| Airsport | |
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HW100 - 45000
UAW55 - 105000 RRW100 - 175000 PKRR - 7500 |
Airsport Airsport s.r.o. Company type - Privately held company Industry - Aerospace Founded - April 27, 2002 Founder - Jan Pajer Headquarters - Zbraslavice, Czech Republic Products - Kit aircraft, microlight aircraft, motorgliders Website - www.airsport.cz/AIRSPORT/DOMU.html Airsport s.r.o. is a Czech aircraft manufacturer based in Zbraslavice. The company specializes in the design and manufacture of microlight aircraft and motorgliders in the form of kits for amateur construction and ready-to-fly aircraft for the European Fédération Aéronautique Internationale microlight category. The organization is a Czech společnost s ručením omezeným (s.r.o.), or private limited company. The company has three designs in production as of 2015, all constructed from composite materials. The Airsport Sonet is a light touring aircraft derived from the Airsport Sonata motorglider. The Airsport Song is a single-seat motorglider, with an unusual twin-boom and inverted V-tail layout. Aircraft Summary of aircraft built by Airsport Model name - First flight - Number built - Type Airsport Sonet - _ - _ - Two-seat light touring microlight aircraft Airsport Sonata - _ - _ - Two-seat motorglider Airsport Song - _ - _ - Single-seat motorglider Airsport Sonata Airsport Sonata Role - Ultralight aircraft National origin - Czech Republic Manufacturer - Airsport Status - In production The Airsport Sonata is a Czech ultralight motor glider with retractable propeller, designed and produced by Airsport of Zbraslavice. Design and development The aircraft features a cantilever low-wing, a T-tail, a two-seats-in-side-by-side configuration enclosed cockpit, electric flaps, a retractable landing gear, and a single engine in tractor configuration. The Sonata is made from composites. Its polyhedral wing is 15 m (49.2 ft). Standard engines available are the 65 hp (48 kW) Rotax 582 two-stroke and the 60 hp (45 kW) Hirth F34 powerplant. Specifications (Data from Pilotmix) General characteristics Crew: one Capacity: one passenger Empty weight: 278 kg (613 lb) Gross weight: 450 kg (992 lb) Powerplant: 1 × Rotax 582 twin cylinder, liquid air-cooled, two stroke, 37 kW (50 hp) Performance Cruise speed: 90 km/h (56 mph, 49 kn) Stall speed: 55 km/h (34 mph, 30 kn) Never exceed speed: 330 km/h (210 mph, 180 kn) Rate of climb: 2 m/s (390 ft/min) Airsport Sonet Airsport Sonet Role - Ultralight aircraft National origin - Czech Republic Manufacturer - Airsport Status - In production (2015) Developed from - Airsport Sonata The Airsport Sonet (English: Sonnet) is a Czech ultralight aircraft, designed and produced by Airsport of Zbraslavice. The aircraft is supplied in complete, ready-to-fly form. Design and development The aircraft was derived from the Airsport Sonata motor glider and designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a T-tail, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration. The Sonet is made from composites. Its polyhedral wing comes in three optional spans: 10.2 m (33.5 ft), 11.4 m (37.4 ft) and 15 m (49.2 ft). It requires an engine of about 65 hp (48 kW) and no more than 60 kg (132 lb). Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke and the 60 hp (45 kW) HKS 700E four-stroke powerplant. Specifications (Sonet 11.4) (Data from Bayerl and Tacke) General characteristics Crew: one Capacity: one passenger Wingspan: 11.7 m (38 ft 5 in) Wing area: 10.5 m2 (113 sq ft) Empty weight: 265 kg (584 lb) Gross weight: 450 kg (992 lb) Fuel capacity: 60 litres (13 imp gal; 16 US gal) in two tanks Powerplant: 1 × Rotax 582 twin cylinder, liquid air-cooled, two stroke, 48 kW (64 hp) Performance Maximum speed: 201 km/h (125 mph, 109 kn) Cruise speed: 140 km/h (87 mph, 76 kn) Stall speed: 64 km/h (40 mph, 35 kn) Rate of climb: 4 m/s (790 ft/min) Wing loading: 42.9 kg/m2 (8.8 lb/sq ft) Airsport Song Airsport Song Role - Ultralight aircraft National origin - Czech Republic Manufacturer - Airsport Designer - Marek Ivanov Status - In production The Airsport Song is a Czech ultralight aircraft, designed by Marek Ivanov and produced by Airsport of Zbraslavice. Design and development The aircraft was designed to comply with the LTF-L 120 kg, US FAR 103 Ultralight Vehicles and English SSDR categories. It features a cantilever low-wing, twin-booms, a single seat enclosed cockpit, fixed tricycle landing gear and a single engine in pusher configuration. The Song has been produced in both a twin–tail and inverted V-tail layout. In most configurations, the Song includes a Galaxy GRS 3/270 ballistic parachute rescue system. The Song is made from composites. Its polyhedral wing comes in two optional spans: 7.5 m (24.6 ft) (with flaperons) and 11.2 m (36.7 ft) (with ailerons and either spoilers or flaps). Standard engines available are the 20.5 hp (15 kW) Bailey V5 four-stroke and the 35 hp (26 kW) Verner JCV 360 four-stroke powerplant. Randall Fishman of Electric Aircraft Corporation produces an electric-powered version of the Song, the Electric Aircraft Corporation ElectraFlyer-ULS. Specifications (Song SW-V) (Data from Airsport) General characteristics Crew: one Length: 5.9 m (19 ft 4 in) Wingspan: 11.2 m (36 ft 9 in) Wing area: 10.5 m2 (113 sq ft) Empty weight: 110 kg (243 lb) Gross weight: 220 kg (485 lb) Fuel capacity: 25 litres (5.5 imp gal; 6.6 US gal) Powerplant: 1 × Bailey V5 Single Cylinder, 4 stroke, force air cooled, 2 valves per cylinder, cast alloy, 15.3 kW (20.5 hp) Performance Maximum speed: 201 km/h (125 mph, 109 kn) Cruise speed: 80 km/h (50 mph, 43 kn) Stall speed: 50 km/h (31 mph, 27 kn) Never exceed speed: 140 km/h (87 mph, 76 kn) Rate of climb: 1.5 m/s (300 ft/min) with Bailey V5, (5 m/s with Verner JCV 360) |