Performance data can be downloaded here: Simulation Results of MTOW Mission (PL 17 to, 2500 NM): CSR 01 MissionDesign R4630 PL17000 Out
| Parameter | Comment | Unit | Value |
|---|---|---|---|
| Mission specifications | |||
| Range | NM | 2500 | |
| Payload (PL) | kg | 17000 | |
| Cruise Mach number | - | 0.78 | |
| Cruise climb steps | ft | 2000 | |
| Climb Mach number | above crossover altitude | - | 0.76 |
| CAS above FL100 | KCAS | 300 | |
| CAS below FL100 | KCAS | 250 | |
| Taxi-out time | min | 9 | |
| Taxi-in time | min | 5 | |
| Alternate distance | NM | 200 | |
| Fuel reserves method | JAR-OPS 1.255 | ||
| Mission simulation results | |||
| Take-off weight | TOW = OWE + PL + MF - TXFout | kg | 76999 |
| Mission (loaded) fuel | MF = BF + RF | kg | 18183 |
| Block fuel | BF = TF + TXFout + TXFin | kg | 14789 |
| Trip fuel | TF | kg | 14360 |
| Reserve fuel | RF | kg | 3394 |
| Taxi-out fuel | TXFout | kg | 276 |
| Taxi-in fuel | TXFin | kg | 153 |
| Landing weight | LW = MTOW - TF | kg | 62639 |
| Block time | h | 6.01 | |
| Flight time | h | 5.78 | |
Note: the small CL peak at the very beginning of the cruise phase is due to the acceleration phase from climb Mach number (Ma 0.76) to initial cruise Mach number (Ma 0.78).