| Liberty |
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Engine Model: Liberty. Propellants: Lox/Kerosene. Thrust(sl): 18.900 kN (4,249 lbf). Isp (sea level): 245 sec. Burn time: 300 sec. Mass Engine: 23 kg (50 lb). Chambers: 1. Thrust to Weight Ratio: 85.00. Country: USA. Status: Development 1994-2006. Pressure-fed engine. Price $ 12,000 in 1995. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |