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{{Page|J-2|Classes|cryogenic rocket engine by Rocketdyne}}
{{Page|J-2|Classes|cryogenic rocket engine by Rocketdyne|J2, Rocketdyne J-2, Rocketdyne J2}}

Revision as of 16:07, 17 February 2025




The J-2, commonly known as Rocketdyne J-2, was a liquid-fuel cryogenic rocket engine used on NASA's Saturn IB and Saturn V launch vehicles. Built in the United States by Rocketdyne, the J-2 burned cryogenic liquid hydrogen (LH2) and liquid oxygen (LOX) propellants, with each engine producing 1,033.1 kN (232,250 lbf) of thrust in vacuum. The engine's preliminary design dates back to recommendations of the 1959 Silverstein Committee. Rocketdyne won approval to develop the J-2 in June 1960 and the first flight, AS-201, occurred on 26 February 1966. The J-2 underwent several minor upgrades over its operational history to improve the engine's performance, with two major upgrade programs, the de Laval nozzle-type J-2S and aerospike-type J-2T, which were cancelled after the conclusion of the Apollo program.

WikimediaWikidata
J2, Rocketdyne J-2, Rocketdyne J2
diameter 2.07 metre, height 3.38 metre, maximum thrust 200000 pound-force, maximum thrust 230000 pound-force, maximum thrust 225000 pound-force, specific impulse by weight 419 second, specific impulse by weight 418 second, specific impulse by weight 421 second, mass 1578.5 kilogram, mass 1583.9 kilogram, 
cryogenic rocket engineRocketdyne, 
United StatesAshkenazCalvinist Republic of GhentChinlandDemocratic Republic of the CongoHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaSikh ConfederacySwedenTarshishcryogenic rocket engineDong Fang Hong 2EkranRepublic of Haiti


Location: KML, Cluster Map, Maps,

    J-2 engine production at RocketdyneJ-2 engine production at Rocketdyne
    Atlas 10F at Huntsville Alabama 1987 (cropped)Atlas 10F at Huntsville Alabama 1987 (cropped)
    J-2 Engine (97-153-8)J-2 Engine (97-153-8)
    J-2 rocket engineJ-2 rocket engine
    A J-2 engine undergoes static firing. The J-2, developed under the direction of the Marshall Space Flight Center, was propelled by liquid hydrogen and liquid oxygen.A J-2 engine undergoes static firing. The J-2, developed under the direction of the Marshall Space Flight Center, was propelled by liquid hydrogen and liquid oxygen.
    Workmen inspect a J-2 engine at Rocketdyne`s Canoga Park, California production facility. The J-2, developed under the direction of the Marshall Space Flight Center, was propelled by liquid hydrogen and liquid oxygen.Workmen inspect a J-2 engine at Rocketdyne's Canoga Park, California production facility. The J-2, developed under the direction of the Marshall Space Flight Center, was propelled by liquid hydrogen and liquid oxygen.
    Smokeless flame juts from the diffuser of a unique vacuum chamber in which the upper stage rocket engine, the hydrogen fueled J-2, was tested at a simulated space altitude in excess of 60,000 feet. The smoke you see is actually steam.Smokeless flame juts from the diffuser of a unique vacuum chamber in which the upper stage rocket engine, the hydrogen fueled J-2, was tested at a simulated space altitude in excess of 60,000 feet. The smoke you see is actually steam.
    Rocketdyne`s test stand for testing the J-2 engine in Santa Susana Mountains 6417049Rocketdyne's test stand for testing the J-2 engine in Santa Susana Mountains 6417049
    J-2 engines for the Saturn IB/Saturn V launch vehicles are lined up in the assembly area at Rocketdyne`s manufacturing plant in Canoga Park, California.J-2 engines for the Saturn IB/Saturn V launch vehicles are lined up in the assembly area at Rocketdyne's manufacturing plant in Canoga Park, California.
    This image depicts an overall view of the vertical test stand for testing the J-2 engine at Rocketdyne`s Propulsion Field Laboratory, in the Santa Susana Mountains, near Canoga Park, California.This image depicts an overall view of the vertical test stand for testing the J-2 engine at Rocketdyne's Propulsion Field Laboratory, in the Santa Susana Mountains, near Canoga Park, California.