Two artificial satellites,
S1 and
S2 orbit the Earth in a circular
motion at distances, respectively, equal to
r1 =
R and
r2 = 3
R 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:
Solution
From Figure 1, we see that in the triangle Δ
ABC, 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 Δ
ABC 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
\( \overline{AC}=3R \)
\[
\begin{gather}
\bbox[#99CCFF,10px]
{c^{2}=a^{2}+b^{2}}
\end{gather}
\]
\[
\begin{gather}
(3R)^{2}=R^{2}+d^{2}\\[5pt]
9R^{2}=R^{2}+d^{2}\\[5pt]
d^{2}=9R^{2}-R^{2}\\[5pt]
d=\sqrt{8R^{2}}\\[5pt]
d=\sqrt{2^{3}R^{2}}
\end{gather}
\]
\[
\begin{gather}
\bbox[#FFCCCC,10px]
{d=2R\sqrt{2}}
\end{gather}
\]