Saturn MS-IC-4(S)B
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 336 inch stretch, 6,000,0000 lbs propellant, structural strength increased from 56% to 65% depending on station, resulting in 13.9% increase in empty weight.
No Engines: 5.
Related
- Country
- USA
- Engines
- F-1
- Launch Vehicles
- Saturn MLV-V-4(S)-A, Saturn V-ELV
- Propellants
- Lox/Kerosene