Raisner Graffiti
Graffiti | |
---|---|
Role | Ultralight trike |
National origin | United States |
Manufacturer | Raisner Aircraft Depot |
Designer | Bill Raisner |
Introduction | circa 1997 |
Status | Production completed |
The Raisner Graffiti is an American ultralight trike that was designed by Bill Raisner and produced by Raisner Aircraft Depot, a division of Leading Edge Air Foils of Peyton, Colorado and introduced about 1997. When it was available the aircraft was supplied as a kit for amateur construction.[1]
By 2014 the aircraft was no longer offered for sale by Leading Edge Air Foils.[2]
Design and development[]
The Graffiti was designed with the goals of maximizing safety, performance and simplicity of construction. It was intended to comply with the US FAR 103 Ultralight Vehicles rules, as a two-seat trainer. It features a cable-braced 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 aircraft is made from bolted-together aluminum tubing, with its double surface wing covered in Dacron sailcloth. Its 33.80 ft (10.3 m) span wing is supported by a single tube-type kingpost, uses an "A" frame weight-shift control bar and has a wing area of 160.0 sq ft (14.86 m2). The acceptable power range is 41 to 64 hp (31 to 48 kW) and the standard powerplant used is a de-rated twin cylinder, air-cooled, two-stroke, dual-ignition 53 hp (40 kW) Rotax 582 engine, optimized for quiet operation.[1]
The aircraft has an empty weight of 341 lb (155 kg) and a gross weight of 872 lb (396 kg), giving a useful load of 531 lb (241 kg).[1]
The standard day, sea level, no wind, take off with a 53 hp (40 kW) engine is 100 ft (30 m) and the landing roll is 150 ft (46 m).[1]
Specifications (Graffiti)[]
Data from AeroCrafter[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 33.80 ft (10.30 m)
- Wing area: 160.0 sq ft (14.86 m2)
- Empty weight: 341 lb (155 kg)
- Gross weight: 872 lb (396 kg)
- Powerplant: 1 × Rotax 582 de-rated twin cylinder, liquid-cooled, two stroke aircraft engine, 53 hp (40 kW)
- Propellers: 4-bladed composite
Performance
- Maximum speed: 77 mph (124 km/h, 67 kn)
- Cruise speed: 56 mph (90 km/h, 49 kn)
- Stall speed: 31 mph (50 km/h, 27 kn)
- Range: 200 mi (320 km, 170 nmi)
- Service ceiling: 19,700 ft (6,000 m)
- Wing loading: 5.5 lb/sq ft (27 kg/m2)
References[]
- 1990s United States sport aircraft
- 1990s United States ultralight aircraft
- Homebuilt aircraft
- Single-engined pusher aircraft
- Ultralight trikes
- Leading Edge Air Foils aircraft