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Titan 5 stage
Part of NLS Core Family
LOx/LH2 propellant rocket stage. Part of launch vehicle proposed by Martin as alternative to NLS. All figures estimated based on 1,000,000 lb thrust single engine.

AKA: Titan 5. Status: Study 1988. Thrust: 4,457.10 kN (1,001,996 lbf). Gross mass: 500,000 kg (1,100,000 lb). Unfuelled mass: 45,000 kg (99,000 lb). Specific impulse: 425 s. Specific impulse sea level: 354 s. Burn time: 420 s. Height: 60.00 m (196.00 ft). Diameter: 6.00 m (19.60 ft). Span: 6.00 m (19.60 ft).



Country: USA. Engines: PW 1000000 lb LH2. Launch Vehicles: Titan 5. Propellants: Lox/LH2.

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