| Parameter Name | Value |
| Payload Weight (kg) | 550 |
| Cruising Mach Number | 0.8 |
| Cruising Altitude (m) | 12000 |
| Engine Weight (kg) | 250 |
| Estimated Maximum Takeoff Weight (kg) | 3293.7 |
| Number of Engines | 1 |
| Wing Taper Ratio | 0.4 |
| Quarter Chord Sweep Angle (degrees) | 35 |
| Fuselage Surface Area (m2) | 20.42 |
| Fuselage Width (m) | 1.14 |
| AR | 5 |
| Tail Surface Area (m2) | 2.9 |
| Fuel Coefficient | 0.43 |
| Fuselage Length (m) | 9.16 |
| Wing Surface Area (?) | 14.57 |