Research Article
Research on Simulation and Performance Optimization of Mach 4 Civil Aircraft Propulsion Concept
Table 3
Thrust requirements of the TBCC engine at main operation points.
| | (km) | | Operation mode | Thrust (kN) |
| | Take-off | 0 | 0 | Turbofan | 4 × 240.2 | | Climb | 20.9 | 3 | Turbofan (design point) | 4 × 150.6 | | Climb | 25.0 | 4 | Ramjet (design point) | 4 × 137.2 | | Cruise | 25.0 | 4 | Ramjet | 4 × 114.2 |
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