SLS Stage C
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
LOx/LH2 propellant rocket stage. Launch vehicle core stage for Project Lunex. Masses estimated based on optimum apportioning of B+C stage total masses. Thrust, engines estimated based on requirements.
No Engines: 2.
Related
- Country
- USA
- Engines
- M-1
- Launch Vehicles
- SLS BC-2720
- Propellants
- Lox/LH2