Apollo Saturn V J-2 Rocket Engine Turbopump First Stage Turbine Wheel, measuring 12″ in diameter and 1.5″ thick, marked at center with part numbers: "460152, S/N 2749458, HT-KH-344-K2, FR//-SF-1088, C2602, HC 3361." The turbopump on the J-2 Rocket Engine was responsible for generating the necessary pressure to flow propellant through the injector and combustion chamber at the required flow rate.
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.
