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Model: MLLV. Gross Mass: 5,352,400 kg (11,800,000 lb). Empty Mass: 317,400 kg (699,700 lb). Thrust (vac): 71,171.700 kN (16,000,035 lbf). Isp: 455 sec. Burn time: 310 sec. Propellants: Lox/LH2. Isp(sl): 367 sec. Diameter: 21.86 m (71.71 ft). Span: 21.86 m (71.71 ft). Length: 78.63 m (257.97 ft). Country: USA. No Engines: 12. Motor: CD Module. Status: Study 1969. Boeing study, 1969. Used on Launch Vehicles:
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