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Turbojet Engine

  • 80 kgf Turbojet Engine
  • 80 kgf Turbojet Engine
  • 80 kgf Turbojet Engine
  • 80 kgf Turbojet Engine

Technical Parameters


60 kgf Turbojet Engine 75 kgf Turbojet Engine 80 kgf Turbojet Engine 95 kgf Turbojet Engine 140 kgf Turbojet Engine 190 kgf Turbojet Engine 265 kgf with afterburning
Turbojet Engine
Max. thrust (kgf) 60 75 80 95 140 190 265
Max. altitude (m) 8000 8000 10000 12000 12000 12000 12000
Max. speed (Ma) 0.8 0.8 0.8 0.8 0.8 0.9 1.6
Outside diameter(mm) Φ206×535 Φ202×525 Φ230×535 Φ230×535 Φ270×570 Φ320×650 Φ320×1500
Thrust to weight ratio 6.5 7.5 7.0 7.5 7.5 7.6 7.5
Fuel consumption (kg/kgf·h) 1.55 1.55 1.4 1.4 1.35 1.32 2.6(with afterburning)
Electrical power output (W) —— —— 800 800 1200 1500 1500
Lifetime (h) 20 20 30 30 30 30 30