Protective closure assembly for the Rocketdyne F-1 rocket engine's turbopump oxidizer inlet, measuring 18.5″ in diameter, marked with part no. "RX-20633-25H." Includes an unused 6″ Rocketdyne decal and a parts list and diagram showing the location of the closure on the F-1 engine; its purpose was to provide better protection and reduce the possibility of foreign objects entering it during handling and use. The F-1, used to power the S-IC first stage of the Saturn V launch vehicle, remains the most powerful single combustion chamber liquid-propellant rocket engine ever developed. In fine condition.
We use cookies on this site to improve your experience. By using this site, you accept our use of cookies. To learn more, please see our Privacy Policy.