M106 aircraft, UL260i engine hyperflite
M106 aircraft, UL260i engine
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M106 aircraft, UL260i engine
Power
UL260i





Torque Curve




The power and torque curve of the engine has been established by repeated dyno tests on our second prototype, which were performed at sea level and in weather conditions close to the ISA standard. The following graph shows the real, available power and torque coming from the crankshaft of the UL260i





The following graph shows the calculated available power of the UL260i engine at different RPM settings, WOT (wide open throttle) and varying density altitude.
engine corrected to the International Standard Atmosphere conditions at sea level.


Power/Torque Cruve
For more information on ISA, density altitude, interpretation of this graph, the conversion of the figures to actual atmospheric conditions, refer to the "Engine Resources" section on our website and more specifically: "ISA conditions & conversion".
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