RPM, Power Draw, and Airspeed for maintaining level altitude flight in the ANT-E 

Airspeed was measured by observing a Hall wind meter which has no capability to record data. Speed remained constant during the demo period. Other data was recorded in spreadsheet format by the logging capability of the electric drive system. Wing loading was 2.73 lbs/sq ft. (13.35kg/sq M). Ground elevation 680ft. Air temperature 91°F/32.7°C.
The aircraft is an electric powered Aeros Nano Trike and Combat-12T wing. Drive system is Geiger Engineering HPD-16. The prop is a Helix 1.4m with 16° pitch.
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