Let V, T, L, K and r denote the speed, time period, angular momentum, kinetic energy and radius of satellite in circular orbit, then (a) V prop r^(-1)(b) L prop r^(1//2) (c) T prop r^(3//2)(d) K prop r^(-2)

Let V, T, L, K and r denote the speed, time period, angular momentum,

1.	Let V, T, L, K and r denote the speed, time period, angular momentum, kinetic energy and radius of satellite in circular orbit, then (a) V prop r^(-1)(b) L prop r^(1//2) (c) T prop r^(3//2)(d) K prop r^(-2)
Answer» only a & B are TRUE only b & C are true only a, b & d are true only a, b & c are true ANSWER :B