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A body of mass m is moving in a circular
orbit of radius R about a planet of mass
M. At some instant, it splits into two equal
masses. The first mass moves in a circular
orbit of radius \frac{R}{2}, and the other mass, in a
circular orbit of radius \frac{3R}{2} . The difference
between the final and initial total energies
is :

  • Option 1)

    -\frac{GMm}{2R}

     

     

     

  • Option 2)

    +\frac{GMm}{6R}

  • Option 3)

    \frac{GMm}{2R}

  • Option 4)

    -\frac{GMm}{6R}

 

Answers (2)

best_answer

As we learned

 

Graph of satellite -

E\rightarrow Energy\: of\: satellite

K\rightarrow Kinetic\: energy

U\rightarrow Potential\: energy

- wherein

Total Energy

E=-\frac{GMm}{2a}=const.

a=semi-major\: axis

 

  Energy in on or bit = \frac{Gm_{1}m_{2}}{2r}

Initial energy = \frac{4Mm}{2r}

final energy = \frac{-G(\frac{m}{2})\cdot M}{2\cdot \frac{R}{2}} - \frac{G(\frac{m}{2}).M}{2\cdot (\frac{3R}{2})} - \frac{GmM}{R}\left ( \frac{1}{2} + \frac{1}{6}\right )

\therefore Difference = E_{f - E_{i}}

=\frac{-GMm}{6R}


Option 1)

-\frac{GMm}{2R}

 

 

 

Option 2)

+\frac{GMm}{6R}

Option 3)

\frac{GMm}{2R}

Option 4)

-\frac{GMm}{6R}

Posted by

Avinash

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