1. a Deduce that a satellite orbiting a planet of mass M in a circular orbit of radius r has a period of revolution given by T=GM4π2r3 .
(a) Deduce that a satellite orbiting a planet of mass M in a circular orbit of radius r has a period of revolution given by T=GM4π2r3 .
(b) A grazing orbit is one in which the orbit radius is approximately equal to the radius R of the planet. Deduce that the period of revolution in a grazing orbit is given by T=Gρ3π where ρ is the density of the planet.
(c) The period of a grazing orbit around the earth is 85 minutes, and around the planet Jupiter it is 169 minutes. Deduce the ratio ρJupiterρearth .