth), it ejects a rocket of mass m10{m \over {10}} so that subsequently the satellite moves in a circular orbit. The kinetic energy of the rocket is (G is the gravitational constant; M is the mass of the earth) :

Multiple Choice Options

  • A 3m8(u+5GM6R)2{{3m} \over 8}{\left( {u + \sqrt {{{5GM} \over {6R}}} } \right)^2}
  • B m20(u2+113100GMR){m \over {20}}\left( {{u^2} + {{113} \over {100}}{{GM} \over R}} \right)
  • C 5m(u2−119100GMR)5m\left( {{u^2} - {{119} \over {100}}{{GM} \over R}} \right)
  • D m20(u−2GM3R)2{m \over {20}}{\left( {u - \sqrt {{{2GM} \over {3R}}} } \right)^2}

Step-by-Step Verified Solution

JEE Main 2020 (Online) 7th January Morning Slot Physics - Gravitation Question 147 English Explanation 1
Using energy conservation

Ki + Ui = Kf + Uf

⇒\Rightarrow 12mu2−GmMR{1 \over 2}m{u^2} - {{GmM} \over R} = 12mv2−GmM2R{1 \over 2}m{v^2} - {{GmM} \over {2R}}

⇒\Rightarrow v = u2−GMR\sqrt {{u^2} - {{GM} \over R}} JEE Main 2020 (Online) 7th January Morning Slot Physics - Gravitation Question 147 English Explanation 2

After ejecting a rocket of mass m10{m \over {10}} the remaining part of mass 9m10{{9m} \over {10}} will rotate the earth with orbital velocity v0.

∴\therefore v0 = GM2R\sqrt {{{GM} \over {2R}}}

Applying momentum conservation along radial direction,

Before firing rocket momentum of satelite in radial direction = mv

And after firing rocket momentum of satelite in radial direction = 0 and momentum of rocket in radial direction = m10v2{m \over {10}}{v_2}

∴\therefore mv = m10v2{m \over {10}}{v_2}

⇒\Rightarrow v2 = 10v

Now applying momentum conservation along tangential direction we get,

0 = m10v1{m \over {10}}{v_1} - 9m10v0{{9m} \over {10}}{v_0}

⇒\Rightarrow 9m10v0{{9m} \over {10}}{v_0} = m10v1{m \over {10}}{v_1}

⇒\Rightarrow v1 = 9v0

∴\therefore Total Kinetic Energy of rocket

= 12m10(v12+v22){1 \over 2}{m \over {10}}\left( {v_1^2 + v_2^2} \right)

= 12m10(81v02+100v2){1 \over 2}{m \over {10}}\left( {81v_0^2 + 100{v^2}} \right)

= m20(81(GM2R)+100(u2−GMR)){m \over {20}}\left( {81\left( {{{GM} \over {2R}}} \right) + 100\left( {{u^2} - {{GM} \over R}} \right)} \right)

= m20(100u2+81GM2R−100GMR){m \over {20}}\left( {100{u^2} + {{81GM} \over {2R}} - {{100GM} \over R}} \right)

= m20(100u2−119GM2R){m \over {20}}\left( {100{u^2} - {{119GM} \over {2R}}} \right)

= 5m(u2−119GM200R)5m\left( {{u^2} - {{119GM} \over {200R}}} \right)

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