A rocket is launched from the Earth towards the Moon, following a straight trajectory, that joins the
centers of the two bodies. Since the mass of the Earth
ME is approximately 81 times the
mass of the Moon
MM, determine the point in the trajectory where the magnitude of the
gravitational fields due to the Earth and the Moon canceling each other out. Consider the Earth-Moon system
isolated from the rest of the Universe, the system is stationary and with the total mass of each body
concentrated at its center.
Problem data:
- Earth Mass: ME;
- Moon Mass: MM;
- Ratio between the masses of the Earth and the Moon: ME = 81MM .
Problem diagram:
As the problem considers the masses of the Earth and the Moon concentrated in their centers, the problem
reduces to two points representing the Earth and the Moon with a distance
d between them and the
rocket a point, of mass
m, at a distance
x from the Earth. (Figure 1).
We assume the positive direction oriented from Earth to Moon.
The gravitational force of attraction,
\( {\vec{F}}_{rE} \),
acts between the Earth and the rocket, and between the Moon and the rocket, the gravitational force of
attraction,
\( {\vec{F}}_{rM} \).
Solution
The force of gravitational attraction is given by
Newton's Law of Universal Gravitation
\[
\begin{gather}
\bbox[#99CCFF,10px]
{F_{G}=G\frac{Mm}{r^{2}}} \tag{I}
\end{gather}
\]
Applying expression (I) to the Earth-rocket system, where
r =
x
\[
\begin{gather}
F_{rE}=G\frac{M_{E}m}{x^{2}} \tag{II}
\end{gather}
\]
Applying again expression (I) to the Moon-rocket system, where
r =
d−
x
\[
\begin{gather}
F_{rM}=G\frac{M_{M}m}{(d-x)^{2}} \tag{III}
\end{gather}
\]
For the magnitude of the gravitational fields due to the Earth and the Moon to cancel each other out, we
must impose the following condition
\[
\begin{gather}
\sum F=0\\
F_{rM}-F_{rE}=0
\end{gather}
\]
substituting the expressions (II) and (III) into the expression above
\[
\begin{gather}
G\frac{M_{M}m}{(d-x)^{2}}-G\frac{M_{E}m}{x^{2}}=0\\[5pt]
\cancel{G}\frac{M_{M}\cancel{m}}{(d-x)^{2}}=\cancel{G}\frac{M_{E}\cancel{m}}{x^{2}}\\[5pt]
\frac{M_{M}}{(d-x)^{2}}=\frac{M_{E}}{x^{2}}
\end{gather}
\]
canceling the
Universal Gravitational Constant G and the rocket mass
m from both sides
of the equation, and substituting the ratio between the masses of the Earth and the Moon given in the
problem
\[
\begin{gather}
\frac{\cancel{M_{M}}}{(d-x)^{2}}=\frac{81 \cancel{M_{M}}}{x^{2}}\\[5pt]
\frac{1}{(d-x)^{2}}=\frac{81}{x^{2}}\\[5pt]
\frac{x^{2}}{(d-x)^{2}}=81\\[5pt]
\left[\frac{x}{d-x}\right]^{2}=81\\[5pt]
\frac{x}{d-x}=\sqrt{81\;}\\[5pt]
\frac{x}{d-x}=9\\x=9(d-x)\\[5pt]
x=9d-9x\\[5pt]
x+9x=9d\\[5pt]
10x=9d
\end{gather}
\]
\[
\begin{gather}
\bbox[#FFCCCC,10px]
{x=\frac{9}{10}d}
\end{gather}
\]