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- S-IB abstract "The S-IB stage was the first stage of the Saturn IB launch vehicle, which was used for Earth orbital missions. It was composed of nine propellant containers, eight fins, a thrust structure assembly, eight H-1 rocket engines, and many other components. The propellant containers consisted of eight Redstone tanks (four holding LOX and four holding RP-1) clustered around a Jupiter rocket tank containing LOX. The four outboard engines gimballed to steer the rocket in flight, which required a few more engine components. Specifications:Height: 83.6 ft (25.5 m)Diameter: 21.7 ft (6.6 m)Number of fins: 8Finspan: 18 ft (5.5 m)Engines: 8 H-1Thrust: 1,600,000 lbf (7.1 MN)Fuel: RP-1 (Refined kerosene) 41,000 US gal (155 m³)Oxidizer: Liquid oxygen (LOX) 66,000 US gal (250 m³)Burn time: 2.5 minBurnout altitude: 42 miles (68 km)".
- S-IB thumbnail Saturn_IB_1st_stage.jpg?width=300.
- S-IB wikiPageID "1202484".
- S-IB wikiPageRevisionID "582831963".
- S-IB hasPhotoCollection S-IB.
- S-IB subject Category:Rocket_stages.
- S-IB type Abstraction100002137.
- S-IB type FundamentalQuantity113575869.
- S-IB type Measure100033615.
- S-IB type Phase115290337.
- S-IB type RocketStages.
- S-IB type TimePeriod115113229.
- S-IB comment "The S-IB stage was the first stage of the Saturn IB launch vehicle, which was used for Earth orbital missions. It was composed of nine propellant containers, eight fins, a thrust structure assembly, eight H-1 rocket engines, and many other components. The propellant containers consisted of eight Redstone tanks (four holding LOX and four holding RP-1) clustered around a Jupiter rocket tank containing LOX.".
- S-IB label "S-IB".
- S-IB label "S-IB".
- S-IB sameAs S-IB.
- S-IB sameAs m.04gxrh.
- S-IB sameAs Q11242284.
- S-IB sameAs Q11242284.
- S-IB sameAs S-IB.
- S-IB wasDerivedFrom S-IB?oldid=582831963.
- S-IB depiction Saturn_IB_1st_stage.jpg.
- S-IB isPrimaryTopicOf S-IB.
