Angular momentum conservation — prove Kepler's second law

hard JEE-MAIN JEE-ADVANCED JEE Advanced 2022 3 min read

Question

Using the principle of conservation of angular momentum, prove Kepler’s second law — that a planet sweeps out equal areas in equal time intervals.

(JEE Advanced 2022, Paper 1 — this derivation connects two major topics)


Solution — Step by Step

The gravitational force on a planet of mass mm due to the Sun (mass MM) is:

F=GMmr2r^\vec{F} = -\frac{GMm}{r^2}\hat{r}

This force is directed along r^\hat{r} (the line joining the Sun and planet). A force that always points toward (or away from) a fixed point is called a central force.

Torque about the Sun:

τ=r×F=r×(GMmr2r^)=GMmr2(r×r^)=0\vec{\tau} = \vec{r} \times \vec{F} = \vec{r} \times \left(-\frac{GMm}{r^2}\hat{r}\right) = -\frac{GMm}{r^2}(\vec{r} \times \hat{r}) = 0

Since r\vec{r} and r^\hat{r} are parallel, their cross product is zero. Therefore, τ=0\vec{\tau} = 0 and angular momentum L\vec{L} is conserved.

In a small time dtdt, the planet moves by drd\vec{r}. The area swept out by the radius vector is:

dA=12r×dr=12r×vdtdA = \frac{1}{2}|\vec{r} \times d\vec{r}| = \frac{1}{2}|\vec{r} \times \vec{v}|\,dt

But L=m(r×v)\vec{L} = m(\vec{r} \times \vec{v}), so r×v=L/m|\vec{r} \times \vec{v}| = L/m.

dAdt=L2m\frac{dA}{dt} = \frac{L}{2m}

Since LL and mm are both constants, the areal velocity dA/dt=L/(2m)dA/dt = L/(2m) is constant.

This means the planet sweeps equal areas in equal time intervals — which is precisely Kepler’s second law.

dAdt=L2m=constant\boxed{\frac{dA}{dt} = \frac{L}{2m} = \text{constant}}

Why This Works

The proof rests on one physical fact: gravity is a central force. Central forces produce zero torque about the centre, which conserves angular momentum. Angular momentum conservation then directly implies constant areal velocity.

Notice that we never used the inverse-square nature of gravity — only that it’s central. This means Kepler’s second law holds for any central force, not just gravity. The inverse-square law is needed for the elliptical orbit shape (Kepler’s first law) and the T2a3T^2 \propto a^3 relation (third law), but equal areas in equal times follows from centrality alone.


Alternative Method

Using polar coordinates, v=r˙r^+rθ˙θ^\vec{v} = \dot{r}\hat{r} + r\dot{\theta}\hat{\theta}. Then:

L=mr×v=mr2θ˙L = m|\vec{r} \times \vec{v}| = mr^2\dot{\theta}

Area swept: dA=12r2dθdA = \frac{1}{2}r^2\,d\theta, so dAdt=12r2θ˙=L2m\frac{dA}{dt} = \frac{1}{2}r^2\dot{\theta} = \frac{L}{2m}.

In JEE Advanced, this derivation often appears as part of a larger problem — for example, “A comet’s speed at perihelion is v1v_1 at distance r1r_1. Find its speed at aphelion distance r2r_2.” The answer uses L=mr1v1=mr2v2L = mr_1v_1 = mr_2v_2, which is just angular momentum conservation — the same principle behind Kepler’s second law.


Common Mistake

Students sometimes try to “prove” Kepler’s second law using the formula for the area of an ellipse. That approach is circular — Kepler’s law is about the rate of sweeping area, not the total area. The correct approach requires calculus: compute dA/dtdA/dt and show it’s constant using angular momentum conservation.

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