Keitek Streamer
| Streamer | |
|---|---|
| Role | Ultralight trike |
| National origin | Italy |
| Manufacturer | Keitek |
| Status | In production (2013) |
| Unit cost |
€38,000 (2011) |
The Keitek Streamer is an Italian ultralight trike, designed and produced by Keitek of Remanzacco. The aircraft is supplied as a complete ready-to-fly-aircraft.[1]
Design and development
The aircraft 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). It features a strut-braced "topless" Hazard 12S or 15S hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit with a cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.[1]
The Streamer has a double surface wing covered in Dacron sailcloth. The Hazard 12S 9.8 m (32.2 ft) span wing has supporting struts and uses an "A" frame weight-shift control bar. The powerplant is a four cylinder, air and liquid-cooled, four-stroke, dual-ignition 80 hp (60 kW) Rotax 912UL engine. The fuel tank includes internal baffling and the engine oil tank is enclosed inside the fuselage.[1]
With the Hazard 12S wing the aircraft has an empty weight of 185 kg (408 lb) and a gross weight of 450 kg (992 lb), giving a useful load of 265 kg (584 lb). With full fuel of 64 litres (14 imp gal; 17 US gal) the payload is 219 kg (483 lb).[1]
The Hazard 12S wing has an area of 12 m2 (130 sq ft) and is intended for experienced pilots, while the Hazard 15S wing has a wing area of 15 m2 (160 sq ft) and is envisioned as a school and student training wing. The Hazard 12S wing gives a cruising speed that is 30 km/h (19 mph) faster than the 15S wing.[1]
Specifications (Streamer with Hazard 12S wing)
Data from Bayerl[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 9.8 m (32 ft 2 in)
- Wing area: 12 m2 (130 sq ft)
- Empty weight: 185 kg (408 lb)
- Gross weight: 450 kg (992 lb)
- Fuel capacity: 64 litres (14 imp gal; 17 US gal)
- Powerplant: 1 × Rotax 912UL four cylinder, liquid and air-cooled, four stroke aircraft engine, 60 kW (80 hp)
- Propellers: 3-bladed composite
Performance
- Cruising speed: 160 km/h (99 mph; 86 kn)
- Stall speed: 65 km/h (40 mph; 35 kn)
- Wing loading: 37.5 kg/m2 (7.7 lb/sq ft)
References
External links
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