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Titan 3A-1
Part of Titan LR87 stage series Family
N2O4/Aerozine-50 propellant rocket stage. .

Status: Study 1965. Thrust: 2,339.76 kN (525,999 lbf). Gross mass: 116,573 kg (256,999 lb). Unfuelled mass: 5,443 kg (11,999 lb). Specific impulse: 302 s. Specific impulse sea level: 250 s. Burn time: 147 s. Height: 22.28 m (73.09 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 11.600 million. No Engines: 2.



Country: USA. Engines: LR87-11. Launch Vehicles: Titan IIIC, Titan IIIA, Titan 3C7, Titan 23B, 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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