Each second, a single F-1 burned of oxidizer and fuel: of liquid oxygen and of RP-1, generating of thrust. This equated to a flow rate of per second; of LOX and of RP-1. During their two and a half minutes of operation, the five F-1s propelled the Saturn V vehicle to a height of and a speed of . The combined flow rate of the five F-1s in the Saturn V was or per second. Each F-1 engine had more thrust than three Space Shuttle Main Engines combined.