J-2 adalah sebuah mesin roket kriogenik bahan bakar cair yang digunakan pada Saturn IB dan kendaraan peluncur Saturn V NASA. Dibangun di Amerika Serikat oleh Rocketdyne, J-2 membakar propelan cair hidrogen & oksigen cair kriogenik, dengan masing-masing mesin memproduksi 1,033.1 kN (232.250 lbf) dorong dalam ruang hampa.

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