We are bounded in a nutshell of Infinite Space: Week 8: Worksheet #13:
Problem #1: Turns out stars rotate within their solar system
1. (a) We
often say that planets orbit stars. But planets and their stars actually orbit
their mutual center of mass, which in general is given by xcom=Σimixi/Σimi . Set up the problem by drawing an x-axis with the
star at x=−a⋆ with mass M⋆, and the planet at x=aP
and mP. Also, set xcom=0. How do aP and a⋆ depend
on the masses of the star and planet?
(b) In a
two-body orbital system the variable a
is the mean semimajor axis, or the sum of the planet’s and star’s distances
away from their mutual center of mass: a=aP+a⋆. Label this on
your diagram. Now derive the relationship between the total mass M⋆+mP≈M⋆, orbital period P and the mean semimajor axis a, starting
with the Virial Theorem for a two-body orbit (assume circular orbits from here
on).
(c) By how
much is the Sun displaced from the Solar System’s center of mass (a.k.a. the
Solar System “barycenter”) as a result of Jupiter’s orbit? Express this
displacement in a useful unit such as Solar radii. (Potentially useful numbers M⊙≈1000MJup and aJup≈5.2AU.)
a. Taking
this problem as a simple center of mass problem, we can use the illustration
below:
and now we
can better understand the original sum equation: xcom=∑imixi∑imi, and identifying all the masses and their position
relative to the center: xcom=M⋆(a⋆)+mPaPM⋆+mP,
and setting xcom to 0: 0=M⋆(−a⋆)+mPaPM⋆+mP,
we continue simplifying −mPaPM⋆+mP=−M⋆a⋆M⋆+mP,
and a simpler equality begins to
emerge: mPaP=M⋆a⋆,
meaning we find a direct correlation of mass of an entangled system between the
objects’ masses and their semi-major axis of rotation: mPM⋆=a⋆aP
b.
Using
the virial theorem (similar to a problem directly involving the Orbital period
earlier in the semester) we can find the correlation of mass to Period, and
semi-major axis. Starting off with the base equation: K=−12U,
we begin representing these energy values with the objects in question, mainly
the gravitational potential energy and the kinetic energy (the movement of the
star at the center of the system is negligible here): 12mPv2=−12−GM⋆mPa⋆+aP,
and we take into account the definitions discussed by
the problem: M⋆+mP≈M⋆,
a⋆+aP=a,
which allow the previous equation to simplify
down to: v2=GM⋆a,
and now we define the velocity as a
rotational system: v=2πaP,
and plug this in: 4π2a2P2=GM⋆a,
which is then placed simplified
into a version of Kepler’s third law: P=(4π2a3GM⋆)13
c. Using
the equations we just derived, we know the proportion is mPM⋆=a⋆aP,
and we substitute in the values for the mass of
Jupiter and the axis of the orbit of Jupiter: 1/1000M⊙1M⊙=a⋆5.2AU,
which solves to: 5.2AU1000=a⋆
a⋆=5.2×10−3AU,
and knowing a particular
equivalence of: 1AU=214.94R⊙,
we can see how the Sun’s orbit is shifted by the mass of Jupiter by
the following distance: a⋆=1.1R⊙.
Correct.
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