This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Liberty 1. Used on launch vehicles: Liberty. Propellants: Lox/Kerosene Thrust(vac): 25,000 kgf. Thrust(vac): 245.20 kN. Isp: 270 sec. Isp (sea level): 230 sec. Burn time: 157 sec. Mass Engine: 270 kg. Diameter: 1.6 m. Chambers: 1. Area Ratio: 5.00. Country: USA. Status: Developed 1982-1988. Comments: Pressure-fed engine.
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 .