Outlay of Trajectories for the Army's Juno I and Juno II Program

This paper presents a description of the factors associated with establishing trajectories for the Juno I and Juno II program. It gives a description of the following orbital elements: inclination, eccentricity, semi-major axis, right ascension of the ascending node, argument of perigee, and time of perigee passage. Also included is a detailed description of the trajectory arrangement for the Lunar Probe, and a list of the elliptical characteristics for the Explorer VII trajectory.