Which of the following gives the total mechanical energy per unit mass of a satellite…

PHYSICS · Single correct · A Level · Physics · Fields and their consequences · Fields and their consequences

Problem

Which of the following gives the total mechanical energy per unit mass E/mE/m of a satellite moving in a circular orbit of radius rr around Earth (mass MM, gravitational constant GG)? (a) GM2r\dfrac{GM}{2r} (b) −GMr-\dfrac{GM}{r} (c) −GM2r-\dfrac{GM}{2r} (d) −3GM4r-\dfrac{3GM}{4r}

Related theory

Browse the problem library