S-IB

The S-IB stage was the first stage of the Saturn IB launch vehicle, which was used for Earth orbital missions. It was an upgraded version of the S-I stage used on the earlier Saturn I rocket and was composed of nine propellant containers, eight fins, a thrust structure assembly, eight H-1 rocket engines, and many other components. It also contained the ODOP transponder. The propellant containers consisted of eight Redstone-derived tanks clustered around a Jupiter rocket-derived tank containing LOX. The four outboard engines gimballed to steer the rocket in flight, which required a few more engine components. The S-IB burned for nearly 2.5 minutes before separating at an altitude of 42 miles (68 km).

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Wikimedia, Wikidata
Saturn S-IB
diameter 6.55 metre, diameter 6.6 metre, height 24.44 metre, mass 125600 kilogram, mass 286353 kilogram, mass 38342 kilogram, mass 450831 kilogram, maximum thrust 200000 pound-force, 
liquid-propellant rocket, Stellantis North America, United States, 
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, Republic of Haiti, 

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Location: KML, Cluster Map, Maps,

Frameless

Nighttime view of Launch Complex 34, Kennedy Space Center, showing the Apollo 7 (Spacecraft 101/Saturn 205) stack on pad.

S68-48666

The Apollo 7/Saturn IB space vehicle is launched from the Kennedy Space Center's Launch Complex 34

Type	Subtype	Date	Description	Notes	Source
commons	image		Nighttime view of Launch Complex 34, Kennedy Space Center, showing the Apollo 7 (Spacecraft 101/Saturn 205) stack on pad.		Commons
commons	image		S68-48666		Commons
commons	image		The Apollo 7/Saturn IB space vehicle is launched from the Kennedy Space Center's Launch Complex 34		Commons