F-1 Rocket Engine

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    F-1 Rocket Engine

    The F-1 engine, with 1.5 million pounds of thrust, was the powerplant for the first stage of the 363-foot long Saturn V launch vehicle that took the first astronauts to the Moon for six successful landing missions.

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    IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu

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    F-1 Rocket Engine

    Bell-shaped nozzle with fuel manifold pipe wrapped around center and starting with smaller diameter and gradually expanding to larger diameter then joining to vertically mounted cylinders to pump and other plumbing arrangement on top of nozzle. Nozzle with longitudinally placed cooling tubes around entire periphery of nozzle. Tubes reinforced by ridged and equi-distant hoops around nozzle.

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    Usage Conditions Apply

    There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page.

    IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu

    View Manifest

    View in Mirador Viewer

    F-1 Rocket Engine

    Bell-shaped nozzle with fuel manifold pipe wrapped around center and starting with smaller diameter and gradually expanding to larger diameter then joining to vertically mounted cylinders to pump and other plumbing arrangement on top of nozzle. Nozzle with longitudinally placed cooling tubes around entire periphery of nozzle. Tubes reinforced by ridged and equi-distant hoops around nozzle.

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    Usage Conditions Apply

    There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page.

    IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu

    View Manifest

    View in Mirador Viewer

    F-1 Rocket Engine

    Bell-shaped nozzle with fuel manifold pipe wrapped around center and starting with smaller diameter and gradually expanding to larger diameter then joining to vertically mounted cylinders to pump and other plumbing arrangement on top of nozzle. Nozzle with longitudinally placed cooling tubes around entire periphery of nozzle. Tubes reinforced by ridged and equi-distant hoops around nozzle.

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    Usage Conditions Apply

    There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page.

    IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu

    View Manifest

    View in Mirador Viewer

    F-1 Rocket Engine

    Bell-shaped nozzle with fuel manifold pipe wrapped around center and starting with smaller diameter and gradually expanding to larger diameter then joining to vertically mounted cylinders to pump and other plumbing arrangement on top of nozzle. Nozzle with longitudinally placed cooling tubes around entire periphery of nozzle. Tubes reinforced by ridged and equi-distant hoops around nozzle.

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    Usage Conditions Apply

    There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page.

    IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu

    View Manifest

    View in Mirador Viewer

    F-1 Rocket Engine

    Bell-shaped nozzle with fuel manifold pipe wrapped around center and starting with smaller diameter and gradually expanding to larger diameter then joining to vertically mounted cylinders to pump and other plumbing arrangement on top of nozzle. Nozzle with longitudinally placed cooling tubes around entire periphery of nozzle. Tubes reinforced by ridged and equi-distant hoops around nozzle.

    6 of 13

    Usage Conditions Apply

    There are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page.

    IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections. More - https://iiif.si.edu

    View Manifest

    View in Mirador Viewer

    F-1 Rocket Engine

    The F-1 engine, with 1.5 million pounds of thrust, was the powerplant for the first stage of the 363-foot long Saturn V launch vehicle that took the first astronauts to the Moon for six successful landing missions.

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    F-1 Engine

    An F-1 engine on display in the Apollo to the Moon gallery at the National Mall building.
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    F-1 Rocket Engine

    The F-1 engine, with 1.5 million pounds of thrust, was the powerplant for the first stage of the 363-foot long Saturn V launch vehicle that took the first astronauts to the Moon for six successful landing missions.

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    F-1 Liquid Fuel Rocket Engine

    The F-1 engine, with 1.5 million pounds of thrust, was the powerplant for the first stage of the 363-foot long Saturn V launch vehicle that took the first astronauts to the Moon for six successful landing missions between 1969 and 1972 in the Project Apollo program.  The first stage of the Saturn V had five F-1's for a total lift-off thrust of 7.5 million pounds.

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    F-1 Rocket Engine

    F-1 Rocket Engine

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    F-1 rocket engines in Apollo to the Moon

    Five huge F-1 rocket engines were needed to lift the 30-story-tall Saturn V Moon rocket off the launchpad. Through the use of mirrors, one full engine and a one quarter cutaway produce a view of the five-engine cluster at the base of the Saturn V first stage. The F-1 rocket engines are on display at the National Air and Space Museum in the Apollo to the Moon exhibit.

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    The F-1 Engine and the Conquest of Space

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The F-1 engine, with 1.5 million pounds of thrust, was the powerplant for the first stage of the 363-foot long Saturn V launch vehicle that took the first astronauts to the Moon for six successful landing missions between 1969 and 1972 in the Project Apollo program. The first stage of the Saturn V had five F-1's for a total lift-off thrust of 7.5 million pounds. The fully-fueled Saturn V weighed 6.1 million pounds.

The F-1 used RP-1, a type of kerosene, and liquid oxygen as the propellants. The F-1's 2,500-pound turbopump pumped in the propellants at 42,500 gallons per minute. This engine was constructed in 1963 by the Rocketdyne Division of Rockwell International and underwent four start tests, totaling 192.6 seconds. The engine was donated to the Smithsonian in 1970 by the NASA Marshall Space Flight Center.