This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com Sanger-Bredt


Used on stages: Sanger-Bredt. Used on launch vehicles: Sanger. Propellants: Lox/Kerosene Thrust(vac): 145,700 kgf. Thrust(vac): 1,428.80 kN. Isp: 306 sec. Isp (sea level): 210 sec. Burn time: 168 sec. Chambers: 1. Country: Germany. Status: Study 1942. Comments: Used in Sanger-Bredt.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .