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Titan 2-1
Part of Titan LR87 stage series
N2O4/Aerozine-50 propellant rocket stage. .
Status: Study 1961. Thrust: 2,172.23 kN (488,337 lbf). Gross mass: 117,866 kg (259,850 lb). Unfuelled mass: 6,736 kg (14,850 lb). Specific impulse: 296 s. Specific impulse sea level: 258 s. Burn time: 139 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:
LR87-7.
Launch Vehicles:
Titan II,
Soltan,
Titan C,
Titan II GLV,
Titan 2B,
Titan II SLV.
Propellants:
N2O4/Aerozine-50.
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