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Titan 4-2
Part of Titan LR91 stage series
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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