| Project Peninsula I |
| Type | Medium Lift Launch Vehicle |
| Stage | 2 - without Booster |
| Displacement | IA - 140 t IB - 170 t IC - 200 t ID - 230 t IE - 260 t IF - 290 t |
| Length | 30 m |
| Diameter | 3 m |
| Propellant | Kerosene Liquid Oxygen |
| Payload | IA - 4 t (LEO) / 2 t (GTO) IB - 5.3 t / 2.65 t IC - 6.4 t / 3.2 t ID - 7.4 t / 3.7 t IE - 8.3 t / 4.15 t IF - 9 t / 4.5 t |
| Booster |
| Booster | IA - USRB x 0 IB - USRB x 1 IC - USRB x 2 ID - USRB x 3 IE - USRB x 4 IF - USRB x 5 |
| First Stage |
| Engine | KE-3(SL) x 2 |
| Thrust | 2,000 kN |
| Propellant | RP-1 / LOX |
| Specific impulse | 260s |
| Burn Time | 155s |
| Second Stage |
| Engine | KE-2(V) x 1 |
| Thrust | 500 kN |
| Propellant | RP-1 / LOX |
| Specific impulse | 320s |
| Burn Time | 180s |
| Third Stage |
| Kickmotor | UHKM x 1 |
