This page no longer updated from 31 October 2001. Latest version can be found at A-10

Used on stages: A-10. Used on launch vehicles: A-9/A-10, A11. Propellants: Lox/Alcohol Thrust(vac): 235,238 kgf. Thrust(vac): 2,306.80 kN. Isp: 247 sec. Isp (sea level): 210 sec. Burn time: 55 sec. Diameter: 4.1 m. Chambers: 1. Country: Germany. Status: Developed 1940-43. Comments: Planned for use in A-10. Unique dual-thrust chamber / single nozzle design.
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Last update 12 March 2001.
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© Mark Wade, 2001 .