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Model: Titan 5. Gross Mass: 500,000 kg (1,100,000 lb). Empty Mass: 45,000 kg (99,000 lb). Thrust (vac): 4,457.100 kN (1,001,996 lbf). Isp: 425 sec. Burn time: 420 sec. Propellants: Lox/LH2. Isp(sl): 354 sec. Diameter: 6.00 m (19.60 ft). Span: 6.00 m (19.60 ft). Length: 60.00 m (196.00 ft). Country: USA. No Engines: 1. Motor: PW 1000000 lb LH2. Status: Study 1988. Part of launch vehicle proposed by Martin as alternative to NLS. All figures estimated based on 1,000,000 lb thrust single engine. 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. |