To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Sportinė Aviacija LAK-20

From Wikipedia, the free encyclopedia

LAK-20
Role Open Class sailplane
National origin Lithuania
Manufacturer AB Sportinė Aviacija

The LAK-20 is a Lithuanian Open Class two-seat sailplane produced by Sportinė Aviacija.

YouTube Encyclopedic

  • 1/2
    Views:
    789
    727
  • Prie sportinės aviacijos ištakų su Jonu Balčiūnu
  • Visi į aviacijos šventę ! Kauno aerodromui - 95

Transcription

Design and development

The LAK-20 is an Open Class two-seat sailplane with a wingspan of 23-metres or 26-metres. Made out of modern composite materials, it features a T-tail and retractable landing gear. The wings are slightly swept forward and interchangeable outer wing panels are provided to enable it to fly with a wingspan of either 23 metres or 26 metres. The glider is available as the self-sustaining LAK-20T variant or the self-launching LAK-20M variant, both equipped with an engine. The engines used are two-stroke two-cylinder retractable engines from engine manufacturer SOLO.

Variants

LAK-20T
Production variant, self-sustaining sailplane with a 22 kW (30 hp) two-stroke two-cylinder air-cooled Solo 2350C retractable engine.
LAK-20M
Production variant, self-launching sailplane with a 47 kW (64 hp) two-stroke two-cylinder liquid-cooled Solo 2625 02 retractable engine.

Specifications (LAK-20T 26-metre)

Data from [1][2]

General characteristics

  • Crew: two
  • Length: 8.65 m (28 ft 4.5 in)
  • Wingspan: 26 m (85 ft 4 in)
  • Height: 1.011 m (3 ft 4 in)
  • Wing area: 16.4 m2 (176.5 sq ft)
  • Aspect ratio: 41.25
  • Empty weight: 485 kg (1,069 lb)
  • Gross weight: 850 kg (1,873 lb)
  • Powerplant: 1 × Solo 2350C , 22 kW (30 hp)

Performance

  • Maximum speed: 275 km/h (171 mph, 149 kn)
  • Maximum glide ratio: 60

References

  1. ^ "LAK-20T/M". lak.lt. Retrieved 2012-12-09.
  2. ^ Solo Kleinmotoren GmbH. "Solo Kleinmotoren GmbH Flugmotoren". Aircraft.solo-online.com. Retrieved 2012-12-09.
This page was last edited on 31 October 2020, at 10:41
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.