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Aerosport OY Spider

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]

Spider
Role Paramotor
National origin Estonia
Manufacturer Aerosport OY
Status Production completed

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

References edit

  1. ^ a b c d e f g h i j k Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 63. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X

aerosport, spider, family, estonian, paramotors, that, designed, produced, aerosport, keila, powered, paragliding, production, when, series, were, available, aircraft, were, supplied, complete, ready, spiderrole, paramotornational, origin, estoniamanufacturer,. 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 SpiderRole ParamotorNational origin EstoniaManufacturer Aerosport OYStatus Production completed Contents 1 Design and development 2 Variants 3 Specifications Spider F33 4 ReferencesDesign and development editThe 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 editSpider 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 editData from Bertrand 1 General characteristicsCrew 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 diameterReferences edit a b c d e f g h i j k Bertrand Noel Rene Coulon et al World Directory of Leisure Aviation 2003 04 page 63 Pagefast Ltd Lancaster UK 2003 ISSN 1368 485X Retrieved from https en wikipedia org w index php title Aerosport OY Spider amp oldid 1113330168, wikipedia, wiki, book, books, library,

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