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A-12
LOx/Alcohol propellant rocket stage. All values estimated.

Status: Study 1944. Thrust: 98,000.00 kN (22,031,000 lbf). Gross mass: 3,500,000 kg (7,700,000 lb). Unfuelled mass: 350,000 kg (770,000 lb). Specific impulse: 247 s. Specific impulse sea level: 210 s. Height: 33.00 m (108.00 ft). Diameter: 11.00 m (36.00 ft). Span: 23.00 m (75.00 ft).

No Engines: 50.



Country: Germany. Engines: A-10 engine. Launch Vehicles: A9/A10/A11/A12. Propellants: Lox/Alcohol.

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