Titan 3B-2 (original) (raw)

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Titan 3B-2

Part of Titan LR91 stage series

N2O4/Aerozine-50 propellant rocket stage. .

Status: Study 1965. Thrust: 460.31 kN (103,483 lbf). Gross mass: 37,560 kg (82,800 lb). Unfuelled mass: 2,900 kg (6,300 lb). Specific impulse: 316 s. Specific impulse sea level: 145 s. Burn time: 230 s. Height: 8.60 m (28.20 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 3BAS2, Titan 3M, Titan IIIB, Commercial Titan 3. Propellants: N2O4/Aerozine-50.

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