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Titan 3A-2
Status: Study 1965. Thrust: 453.71 kN (101,999 lbf). Gross mass: 29,188 kg (64,348 lb). Unfuelled mass: 2,653 kg (5,848 lb). Specific impulse: 316 s. Specific impulse sea level: 145 s. Burn time: 205 s. Height: 7.90 m (25.90 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 IIIC, Titan IIIA, Titan 3C7, Titan 23B, Titan 33B, Titan IIID, Titan 24B, Titan 23C, Titan IIIE, Titan 34B, Titan 34D/IUS, Titan 34D, Titan 34D/Transtage. Propellants: N2O4/Aerozine-50.
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