NAME
G250 Eagle
ENGINE
TS100 DA
TOP SPEED
190 Km/h
MTOW
650 Kg
The G-250 is our first high-tech two-seater ultralight helicopter equipped with an aero turbine. It was designed and built with a focus on the most innovative materials.
Specification
Main and Tail rotor data
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MR diameter.................................................................. 7,6 m (24,90 ft)
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Nominal MR speed...................................................... 530 RPM
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Tr diameter................................................................... 1,1 m (3,61 ft)
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Nominal TR speed...................................................... 3340 RPM
Powerplant data
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Output shaft speed................................................... 2158 RPM
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Take-off rating............................................................ 151 hp
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Nominal rating........................................................... 124 hp
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Cruising rating........................................................... 107 hp
Fuel & Oil
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Maximum fuel capacity............................................ 130 L (36,9 U.S. gal)
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Approved Fuel........................................................... JET A, JET A-1 and JET B
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Maximum fuel consumption..................................... 54 L/h
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Maximum oil capacity............................................... 3,4 L (0,9 U.S. gal)
The main strengths of the G250 eagle
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Included filter allows flying over desert and volcanic areas
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Possibilitỳ of flying in temperatures from -35° to +45°
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It is capable of hovering above ground effect up to a height of 4000 metres
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Autopilot, black box
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Minimum autonomy of about 490 km (about 3 hours)
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Speed in maintenance work
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Low deployment cost (about $/250 hour flight time) with out depreciation
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Road transportability by road trolley
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