Titan I Missile Configuration
Additional information on the Titan I missile and its missile bases can be found at the Titan I Epitaph.
The Titan I evolved into the improved Titan II. 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).
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Taken from p. 1-2 (p. 3 in Section
5 [direct link to 16.7 meg PDF]; of the T.O.
21M-HGM25A-1.1, Technical Manual - Operational and Organization Maintenance
USAF Model HGM-25A Missile Weapon System Operation)
Scan by Titan I Epitaph
Extraction and clean-up by heroicrelics.org.
Missile Configuration
- Re-entry vehicle
- Guidance antenna
- External conduit (typical)
- Access panel (typical)
- Staging rocket (2 places)
- Vernier nozzle (4 places)
- Tail skirt and tail fairing assemblies (Stage I engine compartment)
- Thrust chambers
- Air scoop (2 places)
- Main longeron (4 places)
- Fuel tank
- Stage I between tanks structure (Stage I between tanks compartment)
- Liquid oxygen tank
- Stage I support structure (Stage I transition compartment)
- Stage II aft skirt assembly (Stage II engine compartment)
- Stage II between tanks structure (Stage II between tanks compartment)
- Forward support structure (Stage II transition compartment)