= 2) Impact: The Apollo command-service module (A) attempts to dock with the Soyuz capsule (B), July 15, 1975. Their masses are ma 18Mg and mB = 6.6Mg. The Soyuz is stationary relative to the reference frame shown, and the command-service module approaches with velocity VA 0.2+0.03-0.02k (m/s). = a. If the first attempt at docking is successful, what is the velocity of the center of mass of the combined vehicles afterward. b. If the first attempt is unsuccessful and the coefficient of restitution of the resulting impact is e=0.95, what are the velocities of the two spacecraft after the impact. B A