We are bounded in a nutshell of Infinite Space: Week 10: Worksheet #18:
Problem #1: Where's that moon?
1. Hill spheres. One outcome of planet
formation is systems of satellites around planets. Now you may ask yourself, why
do some planets have moons 10s of millions of kilometers away, while the
Earth’s moon is only 400,000 km away. To answer this question we need to think
about how big of a region around a planet is dominated by the gravity of a
planet, i.e. the region where the gravitational pull of the planet is more
important than the gravitational pull of the central star (or another planet).
a) Gravitational forces. Put a test mass
somewhere between a star of mass \(M_S\) and a planet of mass \(m_P\) at a distance \(r_P\) from the star. Make a drawing marking
clearly these characteristics as well as the distance r between the test particle and the planet. Write separate
expressions for the gravitational force on the particle from the star and on
the particle from the planet. At what distance r from the planet are the two forces balanced? This distance
approximates the radius of the Hill sphere, which in the case of planet
formation is the sphere of disk material which a planet can accrete from.
(b) Planetary Hill radii. Calculate the Hill
radii for Earth, Jupiter, and Neptune. How do they compare with the separation
between the planets and their most distant moons?
a. With
these hill spheres, the defining characteristic is the point of equilibrium at
which the point mass would be find between the two masses. This is expressed
with the law of universal gravitation: \[ F_{G_{r_P}} = F_{G_{r_P - r}} ,\] and
reconfiguring these equations, we find how: \[ \frac{G M_S m_{part} }{(r_P -
r)^2} = \frac{G m_P m_{part}}{r^2}\] \[\frac{M_S}{(r_P - r)^2} =
\frac{m_P}{r^2} \] \[\frac{r^2}{(r_P - r) ^2} = \frac{m_P}{M_S},\] which can be further simplified till finding: \[
\frac{r}{r_P - r} = \sqrt{\frac{m_P}{M_S}}\] \[ r = \sqrt{\frac{m_P}{M_S}} (r_P
- r)\] \[ r(1+ \sqrt{\frac{m_P}{M_S}}) = \sqrt{\frac{m_P}{M_S}} r_P ,\] and
thus we have \[ r = \frac{\sqrt{\frac{m_P}{M_S}} r_P}{ 1+
\sqrt{\frac{m_P}{M_S}}},\] which can be given a final derivation till a fairly
simple relationship emerges: \[ r = \frac{\sqrt{m_P} r_P }{ \sqrt{M_S} + \sqrt{m_P}}\]
b. Now, we
can take the equation we have found and find the hill radii for several planets
in our solar system. But first, let us define a couple of values, such as the
mass of the Earth: \[M _\oplus = 5.9 \times 10^{24} kg \] \[ M_\odot = 2 \times
10^{30} kg,\] and therefore: \[ 1 ~M_\odot = 3.3 \times 1- ^5 M_\oplus ,\]
similarly: \[ 1 ~AU = 1.5 \times 10^8 km\]
First, for the Earth itself, we can find its hill radius: \[ r_\oplus =
\frac{\sqrt{M_\oplus} r_P }{ \sqrt{M_S} + \sqrt{M_\oplus}},\] plugging in
values, we find that: \[ r_\oplus = \frac{\sqrt{1 M_\oplus} (1 ~ AU) }{
\sqrt{3.3 \times 10 ^5 M_\oplus } + \sqrt{ 1 M_\oplus}} ,\] \[ r_\oplus =
\frac{1}{5.7 \times 10^{2}}\] \[ r_\oplus \approx 2 \times 10^{-3} AU \approx 3 \times 10^5 km, \] and comparing it to the
radius at which the Moon is found, we see that the hill radius we have
calculated is similar to the actual distance to the Moon to a factor less than
2.
Now for Jupiter. Following the same process, we find that: \[ r_{Jup} =
\frac{\sqrt{M_{Jup}} r_P }{ \sqrt{M_S} + \sqrt{M_{Jup}}},\] \[ r_{Jup} =
\frac{\sqrt{320 M_\oplus} \cdot 5.2 ~AU} { \sqrt{3.3 \times 10^5 M_\oplus } + \sqrt{ 320 M_\oplus } },\] which means the hill radius is \[ r_{Jup} \approx
0.15 AU \approx 2.2 \times 10^7 km ,\] which which is practically the same as
the actual distance to (one of) the moons of Jupiter, \(2.4 \times 10^7 km\).
And finally Neptune, the hill radius is: \[ r_{Nep} =
\frac{\sqrt{M_{Nep}} r_{Nep} }{ \sqrt{M_S} + \sqrt{M_{Nep} } }\] \[ r_{Nep} =
\frac{\sqrt{17 M_\oplus} \cdot 30~ AU}{ \sqrt{3.3 \times 10^5 M_\oplus } + \sqrt{17 M_\oplus} },\] and therefore it results in:\[ r_{Nep} \approx
0.2 ~AU \approx 3 \times 10^7 km,\] which is but a factor less than two away
from the precise measurement of Neptune’s moon’s distance.
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