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Von Braun-1
Notional Nitric acid/UDMH rocket engine. Study 1952. Used on Von Braun launch vehicle.

Status: Study 1952. Thrust: 3,057.30 kN (687,308 lbf). Specific impulse: 286 s. Specific impulse sea level: 230 s. Burn time: 84 s.

Thrust (sl): 2,458.700 kN (552,738 lbf). Thrust (sl): 250,719 kgf. Propellant Formulation: WFNA/UDMH.

Subtopics
Von Braun 1948-1 Nitric acid/Hydrazine propellant rocket stage. .
Von Braun 1952-1 Nitric acid/Hydrazine propellant rocket stage. .
Family: Storable liquid. Country: Germany. Launch Vehicles: Von Braun 1952. Propellants: Nitric acid/UDMH. Stages: Von Braun 1952-1.
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