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NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

Saturn IB

10FLIGHTS
90%SUCCESS
1FAILURES
6STREAK
Feb 1966FIRST FLIGHT
NOREUSABLE
HEIGHT43.2 m
DIAMETER6.61 m
LAUNCH MASS590 kg
LIFTOFF THRUST7,100 kN
STAGES2

The Saturn IB (pronounced “one B”, also known as the Uprated Saturn I) was an American launch vehicle commissioned by the National Aeronautics and Space Administration (NASA) for the Apollo program. It replaced the S-IV second stage of the Saturn I with the much more powerful S-IVB, able to launch a partially fueled Apollo Command/Service Module (CSM) or a fully fueled Lunar Module (LM) into low Earth orbit for early flight tests before the larger Saturn V needed for lunar flight was ready.

21,000 kg
TO LEO
46,305 lbs
7,100
KILONEWTONS
1,596,144
POUNDS-FORCE
~9,521
HORSEPOWER
Height43.2 m (142 ft)
Diameter6.61 m (21.7 ft)
Launch Mass590 kg (1,301 lbs)
Stages2