Power output adjustable from 120N to 240N. Small and light!.

X240 Turbojet

Groundbreaking in every detail A Next Generation Retracts for the current generation of large aircraft.

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NG RETRACTS

Specifications: Nominal thrust: 250N a 110.000 RPM. Idle thrust: 7N Idle RPM: 28.000 RPM Diameter: 122mm (4.8″) Engine weight: 2.080gr (4.2lb) Installed weight: 2.199gr (4.57lb) Fuel: Kerosene/Diesel 3%-5% Oil. Fuel consumption: 700g/min Start mode: Direct Kerosene

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X240 Turbojet

NG RETRACTS

M250XBL