Additional information on the Titan II missile can be found at the Titan II ICBM Web Page.

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).

Missile Airframe Configuration

Click image for a 4248x5912 pixel version of this image in a new window.
Taken from p. 115 (p. 24 in the PDF) of the Titan II Handbook Sample Download [direct link to 12.3 meg PDF]
Scan by Titan II Handbook
Extraction and clean-up by heroicrelics.org.