Then, from the third law, Newton was able to prove that the forces acting on the planets are inversely proportional to the squares of their distances and directly proportional to their masses. This fact is easy to demonstrate for circular orbits. We begin with the equation for the force on a body in circular motion:
f = mV2 / r
and substituting V = 2 r / t (circumference /time)
f = 4 2 m r / t2
Then, using the subscripts 1 and 2 for planets 1 and 2,
f1 / f2 = m1 r1 t22 / m2 r2 t12
But from Kepler's third law,
t22 / t12 = r23 / r13
Substituting this relationship into the previous expression:
f1 / f2 = m1 r22 / m2 r12
describing the propertirs of the gravitational force.
For the case of elliptical orbits, a, the semi-major axis of the orbit, is substituted for r, but the derivation of this relationship is much less simple.
In the figure above we see the inner 4 planets in our solar system and our moon. The physical parameters of these planets are given in the table below.
Planet | Mass | Orbit Radius | Period | Eccentricity |
---|---|---|---|---|
(kg) | (km) | (days) | ||
Mercury | 3.31 × 1023 | 5.79 × 107 | 87.97 | 0.206 |
Venus | 4.87 × 1024 | 1.08 × 108 | 224.70 | 0.007 |
Earth | 5.98 × 1024 | 1.50 × 108 | 365.26 | 0.017 |
Mars | 6.43 × 1023 | 2.28 × 108 | 686.98 | 0.093 |