This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Rolls Royce. Used on stages: Europa-1. Used on launch vehicles: Europa. Propellants: Lox/Kerosene Thrust(vac): 85,282 kgf. Thrust(vac): 836.30 kN. Isp: 282 sec. Isp (sea level): 248 sec. Burn time: 156 sec. Mass Engine: 750 kg. Diameter: 1.5 m. Chambers: 1. Chamber Pressure: 39.46 bar. Area Ratio: 8.00. Thrust to Weight Ratio: 113.71. Country: UK. Status: Out of Production. First Flight: 1964. Last Flight: 1971. Flown: 22.
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 .