Engineering:Aero Adventure Pegasus
From HandWiki
Pegasus | |
---|---|
Role | Light utility aircraft |
National origin | United States |
Manufacturer | Aero Adventure Aviation |
The Aero Adventure Pegasus is a small civil utility aircraft (As of 2004) under development in the United States for sale as a kitplane. Of conventional monoplane configuration and composite construction, the Pegasus will seat its pilot and passenger in tandem and be available with a choice of two different wings, a longer wing for extended range, and a shorter wing for increased maneuverability.
Specifications (as designed, long wing)
General characteristics
- Crew: 1
- Capacity: 1 passenger
- Length: 20 ft 0 in (6.09 m)
- Wingspan: 23 ft 0 in (7.01 m)
- Height: 8 ft 0 in (2.44 m)
- Wing area: 62 sq ft (5.8 m2)
- Empty weight: 400 lb (181 kg)
- Gross weight: 2,756 lb (1,250 kg)
- Powerplant: 1 × Rotax 914 4-cylinder air-cooled horizontally-opposed piston engine, 115 hp (86 kW)
Performance
- Maximum speed: 248 kn (285 mph, 459 km/h)
- Range: 1,900 nmi (2,200 mi, 3,500 km)
- Service ceiling: 20,000 ft (6,100 m)
- Rate of climb: 800.6 ft/min (4.067 m/s)
See also
Original source: https://en.wikipedia.org/wiki/Aero Adventure Pegasus.
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