Saturn I (1961-1965)
First Flight: October 27, 1961
Last Flight: July 30, 1965
Stages: 2 or 3 (third stage never flown)
Total Mass: 510 tons
Payload Mass: 9,070 kg to LEO; 4,900 kg to LEO (2 stage)
Diameter: 6.52 m
Length: 55 m
First Stage
Type: S-I Core
Arrangement: 8 x H-1
Thrust (kN): 6,700
Propellant: RP-1/LOX
ISP:
ISP (sea level): 289 s
Burn Time: 155 s
Gross Mass: ?
Second Stage
Type: S-IV Core
Arrangement: 6 x RL10
Thrust (kN): 400
Propellant: LH2/LOX
ISP: 373-470 s
ISP (sea level):
Burn Time: 482 s
Gross Mass: ?
Third Stage
Type: S-V (Centaur-C) Core (unflown)
Arrangement: 2x RL10
Thrust (kN): 133
Propellant: LH2/LOX
ISP: 373-470 s
ISP (sea level):
Burn Time: approx. 430 s
Gross Mass: ?