Encyclopedia entry

Von Braun-2

Engine · Germany

Original archive entry. The text, images and links below are kept as they were written.

Notional Nitric acid/UDMH rocket engine. A11, Von Braun studies 1943-1952.

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.