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Powerplant: 1 × Rotax 912ULS 4 cylinder horizontally-opposed piston engine, 75 kW (100 hp) Main rotor diameter: 8.4 m (27 ft 7 in) Main rotor area: 55.4 m 2 (596 sq ft) teetering head rotor; Propellers: 3-bladed composite fixed pitch; Performance. Maximum speed: 160 km/h (99 mph, 86 kn) Cruise speed: 160 km/h (99 mph, 86 kn)
This category is for aircraft designed, manufactured or marketed by Apollo Ultralight Aircraft. Pages in category "Apollo Ultralight Aircraft aircraft" The following 6 pages are in this category, out of 6 total.
Apollo Ultralight Aircraft is a Hungarian aircraft manufacturer based in Eger.The company specializes in the design and manufacture of ultralight aircraft, gyroplanes and ultralight trikes, in the form of kits for amateur construction and ready-to-fly aircraft for the European Fédération Aéronautique Internationale microlight and the American light-sport aircraft categories.
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AG1 and AG-1 may refer to: Apollo Gyro AG1, a Hungarian autogyro; Christopher AG-1, a proposed Second World War American assault glider; Hispasat AG1, a Spanish ...
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