DimensionsPerformance with 0.9 kg payload span 3.00 m max level speed 145 km/h 79 kt area 0.70 sq m cruise speed 80 km/h 44 kt overall length 1.60 m max vertical climb @ max weight, SL 1.0 m/s 200 ft/min rotor diameter 1.85 m max climb @ max weight, SL 3.8 m/s 750 ft/min fuselage diameter 0.18 m endurance, no reserves more than 40 hr max VTO weight 19.2 kg still-air range @ max endurance more than 3000 km/2000 nm
Подскажите какой двигатель подходит и какой пропеллер ?
Подскажите какой двигатель
The main rotor is powered by a single-cylinder 28 cc two-stroke through a reduction gearbox. It is placed forward of the wing in a tractor layout, but aft of a non-rotating nose reserved for an imaging turret or other payload.
гуглоперевод “Основной ротор оснащен одноцилиндровым 28 см двухтактных через редуктор. Он расположен спереди от крыла в компоновке трактора, но в кормовой части невращающегося носа защищены для башни изображений или других полезных данных.” spacedaily.com/…/Aerovel_Strolls_Out_Flexrotor_Lon…
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