Q. A comet of mass $m$ moves in a highly elliptical orbit around the sun of mass $M$. The maximum and minimum distances of the comet from the centre of the sun are $r_{1}$ and $r_{2}$ respectively. The magnitude of angular momentum of the comet with respect to the centre of sun is

A) $\left\lbrack \frac{GMr_{1}}{\left( r_{1} + r_{2} \right)} \right\rbrack^{1/2}$
B) $\left\lbrack \frac{GM{mr}_{1}}{\left( r_{1} + r_{2} \right)} \right\rbrack^{1/2}$
C) $\left( \frac{2Gm^{2}r_{1}r_{2}}{r_{1} + r_{2}} \right)^{1/2}$
D) $\left( \frac{2G{Mm}^{2}r_{1}r_{2}}{r_{1} + r_{2}} \right)^{1/2}$
Explanation

(d) The gravitational force of sun on comet is radial, hence angular momentum is constant over the entire orbit. Using law of conservation of angular momentum, at locations $A$ and $B$
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$L = mv_{1}r_{1} = mv_{2}r_{2}$ or $v_{2} = \frac{v_{1}r_{1}}{r_{2}}$ …(i)
Using the principle of conservation of total energy at $A$ and $B$
$\frac{1}{2}mv_{1}^{2} - \frac{GMm}{r_{1}} = \frac{1}{2}m\ v_{2}^{2} - \frac{GMm}{r_{2}}$
or $v_{2}^{2} - v_{1}^{2} = 2GM\left( \frac{1}{r_{2}} - \frac{1}{r_{1}} \right)$ …(ii)
Putting the values from Eq. (i) in Eq. (ii) and solving, we get
$v_{1} = \left\lbrack \frac{2GMr_{2}}{r_{1}\left( r_{1} + r_{2} \right)} \right\rbrack^{1/2}$
$\therefore L = mv_{1}r_{1} = m\left\lbrack \frac{2GMr_{1}r_{2}}{\left( r_{1} + r_{2} \right)} \right\rbrack^{1/2}$

Dr. Abubacker
Reviewed by Dr. Abubacker

Physics Educator & NEET/JEE Specialist

Ph.D. in Physics with 19+ years of teaching experience.

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