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Titan 4-1
Part of Titan LR87 stage series Family
N2O4/Aerozine-50 propellant rocket stage. .

Status: Retired 2005. Thrust: 2,428.31 kN (545,906 lbf). Gross mass: 163,000 kg (359,000 lb). Unfuelled mass: 8,000 kg (17,600 lb). Specific impulse: 302 s. Specific impulse sea level: 250 s. Burn time: 164 s. Height: 26.37 m (86.51 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 13.000 million. No Engines: 2.



Country: USA. Engines: LR87-11. Launch Vehicles: Titan 402A/IUS, Titan 405A, Titan 403A, Titan 404A, Titan 401A/Centaur, Titan 402B/IUS, Titan 401B/Centaur, Titan 404B, Titan 403B. Propellants: N2O4/Aerozine-50.

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