ซูเปอร์ดราโค
Status | Operational |
---|---|
Propellant capacity | 1,388 kg (3,060 lb)[3] |
Propellant | NTO[2][3] / MMH[2][3] |
Chamber pressure | 6,900 กิโลปาสกาล (1,000 ปอนด์ต่อตารางนิ้ว)[1] |
Thrust (SL) | 71,000 newton (16,000 pound-force),[4] individually 32,000 lbf, dual-engine cluster[5] |
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] |