Search results
Results from the WOW.Com Content Network
The Apollo Gyro AG1 is a Hungarian autogyro produced by Apollo Ultralight Aircraft of Eger and introduced in 2012. The aircraft is supplied ready-to-fly. The aircraft is supplied ready-to-fly. [ 1 ]
Apollo Gyro AG1; Apollo Jet Star; Apollo Monsoon; Apollo Racer GT This page was last edited on 5 July 2020, at 21:28 (UTC). Text ...
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.
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 ...
The Jet Star was designed to comply with the Fédération Aéronautique Internationale microlight category as well as the US light-sport aircraft category. It features a cable-braced or strut-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem, open cockpit, tricycle landing gear with wheel pants and a single engine in pusher configuration.
A number of different Apollo wings can be fitted to the basic carriage, including the C-15, C-15TN, C-17 and CXMD. Te Racer GT is the only aircraft built by Apollo that is approved to be fitted with floats. Optional equipment includes instructor training pedals, a hang glider towing system, ballistic parachute, windshield and main wheel brakes .
The Cavalon is a two-seats-in-side-by-side configuration development of the tandem-seating AutoGyro Calidus.It features a single main rotor, an enclosed cockpit with a complete aerodynamic cockpit fairing, tricycle landing gear with wheel pants and a four-cylinder, air and liquid-cooled, four-stroke, dual-ignition 100 hp (75 kW) Rotax 912 engine or turbocharged 115 hp (86 kW) Rotax 914 or 135 ...
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category and the US light-sport aircraft category. It features a cable-braced or strut-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem, open cockpit, tricycle landing gear with wheel pants and a single engine in pusher configuration.