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.

// request.cf · coarse context

A page that knows where it met you.

Only coarse request metadata is shown. This demo does not display or persist visitor IP addresses.

Country
US
Cloudflare location
CMH
Connection
HTTP/2
Language
Not provided

Ray ID: a2460bef5f094b2a

Jump to content

// Workers AI · dad joke modeWhat did Wezel Apis 2 say to its friend? Bee there soon.

From Wikipedia, the free encyclopedia

Apis 2
General information
TypeMotor glider
National originGermany
ManufacturerWezel Flugzeugtechnik
StatusIn production
History
First flight2002

The Wezel Apis 2 is a German mid-wing, T-tailed, single-seat motor glider that was designed and produced by Wezel Flugzeugtechnik.[1][2] It first flew in 2002.

Often confused with the very similar Albastar Apis, the two designs are not related.[1]

The rights to the Apis 2 design were sold to Yuneec International of China in 2011 with the intention of selling only an electric version. Wezel announced in June 2012 that the move of production had been delayed indefinitely.[3][4]

Design and development

[edit]

The Apis 2 is a retractable engine motor glider that is powered by a 28 hp (21 kW) Hirth F-33 single cylinder, two-stroke powerplant, fitted with a tractor propeller. The engine is retracted into a bay behind the cockpit for soaring flight. The Apis 2 is built predominantly of composites. The 15 m (49.2 ft) span wing features winglets and produces a 39:1 glide ratio. The landing gear is a retractable monowheel gear.[1]

In 2003 the aircraft was offered for 50,950 complete.[1]

Specifications (Apis 2)

[edit]

Data from World Directory of Leisure Aviation 2003-04[1]

General characteristics

  • Crew: one
  • Wingspan: 15.00 m (49 ft 3 in)
  • Wing area: 12.4 m2 (133 sq ft)
  • Gross weight: 300 kg (661 lb)

Performance

  • Stall speed: 60 km/h (37 mph, 32 kn)
  • Never exceed speed: 200 km/h (120 mph, 110 kn)
  • Maximum glide ratio: 39:1
  • Rate of sink: 0.6 m/s (120 ft/min)
  • Wing loading: 24.2 kg/m2 (5.0 lb/sq ft)

See also

[edit]

References

[edit]
  1. 1 2 3 4 5 Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 60. Pagefast Ltd, Lancaster OK, 2003. ISSN 1368-485X
  2. Pilot Mix (n.d.). "Martin Wezel Flugzeugtechnik Apis 2". Retrieved 25 October 2011.
  3. Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 138. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  4. Wezel Flugzeuge (2012). "Apis 2". Retrieved 5 December 2012.
[edit]