SuperDraco
| Status | Operational |
|---|---|
| Propellant capacity | 1,388 kg (3,060 lb)[3] |
| Propellant | NTO[2][3] / MMH[2][3] |
| Thrust (SL) | 71,000 newton (16,000 pound-force),[4] individually 32,000 lbf, dual-engine cluster[5] |
| Chamber pressure | 6,900 กิโลปาสกาล (1,000 ปอนด์ต่อตารางนิ้ว)[1] |
| Country of origin | United States |
| Isp (SL) | 235 s (2.30 km/s)[6] |
| Manufacturer | SpaceX |
| Burn time | 25 seconds[6] |
| Application | Launch escape system, powered landing[1] |
