S-IB
 Diagram of the S-IB first stage of the Saturn IB rocket | |
| Manufacturer | Chrysler[1] |
|---|---|
| Country of origin | United States |
| Used on | Saturn IB (stage 1) |
| General characteristics | |
| Height | 25.5 m (84 ft) |
| Diameter | 6.6 m (22 ft) |
| Gross mass | 448,648 kg (989,100 lb) |
| Derived from | S-I |
| Launch history | |
| Status | Retired |
| Total launches | 9 |
| Successes (stage only) | 9 |
| First flight | February 26, 1966 |
| Last flight | July 15, 1975 |
| Powered by | 8 H-1 engines |
| Maximum thrust | 7.1 MN (1,600,000 lbf) |
| Specific impulse | 296 s (2.90 km/s) |
| Burn time | 155 seconds |
| Propellant | RP-1/LOX |
The S-IB stage was the first stage of the Saturn IB launch vehicle, which was used for Earth orbital missions.[2] 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 42 miles (68 km).
Specifications
[edit]- Height: 80.17 ft (24.44 m)
- Diameter: 21.42 ft (6.53 m)
- Number of fins: 8
- Finspan: 39.42 ft (12.02 m)
- Engines: 8 Rocketdyne H-1
- Thrust: 1,600,000 lbf (7,100 kN)
- Fuel: RP-1 (Refined kerosene) 41,000 US gal (155 m3)
- Oxidizer: Liquid oxygen (LOX) 66,277 US gal (251 m3) nominal capacity including 1.5% ullage volume (43,284 US gal / 163 m3 in four outer tanks plus 22,993 US gal / 87 m3 in center tank[3])
- Burn time: 2.5 min
- Burnout altitude: 37 nmi (69 km)
Stages built
[edit]Apollo flights:[1]
- 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 manned Apollo 7 orbital mission.
Post-Apollo Flights:[1]
- S-IB-6: Launched 5/25/1973 on Skylab-2 orbital mission.
- S-IB-7: Launched 7/23/1973 on Skylab-3 orbital mission.
- S-IB-8: Launched 11/16/1973 on Skylab-4 orbital mission.
- S-IB-10: Launched 7/15/1975 on ASTP orbital mission.
Hardware Not Flown:[1]
- S-IB-9: Stacked on MLP ready to fly as Skylab backup. Now on display at Kennedy Space Center Visitor Complex.
- S-IB-11: Flight not assigned. Displayed vertically at Alabama Welcome Center until late 2023, when it was dismantled due to weathering.[4]
- 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.
References
[edit]- ^ a b c d Kyle, Ed (December 6, 2012). "Saturn IB History". Space Launch Report . . . Saturn Vehicle History. Archived from the original on January 4, 2013. Retrieved 2014-09-01.
{{cite web}}: CS1 maint: unfit URL (link) - ^ Wade, Mark (2001). "Saturn IB". Encyclopedia Astronautica. Archived from the original on May 4, 2002.
- ^ "Skylab Saturn IB Flight Manual (MSFC-MAN-206)". Technical Memorandum. NASA Marshall Spaceflight Center. 1972-09-30.
- ^ "Historic Alabama welcome center rocket dismantling begins". Retrieved 2023-09-20.