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KP12 Turbojet Engine

Source: Date:2024/12/01
KP12 Turbojet Engine

The KP12 turbojet engine has a maximum thrust of 120 kg, fuel consumption of 1.2 kg/(kg·h), and overall dimensions of Φ245 mm. It provides an electrical power output of no less than 2 kW, is compatible with various starting modes such as electric start and air start, and can equip light aircraft like trainers, sport aircraft, or private planes; multi-role UAVs for reconnaissance, early warning, counter-terrorism, and communication relay; as well as high-end model aircraft, flight packs/motors, etc.

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