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MLLV Core
Part of MLLV Family
LOx/LH2 propellant rocket stage. Boeing study, 1969.

AKA: MLLV. Status: Study 1969. Thrust: 71,171.70 kN (16,000,035 lbf). Gross mass: 5,352,400 kg (11,800,000 lb). Unfuelled mass: 317,400 kg (699,700 lb). Specific impulse: 455 s. Specific impulse sea level: 367 s. Burn time: 310 s. Height: 78.63 m (257.97 ft). Diameter: 21.86 m (71.71 ft). Span: 21.86 m (71.71 ft).

No Engines: 12.



Country: USA. Engines: CD Module. Launch Vehicles: MLLV. Propellants: Lox/LH2.

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