TJ80 TURBOJET ENGINE - 2 Pages

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Catalogue excerpts

Small turbojet engine designed for missiles, target drones and UAVs

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Technical parameters Max. thrust (5 min.) Thrust (continuous) Specific fuel consumption (SFC) RPM Airflow Compression ratio Operation conditions: Altitude Ambient temperature Speed Additional data: Electric generator power Engine atarting Standard accessories (airframe installation) Fuel Lubrication Mode 100% 97% 100% 100% 100% Ink] Starting envelope 0 e 6,000 m -40°C e +50°C < 0.6 M 28 V - 1,000 W BLDC starter Engine control unit (ECU), Exciter ignition, Electromagnetic stop valve JET-A1, TS-1, RT 3% oil in fuel (MIL-L-23 699) Dimension and weight: Max. outer diameter    235 mm Length (including...

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