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Saturn S-IC-TLB
Part of Saturn V
American orbital launch vehicle. 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

Status: Study 1967. Payload: 39,000 kg (85,000 lb). Thrust: 13,540.00 kN (3,043,910 lbf). Gross mass: 1,118,100 kg (2,464,900 lb). Height: 65.00 m (213.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 185 km (114 mi).

LEO Payload: 39,000 kg (85,000 lb) to a 185 km orbit at 28.00 degrees.

Stage Data - Saturn S-IC-TLB



Family: orbital launch vehicle. People: von Braun. Country: USA. Stages: Saturn IVB (S-IB), Saturn S-IC-TLB stage.

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