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Titan 4-2
Part of Titan LR91 stage series Family
N2O4/Aerozine-50 propellant rocket stage. .

Status: Retired 2005. Thrust: 459.51 kN (103,302 lbf). Gross mass: 39,500 kg (87,000 lb). Unfuelled mass: 4,500 kg (9,900 lb). Specific impulse: 316 s. Specific impulse sea level: 160 s. Burn time: 223 s. Height: 9.94 m (32.61 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 4.640 million.



Country: USA. Engines: LR91-11. 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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