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Titan C-2
LOx/LH2 propellant rocket stage. Engine developed 1958-1960, but launch vehicle cancelled 1961.

AKA: Titan C. Status: Development ended 1961. Thrust: 666.00 kN (149,722 lbf). Gross mass: 57,400 kg (126,500 lb). Unfuelled mass: 6,000 kg (13,200 lb). Specific impulse: 403 s. Specific impulse sea level: 350 s. Burn time: 300 s. Height: 19.50 m (63.90 ft). Diameter: 4.07 m (13.35 ft). Span: 4.07 m (13.35 ft).



Country: USA. Engines: LR87 LH2. Launch Vehicles: Titan C. Propellants: Lox/LH2.

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