Saturn IB
NASA
Details
Height
43.2 m
Diameter
6.61 m
GTO
Unknown
LEO
21,000 kg
Thrust at Liftoff
7,100 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
February 26, 1966
Description
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.