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Albatros Carrier Aircraft
LOx/LH2 propellant rocket stage. Configuration: delta wing with wingtip vertical stabilizers and canards. Engine type and performance, empty weight estimated.

Status: Study 1974. Thrust: 7,840.00 kN (1,762,500 lbf). Gross mass: 1,250,000 kg (2,750,000 lb). Unfuelled mass: 210,000 kg (460,000 lb). Specific impulse: 455 s. Specific impulse sea level: 337 s. Burn time: 580 s. Height: 91.00 m (298.00 ft). Diameter: 7.00 m (22.90 ft). Span: 40.00 m (131.00 ft).

No Engines: 4.



Country: Russia. Engines: RD-0120. Spacecraft: Albatros. Propellants: Lox/LH2.

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