190 kgf Turbojet Engine | |
Max. thrust (kgf) | 190 |
Max. altitude (m) | 12000 |
Max. speed (Ma) | 0.9 |
Outside diameter(mm) | Φ320×650 |
Thrust to weight ratio | 7.6 |
Fuel consumption (kg/kgf·h) | 1.32 |
Electrical power output (W) | 1500 |
Lifetime (h) weight |
30 25kg |