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Rombus core
Part of Rombus Family
LOx/LH2 propellant rocket stage. 36 x plug-nozzle engines (20 atm chamber pressure, 7:1 mixture ratio).

AKA: Rombus. Status: Study 1964. Thrust: 101,900.00 kN (22,908,000 lbf). Gross mass: 5,102,041 kg (11,248,075 lb). Unfuelled mass: 306,175 kg (675,000 lb). Specific impulse: 455 s. Specific impulse sea level: 359 s. Burn time: 215 s. Height: 28.96 m (95.01 ft). Diameter: 16.00 m (52.00 ft). Span: 24.39 m (80.01 ft).

Cost $ : 50.000 million.



Country: USA. Engines: Plug-Nozzle Rombus. Launch Vehicles: Rombus. Propellants: Lox/LH2.

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