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A-9 stage
Part of A-4 Family
LOx/Alcohol propellant rocket stage. Winged version.

AKA: A-9. Status: Study 1944. Thrust: 288.68 kN (64,897 lbf). Gross mass: 16,259 kg (35,844 lb). Unfuelled mass: 3,000 kg (6,600 lb). Specific impulse: 255 s. Specific impulse sea level: 220 s. Burn time: 115 s. Height: 14.18 m (46.52 ft). Diameter: 1.65 m (5.41 ft). Span: 3.20 m (10.40 ft).

Cost $ : 3.000 million.



Country: Germany. Engines: Model 39a. Launch Vehicles: A9/A10, A9/A10/A11/A12, A9/A10/A11. Propellants: Lox/Alcohol.

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