Jump to content

Airfer Titan

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Cydebot (talk | contribs) at 06:50, 8 May 2019 (Robot - Moving category Spanish ultralight aircraft 2000–2009 to Category:2000s Spanish ultralight aircraft per CFD at Wikipedia:Categories for discussion/Log/2019 April 19.). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Titan
Role Paramotor
National origin Spain
Manufacturer Airfer
Status Production completed

The Airfer Titan is a family of Spanish paramotors that was designed and produced by Airfer of Pontevedra for powered paragliding. Now out of production, when the line was available the aircraft were supplied complete and ready-to-fly.[1]

Design and development

The Titan 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 Falcon 18 to 20 hp (13 to 15 kW) engine in pusher configuration with a 2.2:1 or 3.42:1 ratio reduction drive and a 99 to 122 cm (39 to 48 in) diameter two-bladed composite propeller. The fuel tank capacity is 9 litres (2.0 imp gal; 2.4 US gal). The aircraft is built from a combination of aluminium tubing, with a titanium chassis.[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

Titan 110
Model powered by a 18 hp (13 kW) Falcon engine with a 2.2:1 ratio reduction drive and a 99 cm (39 in) diameter two-bladed composite propeller.[1]
Titan 120
Model powered by a 20 hp (15 kW) Falcon engine with a 3.42:1 ratio reduction drive and a 122 cm (48 in) diameter two-bladed composite propeller.[1]

Specifications (Titan 110)

Data from Bertrand[1]

General characteristics

  • Crew: one
  • Empty weight: 20 kg (44 lb)
  • Fuel capacity: 9 litres (2.0 imp gal; 2.4 US gal)
  • Powerplant: 1 × Falcon single cylinder, two-stroke, air-cooled aircraft engine, with a 2.2:1 reduction drive, 13 kW (18 hp)
  • Propellers: 2-bladed composite, fixed pitch, 0.99 m (3 ft 3 in) diameter

References

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