Solved Problem on Kepler's Laws and Gravitation
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Two artificial satellites, S1 and S2 orbit the Earth in a circular motion at distances, respectively, equal to r1 = R and r2 = 3R from their center. At a certain instant, the line connecting the centers of the satellites is tangent to the orbit of S1. Determine at this instant the distance d between S1 and S2.


Problem data:
  • Distance from satellite S1 to Earth:    r1 = R;
  • Distance from satellite S2 to Earth:    r2 = 3R.
Problem diagram:

Figure 1

Solution

From Figure 1, we see that in the triangle ΔABC, segment \( \overline{AB} \) is the distance from satellite S1 to Earth, segment \( \overline{AC} \) is the distance from satellite S2 to Earth, segment \( \overline{BC} \) connects the centers of the two satellites and is tangent to the orbit of S1 and perpendicular to \( \overline{AB} \), therefore the triangle ΔABC is a right triangle and the distance between the two satellites d, segment \( \overline{BC} \), will be given by the Pythagorean Theorem, we have the legs \( \overline{AB}=R \), \( \overline{BC}=d \) and the hypotenuse \( \overline{AC}=3R \)
\[ \begin{gather} \bbox[#99CCFF,10px] {c^{2}=a^{2}+b^{2}} \end{gather} \]
\[ \begin{gather} (3R)^{2}=R^{2}+d^{2}\\[5pt] 9R^{2}=R^{2}+d^{2}\\[5pt] d^{2}=9R^{2}-R^{2}\\[5pt] d=\sqrt{8R^{2}}\\[5pt] d=\sqrt{2^{3}R^{2}} \end{gather} \]
\[ \begin{gather} \bbox[#FFCCCC,10px] {d=2R\sqrt{2}} \end{gather} \]
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