Edge Rewrite
// HTMLRewriter · presentation

This page was redesigned at the edge.

Cloudflare fetched the original article and streamed it through HTMLRewriter to apply an entirely new visual system without rebuilding the source page.

Jump to content

Mini-Fly Set

From Wikipedia, the free encyclopedia

Mini-Fly Set
General information
TypePowered hang glider
National origin
Germany
ManufacturerMini-Fly GmbH
StatusProduction completed

The Mini-Fly Set is a German powered hang glider that was designed and produced by Mini-Fly GmbH of Kirchardt. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.[1]

Design and development

[edit]

The aircraft features a cable-braced hang glider-style high-wing, weight-shift controls, single-place accommodation, foot-launching and landing and a single engine in pusher configuration.[1]

The aircraft uses a standard hang glider wing, made from bolted-together aluminum tubing, with its double surface wing covered in Dacron sailcloth. The wing is supported by a single tube-type kingpost and uses an "A" frame control bar. The engine is a two-stroke, single cylinder Sachs 166 industrial engine of 14 hp (10 kW) driving a 3.4:1 reduction drive. The engine is mounted at the front of, and below the wing on a separate tube running parallel to the wing's keel tube. The 10 litres (2.2 imp gal; 2.6 US gal) fuel tank is mounted above and behind the engine. The two-bladed, wooden, fixed pitch propeller with a 134 cm (53 in) diameter is located at the rear of the wing's keel tube and is protected from ground contact by a tail wheel mounted on a long aluminum tube. The propeller is driven by a long extension shaft.[1]

The pilot may take off in the prone position or from a standing start as in a conventional hang glider hill launch.[1]

Specifications

[edit]

Data from Bertrand[1]

General characteristics

  • Crew: one
  • Empty weight: 16 kg (35 lb) power unit only
  • Fuel capacity: 10 litres (2.2 imp gal; 2.6 US gal)
  • Powerplant: 1 × Sachs 166 single cylinder, air-cooled industrial engine with a 3.4:1 reduction drive, 10 kW (14 hp)
  • Propellers: 2-bladed wooden, fixed pitch, 1.34 m (4 ft 5 in) diameter

References

[edit]
  1. 1 2 3 4 5 Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 68. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X