Planets and Satellites: Kepler's Laws — Question 4

Section 13-6 · Physics pages 1998–1999

Question 4 Orbital period depends on semimajor axis rather than eccentricity Two small bodies orbit the same central mass. Body A has period TA and semimajor axis aA; body B has period 8TA. Use T 2 = 4π2a3/(GM). M 2aB rp,B An eccentric orbit can have a small periapsis even when its semimajor axis and period are large; schematic focus offset. (a) Find aB/aA. (b) If B has eccentricity .75, compare its periapsis radius with aA and explain why its long period does not imply it is always farther away.
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Question 4 - Solution Orbital period depends on semimajor axis rather than eccentricity M 2aB rp,B (a) Derivation and calculation For the same central mass, T 2 B T 2 A = a3 B a3 A . Since TB/TA = 8, aB aA = 82/3 = 4 . (b) Result and interpretation With eB = .75, rp,B = aB(1 −eB) = 4aA(.25) = aA . The far apsis is ra,B = aB(1 + eB) = 4aA(1.75) = 7aA. Thus the long period is compatible with an approach to aA; the body spends much of its orbit at larger radii. Physical check The apsis average is (aA + 7aA)/2 = 4aA, recovering the inferred semimajor axis.

Question 4

Orbital period depends on semimajor axis rather than eccentricity

Two small bodies orbit the same central mass. Body A has period TAT_A and semimajor axis aAa_A; body B has period 8TA8T_A. Use T2=4π2a3/(GM)T^2=4\pi^2a^3/(GM).

Diagram shown in the original SVG worksheet.

  1. Find aB/aAa_B/a_A.

  2. If B has eccentricity .75.75, compare its periapsis radius with aAa_A and explain why its long period does not imply it is always farther away.

Question 4 - Solution

Orbital period depends on semimajor axis rather than eccentricity

Diagram shown in the original SVG worksheet.

(a) Derivation and calculation

For the same central mass, TB2TA2=aB3aA3.\frac{T_B^2}{T_A^2}=\frac{a_B^3}{a_A^3}. Since TB/TA=8T_B/T_A=8, aBaA=82/3=4.\boxed{\frac{a_B}{a_A}=8^{2/3}=4}.

(b) Result and interpretation

With eB=.75e_B=.75, rp,B=aB(1−eB)=4aA(.25)=aA.\boxed{r_{p,B}=a_B(1-e_B)=4a_A(.25)=a_A}. The far apsis is ra,B=aB(1+eB)=4aA(1.75)=7aA.r_{a,B}=a_B(1+e_B)=4a_A(1.75)=7a_A. Thus the long period is compatible with an approach to aAa_A; the body spends much of its orbit at larger radii.

Physical check

The apsis average is (aA+7aA)/2=4aA(a_A+7a_A)/2=4a_A, recovering the inferred semimajor axis.