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Von Braun 1952-1
Part of Von Braun-1 Family
Nitric acid/Hydrazine propellant rocket stage. .

Status: Study 1952. Thrust: 141,286.30 kN (31,762,424 lbf). Gross mass: 5,500,000 kg (12,100,000 lb). Unfuelled mass: 700,000 kg (1,540,000 lb). Specific impulse: 257 s. Specific impulse sea level: 217 s. Burn time: 84 s. Height: 36.50 m (119.70 ft). Diameter: 20.00 m (65.00 ft). Span: 37.00 m (121.00 ft).

No Engines: 51.

Country: Germany. Engines: Von Braun-1. Launch Vehicles: Von Braun 1952. Propellants: Nitric acid/Hydrazine.



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