Aerosport OY Spider
| Spider | |
|---|---|
| Role | Paramotor |
| National origin | Estonia |
| Manufacturer | Aerosport OY |
| Status | Production completed |
The Aerosport OY Spider is a family of Estonian paramotors that was designed and produced by Aerosport OY of Keila for powered paragliding. Now out of production, when the series were available the aircraft were supplied complete and ready-to-fly.[1]
Design and development
[edit]The Spider line was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations. It features a paraglider-style wing, single-place accommodation and a single engine in pusher configuration with a reduction drive. The fuel tank capacity is 10 litres (2.2 imp gal; 2.6 US gal). The basic design is built from aluminium tubing, plus a nylon harness. The various models employ different engine, reduction drive and propeller combinations.[1]
As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.[1]
Variants
[edit]- Spider F33
- Model with a single Hirth F33 27 hp (20 kW) engine, a 2.2:1 ratio reduction drive and a 125 cm (49 in) diameter propeller[1]
- Spider F33 BL
- Model with a single Hirth F33 27 hp (20 kW) engine, a 2.7:1 ratio reduction drive and a 125 cm (49 in) diameter propeller[1]
- Spider M21Y
- Model with a single Cors'Air M21Y 24 hp (18 kW) engine and a 2.48:1 ratio reduction drive and a 95 to 125 cm (37 to 49 in) diameter propeller[1]
- Spider M21Y BL
- Model with a single Cors'Air M21Y 24 hp (18 kW) engine, a 2.6:1 ratio reduction drive and a 95 to 125 cm (37 to 49 in) diameter propeller[1]
- Spider PS2000
- Model with a single PS2000 16 hp (12 kW) engine, a 2.5:1 ratio reduction drive and a 125 cm (49 in) diameter propeller[1]
- Spider Racket
- Model with a single Radne Raket 120 14 hp (10 kW) engine, a 3.8:1 ratio reduction drive and a 125 cm (49 in) diameter propeller[1]
- Spider Solo
- Model with a single Solo 210 14 hp (10 kW) engine and a 2.5:1 ratio reduction drive and a 95 to 125 cm (37 to 49 in) diameter propeller[1]
Specifications (Spider F33)
[edit]Data from Bertrand[1]
General characteristics
- Crew: one
- Empty weight: 27 kg (60 lb)
- Fuel capacity: 10 litres (2.2 imp gal; 2.6 US gal)
- Powerplant: 1 × Hirth F33 single cylinder, two-stroke, air-cooled aircraft engine, with a 2.2:1 reduction drive, 20 kW (27 hp)
- Propellers: 2-bladed, 1.25 m (4 ft 1 in) diameter