This page no longer updated from 31 October 2001.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

astronautix.com Otrag


Designer: Otrag. Used on stages: Otrag. Used on launch vehicles: Otrag. Propellants: Nitric acid/Kerosene Thrust(vac): 5,985 kgf. Thrust(vac): 58.70 kN. Isp: 250 sec. Isp (sea level): 240 sec. Burn time: 126 sec. Diameter: 1.2 m. Chambers: 1. Country: Germany. Status: Out of Production. Comments: Pressure-fed, using cheapest possible propellants, windshield wiper motors to operate fuel regulation valves.
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Last update 12 March 2001.
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© Mark Wade, 2001 .