Saturn IVB C-5A
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
LOx/LH2 propellant rocket stage. Final common third stage design for Saturn C-4 and C-5 (November 1961). Developed into Saturn V second stage. After development started, decision taken to boost performance by increasing diameter to 6.61 m and increasing propellant load.
Related
- Country
- USA
- Engines
- J-2
- Launch Vehicles
- Saturn C-5, Saturn C-4B
- Propellants
- Lox/LH2