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Von Braun 1952-1
Part of Von Braun-1
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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