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Saturn IVB-A

Stage · USA

Original archive entry. The text, images and links below are kept as they were written.

LOx/LH2 propellant rocket stage. Douglas Studies, 1965: S-IVB with 215k lbf J-1 (actual final model had 230k J-1).

Country
USA
Engines
J-2
Launch Vehicles
Saturn IB-A
Propellants
Lox/LH2