X-430
Designer: General Electric. Propellants: LF2/LH2. Thrust(vac): 334.000 kN (75,086 lbf). Country: USA. Status: Developed 1960's.

Very high energy engine developed in early 1960's for future large upper stages. Not flown due to toxicity of propellants.  
 
 
 
 
 
 
 
 

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