Von Braun-1
Engine · Germany
Original archive entry. The text, images and links below are kept as they were written.
Notional Nitric acid/UDMH rocket engine. Study 1952. Used on Von Braun launch vehicle.
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. .
Related
- Family
- Storable liquid
- Country
- Germany
- Launch Vehicles
- Von Braun 1952
- Propellants
- Nitric acid/UDMH
- Stages
- Von Braun 1952-1