Question 12.109: Based on observations made during the 1996 sighting of comet...

Based on observations made during the 1996 sighting of comet Hyakutake, it was concluded that the trajectory of the comet is a highly elongated ellipse for which the eccentricity is approximately \varepsilon=0.999887. Knowing that for the 1996 sighting the minimum distance between the comet and the sun was 0.230{ R }_{ E }, where { R }_{ E } is the mean distance from the sun to the earth, determine the periodic time of the comet.

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For Earth’s orbit about the sun,

\nu_{0}=\sqrt{\frac{G M}{R_{E}}}, \quad \tau_{0}=\frac{2 \pi R_{E}}{\nu_{0}}=\frac{2 \pi R_{E}^{3 / 2}}{\sqrt{G M}} \quad \text { or } \quad \sqrt{G M}=\frac{2 \pi R_{E}^{3 / 2}}{\tau_{0}}    (1)

For the comet Hyakutake,

\begin{aligned}\frac{1}{r_{0}} & =\frac{G M}{h^{2}}=(1+\varepsilon), \quad \frac{1}{r_{1}}=\frac{G M}{h^{2}}(1+\varepsilon), \quad r_{1}=\frac{1+\varepsilon}{1-\varepsilon} r_{0} \\a & =\frac{1}{2}\left(r_{0}+r_{1}\right)=\frac{r_{0}}{1-\varepsilon}, \quad b=\sqrt{r_{0} r_{1}}=\sqrt{\frac{1+\varepsilon}{1-\varepsilon}} r_{0} \\h & =\sqrt{G M r_{0}(1+\varepsilon)} \\\tau & =\frac{2 \pi a b}{h}=\frac{2 \pi r_{0}^{2}(1+\varepsilon)^{1 / 2}}{(1-\varepsilon)^{3 / 2} \sqrt{G M r_{0}(1+\varepsilon)}} \\& =\frac{2 \pi r_{0}^{3 / 2}}{\sqrt{G M(1-\varepsilon)^{3 / 2}}}=\frac{2 \pi r_{0}^{3 / 2} \tau_{0}}{2 \pi R_{E}^{3}(1-\varepsilon)^{3 / 2}} \\& =\left\lgroup\frac{r_{0}}{R_{E}}\right\rgroup^{3 / 2} \frac{1}{(1-\varepsilon)^{3 / 2}} \tau_{0} \\& =(0.230)^{3 / 2} \frac{1}{(1-0.999887)^{3 / 2}} \tau_{0}=91.8 \times 10^{3} \tau_{0}\end{aligned}

Since \quad\quad\tau_{0}=1 \mathrm{\ yr}, \tau=\left(91.8 \times 10^{3}\right)(1.000)

\tau=91.8 \times 10^{3} \mathrm{\ yr}\blacktriangleleft

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