This page no longer updated from 31 October 2001.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

Designer: Bell. Application: Titan 3 upper stage. Propellants: LF2/Hydrazine Thrust(vac): 15,900 kgf. Thrust(vac): 155.90 kN. Status: Developed 1960's. Comments: Engine developed for high-energy replacement of Titan 3 transtage in early 1960's. Not flown due to toxicity of propellants.
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Last update 12 March 2001.
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© Mark Wade, 2001 .