S-II, the second stage of the Saturn V moon rocket. Built by North American Aviation in Seal Beach, California. Propellant: LH2 (liquid hydrogen) and LOX (liquid oxygen). Thrust: 1 million lb.

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S-II, the second stage of the Saturn V moon rocket. Built by North American Aviation in Seal Beach, California. Propellant: LH2 (liquid hydrogen) and LOX (liquid oxygen). Thrust: 1 million lb.

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S-IC, the first stage of the Saturn V moon rocket. Propellant: RP-1 (rocket-grade kerosene) and LOX (liquid oxygen). Thrust: 7.5 million lbs. Boeing built these stages at a NASA-owned factory in New Orleans.