Von Braun-2

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Engine Model: Von Braun-2. Propellants: Nitric acid/UDMH. Thrust(vac): 461.500 kN (103,749 lbf). Thrust(sl): 371.100 kN (83,427 lbf). Isp: 286 sec. Isp (sea level): 230 sec. Burn time: 124 sec. Chambers: 1. Country: Germany. Status: Study 1952. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.