| Titan C-2 |
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Model: Titan C-2. Gross Mass: 57,400 kg (126,500 lb). Empty Mass: 6,000 kg (13,200 lb). Thrust (vac): 666.000 kN (149,722 lbf). Isp: 403 sec. Burn time: 300 sec. Propellants: Lox/LH2. Isp(sl): 350 sec. Diameter: 4.07 m (13.35 ft). Span: 4.07 m (13.35 ft). Length: 19.50 m (63.90 ft). Country: USA. No Engines: 1. Motor: LR87 LH2. Status: Development ended 1961. Engine developed 1958-1960, but launch vehicle cancelled 1961. Used on Launch Vehicles: Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |