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Engine Model: Chariot. Designer: Bell. Application: Titan 3 upper stage. Propellants: LF2/Hydrazine. Thrust(vac): 155.900 kN (35,048 lbf). Country: USA. Status: Developed 1960's. Engine developed for high-energy replacement of Titan 3 transtage in late 1950's / early 1960's. Not flown due to toxicity of propellants. 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. |