Saturn MS-IC-3B
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. S-IC with 20 foot stretch, 1.8 million lb thrust F-1's, 5.6 million pounds propellant capacity (fuel offloaded to 4.99 million for LEO or 4.80 million lbs for LOR mission).
No Engines: 5.
Related
- Country
- USA
- Engines
- F-1A
- Launch Vehicles
- Saturn V-3B
- Propellants
- Lox/Kerosene