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Each of the five liquid kerosene (RP-1) and liquid oxygen (LOX) fueled F-1 engines were capable of delivering 1.5 million pounds of takeoff thrust, for a combined thrust of 7.5 million pounds during the boost phase. (Jason Perlow)
Dr. Werner von Braun, lead designer of the Saturn V rocket, shown here dwarfed by the S-IC Stage and its F-1 engines. (NASA)
A schematic of the main component parts of the Rocketdyne F-1 Rocket Engine.