Saturn IVB (S-V)

Gross Mass: 119,900 kg (264,300 lb). Empty Mass: 13,300 kg (29,300 lb). Thrust (vac): 1,031.600 kN (231,913 lbf). Isp: 421 sec. Burn time: 475 sec. Propellants: Lox/LH2. Isp(sl): 200 sec. Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft). Length: 17.80 m (58.30 ft). Country: USA. No Engines: 1. Engine: J-2. First Flight: 1967. Last Flight: 1973. No Launched: 13. Used as: 0.

Saturn V version of S-IVB stage

Used on Launch Vehicles:

Saturn INT-20.

Saturn V.

Saturn V-A.

Saturn V-C.

Saturn V-Centaur.

Saturn V-D.

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