| Function | Orbital Launch Vehicle |
|---|---|
| Size | |
| Height | 19.5 m (63.9 ft) |
| Diameter | 1.5 m |
| Stages | 2 or 2.5 (Including Booster) |
| Capacity – Payload | Cubesats/Microsatellite |
| Payload to LEO | 600 kg (1,300 lb) |
| First Stage | LOX + Kerosene |
| Engines | 4 Solid + 1 Bi-Propellant |
| Second Stage | LOX + LNG |
| 2 Bipropellant Engine + 1 Kickstage |