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Saturn S-IC-TLB stage

Stage · USA

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

LOx/Kerosene propellant rocket stage. Boeing Low-Cost Saturn Derivative Study, 1967 (trade study of 260 inch first stages for S-IVB, all delivering 86,000 lb payload to LEO): S-IC Technology Liquid Booster: 260 inch liquid booster with 2 x F-1 engines, recoverable/reusable.

No Engines: 2.

Country
USA
Engines
F-1
Launch Vehicles
Saturn S-IC-TLB
Propellants
Lox/Kerosene