NASA Saturn IB Apollo AS-203
Saturn IB
Status
Success
Date
5 JUL 1966
14:53
Launch Provider
National Aeronautics and Space Administration
Launch Pad
Space Launch Complex 37B
Cape Canaveral SFS, FL, USA
Mission Overview
The purpose of Apollo 203 was to check out the behaviour of the fuel inside the Saturn-4B stage in weightlessness, which was crucial to allow the reignition of the stage.
Rocket
Saturn IB
Mission Type
Test Flight
Orbit
Low Earth Orbit
Stages
2
Livestream
Not availableRocket Details
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.
Height
43.2 m
Diameter
6.61 m
Launch Mass
590 T
Thrust
7,100 kN