| ABS Aerolight Navigathor | |
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HW100 - 45000
UAW55 - 105000 RRW100 - 175000 PKRR - 7500 |
ABS Aerolight Navigathor Navigathor Role - Powered parachute and roadable aircraft National origin - France Manufacturer - ABS Aerolight Status - Production completed The ABS Aerolight Navigathor is a French powered parachute and roadable aircraft that was designed and produced by ABS Aerolight of Sérignan-du-Comtat. Now out of production, when it was available the aircraft was supplied as a complete ready-to-fly-aircraft and as a kit for amateur construction. The company appears to have gone out of business in late 2007 and production ended. Design and development The Navigathor is a development of the earlier ATE, which stands for Air-Terre-Eau (English: Air-Land-Water) and indicates that the vehicle is capable of being used as a flying car with a top road speed of 150 km/h (93 mph) or as a boat with a top water speed of 7 km/h (4 mph). As an aircraft the Navigathor was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 450 kg (992 lb). The aircraft has a maximum gross weight of 450 kg (992 lb). The aircraft carriage is built from a combination of metal tubing and composites and features a wedge-shaped boat hull. It features a 46 m2 (500 sq ft) parachute-style wing, two-seats-in-tandem in an open cockpit, four-wheeled cross country all terrain vehicle style landing gear and a single 105 hp (78 kW) Hirth F-30 four-cylinder, horizontally opposed, two-stroke, aircraft engine, mounted in pusher configuration. In all modes the vehicle is powered by its ducted propeller. The vehicle has an empty weight of 230 kg (507 lb) and a gross weight of 450 kg (992 lb), giving a useful load of 220 kg (485 lb). With full fuel of 35 litres (7.7 imp gal; 9.2 US gal) the payload is 195 kg (430 lb). Variants 1) ATE Initial model flying car/boat, Air-Terre-Eau (English: Air-Land-Water). 2) Navigathor Improved model flying car/boat. Specifications (Navigathor) Data from Bertrand General characteristics Crew: one Capacity: one passenger Wingspan: 11 m (36 ft 1 in) Wing area: 46 m2 (500 sq ft) Aspect ratio: 2.7:1 Empty weight: 230 kg (507 lb) Gross weight: 450 kg (992 lb) Fuel capacity: 35 litres (7.7 imp gal; 9.2 US gal) Powerplant: 1 × Hirth F-30 four cylinder, two-stroke, air-cooled aircraft engine, 78 kW (105 hp) Performance Rate of climb: 3 m/s (590 ft/min) Wing loading: 9.7 kg/m2 (2.0 lb/sq ft) wikipedia.org (en) |