Von Braun-2 (original) (raw)
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Von Braun-2
Notional Nitric acid/UDMH rocket engine. A11, Von Braun studies 1943-1952.
Status: Study 1952. Thrust: 461.50 kN (103,749 lbf). Specific impulse: 286 s. Specific impulse sea level: 230 s. Burn time: 124 s.
Thrust (sl): 371.100 kN (83,427 lbf). Thrust (sl): 37,844 kgf. Propellant Formulation: WFNA/UDMH.
Subtopics
| Von Braun-3 Notional Nitric acid/UDMH rocket engine. Study 1952. Used on Von Braun launch vehicle. |
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Family: Storable liquid. Country: Germany. Launch Vehicles: A9/A10/A11, Von Braun 1952. Propellants: Nitric acid/UDMH. Stages: Von Braun 1952-2.
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