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 (four holding liquid oxygen (LOX) and four holding RP-1) 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 .

Specifications

  • Height:
  • Diameter:
  • Number of fins: 8
  • Finspan:
  • Engines: 8 Rocketdyne H-1
  • Thrust:
  • Fuel: RP-1 (Refined kerosene) 41,000 US gal (155 m<sup>3</sup>)
  • Oxidizer: Liquid oxygen (LOX) 66,277 US gal (251 m<sup>3</sup>) nominal capacity including 1.5% ullage volume (43,284 US gal / 163 m<sup>3</sup> in four outer tanks plus 22,993 US gal / 87 m<sup>3</sup> in center tank)
  • Burn time: 2.5 min
  • Burnout altitude:

Stages built

Apollo flights:

  • S-IB-1: Launched 2/26/1966 on suborbital AS-201 mission.
  • S-IB-3: Launched 7/5/1966 as AS-203 orbital test mission.
  • S-IB-2: Launched 8/25/1966 on suborbital AS-202 test mission.
  • S-IB-4: Launched 1/22/1968 on Apollo 5 orbital mission.
  • S-IB-5: Launched 10/11/1968 on crewed Apollo 7 orbital mission.

Post-Apollo Flights:

  • S-IB-12: Flight not assigned. Presumed scrapped at Marshall Space Flight Center in late 1970s.
  • S-IB-13: Hardware scrapped.
  • S-IB-14: Hardware scrapped.
  • S-IB-15: Not built, cancelled by NASA in 1968.
  • S-IB-16: Not built, cancelled by NASA in 1968.

Proposed variants

Besides the version flown as the Saturn IB stage, other versions were proposed for several vehicle concepts:

Saturn S-IB-2

The S-IB-2 stage was studied in 1960 to power the Saturn C-3. It was planned to be larger (with a height of 34.50&nbsp;m and a diameter of 8.25&nbsp;m), powered by two F-1 engines developing of thrust, with a fueled mass of .

Saturn S-IB-4

The S-IB-4 stage was studied in 1960 to power the Saturn C-4, using four F-1 engines.

Saturn S-IB-A

The S-IB-A stage was studied in 1965 to power the Saturn IB-A and Saturn IB-B, using eight H-1c engines.

Saturn IB-11

The IB-11 stage was studied in 1966 to power the Saturn INT-11, Saturn INT-13 and Saturn INT-14, using eight H-1b engines and UA1207 solid boosters.

Saturn IB-15

The IB-15 stage was studied in 1966 to power the Saturn INT-15, using eight H-1b engines and Minuteman first-stage strap-ons.

Saturn S-1B-4

The S-1B-4 stage was studied in 1966 to power the Saturn INT-12, using four H-1b engines and UA1205 solid boosters.

References