Titan II Missile Configuration
Additional information on the Titan II missile can be found at the Titan II ICBM Web Page (warning: makes liberal use of the HTML <blink> tag).
The Titan II was an improved version of the Titan I. Although the Titan I used conventional LOX/RP-1 propellants and the Titan II used the hypergolic Aerozine-50/nitrogen tetroxide combination, the two missiles still shared the same first and second stage engines. Also see my info pages on the Titan I First Stage Engines (LR-87) and the Titan I Second Stage Engine (LR-91).