Usage Conditions May Apply 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 Usage Conditions May Apply 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 Usage Conditions May Apply 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

The F-1 engine was the powerhouse of the first stage of the Saturn V rocket that launched the Apollo lunar missions. The thrust chamber was located near the top of the engine. It contained the combustion chamber, where the liquid oxygen (LOX) and rocket-grade kerosene (RP-1) propellants were burned, and a nozzle to then expel the produced gases, thereby generating the required thrust.

This thrust chamber was part of an F-1 engine that launched the Apollo 11 Saturn V. Around 2.5 minutes after launch, the first stage was jettisoned and fell into the Atlantic Ocean. In 2013, F-1 components were recovered from the ocean floor by Bezos Expeditions.

The National Aeronautics and Space Administration transferred the engine parts to the National Air and Space Museum in 2016.

 Display Status

This object is on display in Destination Moon at the National Air and Space Museum in Washington, DC.

Destination Moon
Object Details
Date 1969 Country of Origin United States of America Type PROPULSION-Components (Engine Parts) Manufacturer Rocketdyne Div., North American Rockwell
 Dimensions 3-D: 142.2 × 223.5 × 147.3cm (4 ft. 8 in. × 7 ft. 4 in. × 4 ft. 10 in.)
3-D (With stand): 1197.5kg (2640lb.)
Overall (Object Height on Display Stand): 160cm (5 ft. 3 in.)
 Materials Iron alloy, nickel, electrical wiring, plastic
 Inventory Number A20160016000 Credit Line Transferred from the National Aeronautics and Space Administration Data Source National Air and Space Museum Restrictions & Rights Usage conditions apply
For more information, visit the Smithsonians Terms of Use.