Saturn V (1967-1972)
First Flight: November 9, 1967
Last Flight: December 6, 1972
Stages: 3
Total Mass: 2800 tons
Payload Mass: 120,000 kg to LEO; 45,000 kg to TLI
Diameter: 10.1 m
Length: 110.6 m
First Stage
Type: S-IC Core
Arrangement: 5 x Rocketdyne F-1
Thrust (kN): 34,020
Propellant: RP-1/LOX
ISP:
ISP (sea level): 263 s
Burn Time: 150 s
Gross Mass: 2,300 tons
Empty Mass: 131 tons
Diameter: 10.1 m
Length: 42.1 m
Second Stage
Type: S-II Core
Arrangement: 5 x Rocketdyne J-2
Thrust (kN): 4,400
Propellant: LH2/LOX
ISP: 421 s
ISP (sea level):
Burn Time: 360 s
Gross Mass: 480 tons
Empty Mass: 36 tons
Diameter: 10.1 m
Length: 24.8 m
Third Stage
Type: S-IVB Core
Arrangement: 1 x Rocketdyne J-2
Thrust (kN): 1,000
Propellant: LH2/LOX
ISP: 421 s
ISP (sea level):
Burn Time: 165 s + 335 s (2 burns)
Gross Mass: 120.8 tons
Empty Mass: 10 tons
Diameter: 6.6 m
Length: 18.8 m