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- Q11242284 subject Q8672107.
- Q11242284 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. It burned for nearly 2.5 minutes before separating at an altitude of 42 miles (68 km).".
- Q11242284 thumbnail Saturn_IB_1st_stage.jpg?width=300.
- Q11242284 wikiPageWikiLink Q1093806.
- Q11242284 wikiPageWikiLink Q1146104.
- Q11242284 wikiPageWikiLink Q1161829.
- Q11242284 wikiPageWikiLink Q1473449.
- Q11242284 wikiPageWikiLink Q181114.
- Q11242284 wikiPageWikiLink Q335225.
- Q11242284 wikiPageWikiLink Q400515.
- Q11242284 wikiPageWikiLink Q520336.
- Q11242284 wikiPageWikiLink Q618153.
- Q11242284 wikiPageWikiLink Q719315.
- Q11242284 wikiPageWikiLink Q8672107.
- Q11242284 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.".
- Q11242284 label "S-IB".
- Q11242284 depiction Saturn_IB_1st_stage.jpg.