Saturn MS-II-3B
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
LOx/LH2 propellant rocket stage. S-II with 15.5 foot stretch, 1.29 million pounds propellant, 7 x 400,000 lb thrust toroidal engines.
No Engines: 5.
Related
- Country
- USA
- Engines
- Toroidal 400k
- Launch Vehicles
- Saturn V-3B
- Propellants
- Lox/LH2