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I. Multiple Choice Questions · Q3

Q.A planet moving along an elliptical orbit is closest to the Sun at distance r1r_1 and farthest away at a distance of r2r_2. If v1v_1 and v2v_2 are linear speeds at these points respectively, then the ratio v1v2\dfrac{v_1}{v_2} is (NEET 2016)

(a) r2r1\dfrac{r_2}{r_1}
(b) (r2r1)2\left(\dfrac{r_2}{r_1}\right)^2
(c) r1r2\dfrac{r_1}{r_2}
(d) (r1r2)2\left(\dfrac{r_1}{r_2}\right)^2
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Step 1. At the closest point (r1r_1, perihelion) and farthest point (r2r_2, aphelion), the planet's velocity is exactly perpendicular to its position vector from the Sun (both are turning points, per Q1's reasoning).

Step 2. The planet's angular momentum about the Sun, L=mvrsin⁡θL=mvr\sin\theta, is conserved throughout the orbit (central force, zero torque). Since sin⁡θ=1\sin\theta=1 at both these points, L=mv1r1=mv2r2L=mv_1r_1=mv_2r_2.

Step 3. Cancelling mm: v1r1=v2r2  ⇒  v1v2=r2r1v_1r_1=v_2r_2 \;\Rightarrow\; \dfrac{v_1}{v_2}=\dfrac{r_2}{r_1}.

Step 4. This makes physical sense: r1<r2r_1<r_2 (closer to the Sun), so v1>v2v_1>v_2 -- the planet moves fastest when closest, exactly as Kepler's second law (law of areas) requires.

Step 5. Eliminating the others: (b) and (d) square the ratio, which would be the vis-viva-style relation for kinetic energy, not for the velocity ratio itself; (c) inverts the correct ratio.

✓Final answer

(a) r2r1\dfrac{r_2}{r_1}.

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