Aerial Vehicle
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Power Plant
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15 HP two-stroke,
air cooled aviation engine
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Tank Volume
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12,5 liters (3,30 gal), expandable
up to 30 liters
(7,90 gal)
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Burn-off
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Typical 5 liters (1,30 gal) per hour
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Rotor System
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Two-blade main rotor with Bell-Hiller stabilizer and
two-blade tail rotor
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Cruise Speed
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90 km/h (56 mph)
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Climb Rate
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600 ft/min (180 m/min)
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Service ceiling
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3000 m MSL
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Maximum edurance
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6 hours
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Length
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2680 mm (105.50 inches)
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Main Rotor Diameter
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3090 mm (121.70 inches)
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Empty Weight
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43 kg (95 lbs)
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Max. Payload
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25 kg (55 lbs)
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MTO Weight
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68 kg (150 lbs)
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Payload Interface
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Two switchable video inputs (PAL or NTSC), one RS232
duplex data interface, power supply (5 to 28 VDC / 3,50 Amp.)
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Ground Interface
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Diagnostic port, ground power-in
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