Operating Conditions | Optimum conditions | |||||
Altitude (m) | Mach Number | TIT (K) | Reheat Temperature (K) |
| Thrust (KN) | SFC Kg/N hr |
0 m | 0 | 1450 | 1800 | 16.8504 | 7.10 | 0.1751 |
10,000 m | 0.8 | 1450 | 1800 | 19.6336 | 11.58 | 0.0991 |