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