| Project Francis II |
| Type | Super Heavy Lift Launch Vehicle |
| Stage | 4 |
| Displacement | 6,250 t |
| Length | 140 m |
| Diameter | 12.5 m |
| Propellant | Kerosene Liquid Oxygen |
| Payload | 250 t (LEO) |
| First Stage |
| Engine | KE-5A(SL) x 9 |
| Thrust | 90,000 kN |
| Propellant | RP-1 / LOX |
| Specific impulse | 270s |
| Burn Time | 50s |
| Second Stage |
| Engine | KE-5A(V) x 5 |
| Thrust | 50,000 kN |
| Propellant | RP-1 / LOX |
| Specific impulse | 270s |
| Burn Time | 125s |
| Third Stage |
| Engine | HE-3(V) x 5 |
| Thrust | 12,500 kN |
| Propellant | LH2 / LOX |
| Specific impulse | 460s |
| Burn Time | 360s |
| Forth Stage |
| Engine | NERVA-1(V) x 1 |
| Thrust | 540 kN |
| Propellant | LH2 / Nuke |
| Specific impulse | 800s |
| Burn Time | 1250s |
