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[1] [2] The powerplant options include the four cylinder, liquid-cooled, four-stroke, dual-ignition 100 hp (75 kW) Rotax 912ULS engine, or the 115 hp (86 kW) turbo-charged Rotax 914 engine. [1] [2] Originally an open-cockpit design with dual windshields, in 2013 a bubble canopy was introduced as an option. It weighs 20 kg (44 lb) and can be ...
In London, pilot Beatty demonstrated a Wright aircraft retrofitted with a 50-hp Gyro engine. [8] The Gyro progressed to 80-hp in the seven-cylinder model by 1913, and up to 110 hp in the Model L nine cylinder "Duplex" with a unique cam-driven exhaust valve. The French Gnome Omega and future variants proved to be more popular in sales.
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.
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.
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 communications satellite; Texas A&M College Ag-1, a prototype single seat, single engine aircraft
In June 2018, magniX publicly stated plans to fly an electric Cessna 208 Caravan with a 540 kW (720 hp) motor for up to an hour, by August 2019. [2] By then, the company's magni5 electric motor could produce 265–300 kW (355–402 hp) peak at 2,500 rpm at 95% efficiency with a 53 kg (117 lb) dry mass motor, having a 5 kW/kg (2.3 kW/lb) power ...
The vehicle was 40.0 by 9.8 feet (12.2 by 3 m), and with a 20-horsepower (15 kW) petrol engine, had a speed of 22 miles per hour (35 km/h). The transmission was electric, with the petrol engine driving a generator, and electric motors located on both bogies. This generator also supplied power to the gyro motors and the air compressor.
The air turborocket is a form of combined-cycle jet engine. The basic layout includes a gas generator, which produces high pressure gas, that drives a turbine/compressor assembly which compresses atmospheric air into a combustion chamber. This mixture is then combusted before leaving the device through a nozzle and creating thrust.
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