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Albatros Raketoplan
LOx/LH2 propellant rocket stage. Configuration: delta wing with wingtip vertical stabilizers.

Status: Study 1974. Thrust: 1,960.00 kN (440,620 lbf). Gross mass: 320,000 kg (700,000 lb). Unfuelled mass: 82,000 kg (180,000 lb). Specific impulse: 455 s. Specific impulse sea level: 337 s. Burn time: 270 s. Height: 49.00 m (160.00 ft). Diameter: 7.00 m (22.90 ft). Span: 25.00 m (82.00 ft).

No Engines: 4.



Country: Russia. Spacecraft: Albatros. Propellants: Lox/LH2.

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