Physics

Physics

Problem

For a planet orbiting a star of mass MM, at an orbital radius of RR, and with an orbital period TT, Kepler's third law states that a. T3R2=GM4π2\frac{T^3}{R^2} = \frac{GM}{4\pi^2} b. T3R2=4π2GM\frac{T^3}{R^2} = \frac{4\pi^2}{GM} c. T2R3=GM4π2\frac{T^2}{R^3} = \frac{GM}{4\pi^2} d. T2R3=4π2GM\frac{T^2}{R^3} = \frac{4\pi^2}{GM}

Browse the problem library