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Titan 3A-1
Part of Titan LR87 stage series
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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