From Patterns to Physics
January 27, 2026
By the end of this lecture, you will be able to:
Kepler told us what.
Newton told us why.
Part 1: Patterns Without Explanation
Kepler’s Empirical Laws
Imagine spending twenty years recording planet positions…
You discover three remarkable patterns:
But you have no idea why.
Planets move in ellipses with the Sun at one focus.
Key terms:
A line from planet to Sun sweeps equal areas in equal times.
Translation: Planets move faster near the Sun.
For orbits around a central mass: \(P^2 \propto a^3\)
What this means:
\[P^2 \propto a^3 \;\Rightarrow\; P \propto a^{3/2}\]
\[P = C \cdot a^{3/2}\]
\[\frac{P_2}{P_1} = \frac{\cancel{C} \cdot a_2^{3/2}}{\cancel{C} \cdot a_1^{3/2}} = \left(\frac{a_2}{a_1}\right)^{3/2}\]
Key: Proportionality hides an unknown constant. Dividing cancels it → true equality.
From the previous slide: \[\frac{P_2}{P_1} = \left(\frac{a_2}{a_1}\right)^{3/2}\]
Solve for \(P_2\): \[P_2 = P_1 \times \left(\frac{a_2}{a_1}\right)^{3/2}\]
This is the ratio method. If you know \(P_1\), \(a_1\), and \(a_2\), you can find \(P_2\) without knowing \(G\) or the central mass.
Given: \(a_\text{Mars} = 1.52\,\text{AU}\), \(a_\text{Earth} = 1\,\text{AU}\), \(P_\text{Earth} = 1\,\text{yr}\). Find: \(P_\text{Mars}\)
Start: \(P^2 \propto a^3\) → \(P \propto a^{3/2}\)
Ratio formula: \[P_2 = P_1 \times \left(\dfrac{a_2}{a_1}\right)^{3/2}\]
Let: 1 = Earth, 2 = Mars
Substitute with units: \[P_\text{Mars} = 1\,\text{yr} \times \left(\dfrac{1.52\,\cancel{\text{AU}}}{1\,\cancel{\text{AU}}}\right)^{3/2}\]
Calculate: \(1\,\text{yr} \times (1.52)^{3/2} = 1\,\text{yr} \times 1.87\)
\[\boxed{P_\text{Mars} = 1.87\,\text{yr}}\]
Avoid “\(P^2 = a^3\)” — this hides units and mass dependence!
The full physical law (Newton’s version):
\[P^2 = \frac{4\pi^2}{G(M+m)} a^3\]
The “shortcut” only works for Solar System orbits with \(m \ll M\) measured in years and AU around a ~\(1\,M_\odot\) star.
If you move a planet to twice its orbital distance, by what factor does its period increase?
A. 2× (linear)
B. 4× (squared)
C. 2.83× (\(2^{3/2}\))
D. 8× (cubed)
If you move a planet to twice its orbital distance, by what factor does its period increase?
From \(P^2 \propto a^3\): if \(a\) doubles, \(P^2 \to 2^3 = 8\), so \(P \to \sqrt{8} \approx 2.83\).
Empirical laws summarize data. They don’t explain physics.
Part 2: The Physics of Motion
Newton’s Laws + Circular Motion
First Law: Objects in motion stay in motion (unless acted on by a force)
Second Law: \(\vec{F} = m\vec{a}\)
Third Law: Every action has an equal and opposite reaction
\(\vec{F}\), \(\vec{v}\), \(\vec{a}\) have arrows because they’re vectors.
Speed: how fast
“30 km/s”
Velocity: how fast and which way
“30 km/s heading east”
Changing direction = changing velocity = acceleration
Even without speeding up!
An object moving in a circle at constant speed is accelerating.
Intuition: Faster motion → direction changes more rapidly. Tighter curve → direction changes more sharply. Both increase acceleration.
Centripetal acceleration: \[\boxed{a_c = \dfrac{v^2}{r}}\] (points toward center)
A car drives around a circular track at constant speedometer reading. Is the car accelerating?
A. Yes — direction is changing, so velocity is changing
B. No — speed is constant, so no acceleration
C. Only when the car speeds up or slows down
D. Only at certain points on the track
A car drives around a circular track at constant speedometer reading. Is the car accelerating?
Common misconception: confusing speed with velocity.
By \(F = ma\), if there’s acceleration, there must be a force:
\[F_c = ma_c = \frac{mv^2}{r}\]
Key insight: “Centripetal force” isn’t a new force—it’s the role played by whatever force pulls toward the center.
Part 3: Newton’s Law of Gravitation
From Patterns to Mechanism
\[F_g = \frac{Gm_1 m_2}{r^2}\]
“Every particle of matter in the universe attracts every other particle with a force that is proportional to the product of their masses and inversely proportional to the square of the distance between their centres.” — Newton, Principia (1687)
\(Gm_1 m_2\) (numerator)
More mass → more pull
Product of masses (Newton III)
\(r^2\) (denominator)
Inverse-square law
Double distance → 1/4 the force
\(G\) is the same everywhere in the universe — on Earth, on Mars, in distant galaxies.
Using \(F_g = \dfrac{Gm_1 m_2}{r^2}\):
If you double the distance between two masses, by what factor does the force change?
A. Halves (1/2)
B. Quarters (1/4)
C. Doubles (2×)
D. Unchanged
If you double the distance between two masses, by what factor does the force change?
Inverse-square: \((2r)^2 = 4r^2\), so force is 1/4.
He didn’t guess — he derived it from Kepler III.
The logic:
For circular orbit, gravity provides centripetal force:
\[k\frac{Mm}{r^n} = \frac{mv^2}{r}\]
Planet mass \(m\) cancels (same orbit speed regardless of mass!):
\[\frac{kM}{r^n} = \frac{v^2}{r}\]
Using \(v = \dfrac{2\pi r}{P}\) (circumference/period):
\[P^2 = \frac{4\pi^2}{kM} r^{n+1}\]
Compare to Kepler III: \(P^2 \propto r^3\)
\[n + 1 = 3 \quad \Rightarrow \quad \boxed{n = 2}\]
The inverse-square law is required by Kepler’s Third Law!
Our derivation assumed the Sun stays fixed while the planet orbits.
Is that true?
Newton’s Third Law says no. If the Sun pulls the planet, the planet pulls the Sun.
Both bodies must move.
Both bodies orbit their common center of mass (barycenter).
Balance condition: \[m_1 \, r_1 = m_2 \, r_2\]
The more massive body orbits closer to the center of mass.
When \(M \gg m\): barycenter ≈ center of \(M\)
(Kepler’s approximation)
From center of mass:
\[m_1 r_1 = m_2 r_2\]
Total separation:
\[r = r_1 + r_2\]
Solve for each distance:
\[r_1 = \frac{m_2}{m_1 + m_2}\, r\]
\[r_2 = \frac{m_1}{m_1 + m_2}\, r\]
Each body’s orbital radius depends on both masses through the total \((m_1 + m_2)\).
Gravity on body 2: \[F = \frac{Gm_1 m_2}{r^2}\]
Centripetal force for body 2: \[F = \frac{4\pi^2 m_2 r_2}{P^2}\]
Substitute \(r_2 = \dfrac{m_1 r}{m_1 + m_2}\):
\[\frac{Gm_1 m_2}{r^2} = \frac{4\pi^2 m_2}{P^2} \cdot \frac{m_1 r}{m_1 + m_2}\]
Cancel \(m_1 m_2\), solve for \(P^2\):
\[\boxed{P^2 = \frac{4\pi^2}{G(m_1 + m_2)} r^3}\]
\((m_1 + m_2)\) emerges because each body’s orbital radius depends on how mass is distributed.
Accounting for both bodies’ motion, Newton derived:
\[P^2 = \frac{4\pi^2}{G(M + m)} a^3\]
What’s new compared to Kepler?
Kepler didn’t notice because all his data came from one system — our Solar System.
Part 4: Orbital and Escape Velocity
How fast must you go?
For a circular orbit at radius \(r\) around mass \(M\):
\[\frac{GMm}{r^2} = \frac{mv_{orb}^2}{r}\]
Mass \(m\) cancels (a feather and bowling ball orbit at the same speed!):
\[\boxed{v_{orb} = \sqrt{\frac{GM}{r}}}\]
\[v_{orb} = \sqrt{\frac{GM}{r}}\]
Earth’s orbital velocity: \(v_{orb} \approx 30\) km/s
Given: \(M_\odot = 2 \times 10^{33}\,\text{g}\), \(r = 1.5 \times 10^{13}\,\text{cm}\), \(G = 6.67 \times 10^{-8}\,\frac{\text{cm}^3}{\text{g}\cdot\text{s}^2}\)
\[v_{orb} = \sqrt{\frac{GM_\odot}{r}} = \sqrt{\frac{(6.67 \times 10^{-8}\,\frac{\text{cm}^3}{\text{g}\cdot\text{s}^2})(2 \times 10^{33}\,\text{g})}{1.5 \times 10^{13}\,\text{cm}}}\]
Units: \(\sqrt{\dfrac{\text{cm}^3 \cdot \cancel{\text{g}}}{\cancel{\text{g}} \cdot \text{s}^2 \cdot \text{cm}}} = \sqrt{\dfrac{\text{cm}^{\cancel{3}2}}{\text{s}^2}} = \dfrac{\text{cm}}{\text{s}}\) ✓
Numbers: \(\sqrt{\frac{(6.67)(2)}{1.5} \times 10^{-8+33-13}} = \sqrt{8.9 \times 10^{12}} \approx 3 \times 10^6\,\frac{\text{cm}}{\text{s}} = 30\,\frac{\text{km}}{\text{s}}\)
Mechanics studies motion and the forces that cause it. Energy is the capacity to do work — to move things.
Kinetic Energy: energy of motion
\[K = \frac{1}{2}mv^2\]
Faster or more massive → more kinetic energy
Gravitational Potential Energy: energy of position in a gravitational field
\[U = -\frac{GMm}{r}\]
Closer to mass → more negative (deeper in the “well”)
We define zero at infinity. Far from any mass → \(U = 0\).
As you fall toward a mass:
The deeper in the well (smaller \(r\)) → the more negative \(U\) → the more you need to climb out.
To escape to infinity, you need enough kinetic energy to overcome gravity:
\[\frac{1}{2}mv_{esc}^2 = \frac{GMm}{r}\]
Solving (mass cancels again!):
\[\boxed{v_{esc} = \sqrt{\frac{2GM}{r}} = \sqrt{2} \cdot v_{orb}}\]
| Location | \(v_{orb}\) | \(v_{esc}\) |
|---|---|---|
| Earth surface | 7.9 km/s | 11.2 km/s |
| Moon surface | 1.7 km/s | 2.4 km/s |
| Sun surface | 434 km/s | 618 km/s |
Jupiter orbits at 5 AU from the Sun. Earth orbits at 1 AU. How does Jupiter’s orbital velocity compare to Earth’s?
Jupiter orbits at 5 AU from the Sun. Earth orbits at 1 AU. How does Jupiter’s orbital velocity compare to Earth’s?
From \(v_{orb} \propto 1/\sqrt{r}\): Earth is \(\sqrt{5} \approx 2.2\) times faster.
Part 5: Conservation Laws
Energy and Angular Momentum
Recall: \(K = \frac{1}{2}mv^2\) (positive) and \(U = -\frac{GMm}{r}\) (negative).
Total mechanical energy:
\[E = K + U = \frac{1}{2}mv^2 - \frac{GMm}{r}\]
The sign of \(E\) determines the orbit’s fate — we’ll see how next.
| Total Energy | Orbit Type |
|---|---|
| \(E < 0\) | Bound (ellipse/circle) |
| \(E = 0\) | Parabolic (just escapes) |
| \(E > 0\) | Hyperbolic (escapes with speed to spare) |
At perihelion: High \(K\), low \(U\) (fast, close)
At aphelion: Low \(K\), high \(U\) (slow, far)
Total \(E\): Always constant!
For orbital motion:
\[L = mvr = mr^2\dot{\phi} = \text{constant}\]
\(\dot{\phi}\) (“phi-dot”) = angular velocity = how fast the angle changes (rad/s). The dot means “per unit time.”
Two equivalent forms:
\(v = r\dot{\phi}\) (arc length per time), so both give the same \(L\).
Why conserved? Gravity is a central force—it exerts no torque (twisting force).
Areal velocity (rate of sweeping area):
\[\frac{dA}{dt} = \frac{L}{2m} = \text{constant}\]
Equal areas in equal times isn’t a separate law — it’s angular momentum conservation!
When \(r\) decreases, \(v\) must increase to keep \(L = mvr\) constant.
A planet has perihelion at 1 AU and aphelion at 4 AU. Using \(L = mvr = \text{const}\):
By what factor is the linear speed larger at perihelion?
A. 2× (ratio of distances)
B. 4× (ratio of distances)
C. 16× (ratio squared)
D. 8× (ratio cubed)
A planet has perihelion at 1 AU and aphelion at 4 AU. By what factor is the linear speed larger at perihelion?
From \(v_p r_p = v_a r_a\): \(v_p/v_a = r_a/r_p = 4/1 = 4\).
For bound systems, the virial theorem applies in two situations:
\[\langle K \rangle = -\frac{1}{2}\langle U \rangle\]
For circular orbit (instant = average):
\[K = \dfrac{GMm}{2r},~U = -\dfrac{GMm}{r} → K = -\frac{1}{2}U~✓\]
Where we use it:
When it doesn’t apply:
Part 6: The Big Picture
From Newton to Einstein
Before Newton: celestial physics ≠ terrestrial physics
After Newton: One physics, everywhere
| Kepler’s Laws | Newton’s Explanation |
|---|---|
| Ellipses | Solution under inverse-square gravity |
| Equal areas | Angular momentum conservation |
| \(P^2 \propto a^3\) | Requires inverse-square; constant = \(G\) × mass |
The physics of gravity connects to everything this semester:
| Topic | Connection |
|---|---|
| Binary Stars | Masses from orbits |
| Exoplanets | Transit timing, radial velocity |
| Stellar Structure | Virial theorem |
| Black Holes | Escape velocity → event horizon |
| Galaxies | Rotation curves → dark matter |
Newton’s framework is excellent… but not the final word.
| Newton’s View | Einstein’s View |
|---|---|
| Gravity is a force | Gravity is curved spacetime |
| Space/time are fixed | Space/time are dynamic |
| Objects feel a pull | Objects follow geodesics |
Einstein: “Mass tells spacetime how to curve; spacetime tells mass how to move.”
If you forget everything else from today, remember this:
Patterns become physics
Kepler found the what. Newton explained the why.
This transition — from empirical to physical — is how science works.
| Quantity | Equation |
|---|---|
| Grav. Force | \(F_g = \dfrac{Gm_1m_2}{r^2}\) |
| Orbital Velocity | \(v_{orb} = \sqrt{\dfrac{GM}{r}}\) |
| Escape Velocity | \(v_{esc} = \sqrt{2}\,v_{orb}\) |
| Kepler III | \(P^2 = \dfrac{4\pi^2}{G(M+m)}a^3\) |
| Quantity | Equation |
|---|---|
| Kinetic Energy | \(K = \frac{1}{2}mv^2\) |
| Potential Energy | \(U = -\dfrac{GMm}{r}\) |
| Total Energy | \(E = K + U\) |
| Angular Momentum | \(L = mvr\) |
| Virial Equilibrium | \(\langle K \rangle = -\frac{1}{2}\langle U \rangle\) |
Common questions at this point:
Next time: Light as information — blackbody radiation and stellar spectra
Before then:

ASTR 201 • Dr. Anna Rosen • Lecture 3