First Stage – S-IC
Length Diameter Empty mass
Gross mass
Engines
Thrust Specific Impulse Burn Time Fuel 138.0 feet (42.1 m) 33.0 feet (10.1 m)
287,000 pounds (130,000 kg)
5,040,000 pounds (2,290,000 kg) 5 Rocketdyne F-1 7,648,000 lbf (34,020 kN) 263 seconds (2.58 km/s) 165 seconds RP-1/LOX