The LAK-17 is a Lithuanian single-seat sailplane that was designed at the Lithuanian Aero Club (Lithuanian: Lietuviškos aviacinės konstrukcijos or LAK), and is manufactured by Sportinė Aviacija.

Design and development

The LAK-17 is designed to meet the requirements of the utility category of JAR-22. It is a single-seat mid-wing sailplane of composite construction with a T-tail and flaps, it has a retractable single-wheel main landing gear and has airbrakes on the upper wing surface. The airfoil is a combination of the LAP92-130/15, at its roots, and the LAP-92-150/15, at its tips. The LAK-17 holds water ballast in tanks in the wing and fin. The LAK-17A was certified in November 1994 by the Lithuanian Civil Aviation Authority. A new variant with an improved wing was designated the LAK-17B. All variants have a 15.00 m (49.21 ft) wingspan but a wing with span increased to 18.00 m (59.06 ft) is available as an option; powered self-sustaining versions are also produced.

An optional front electric sustainer engine variant was developed for the LAK-17 by Slovenian engineers at LZ Design. It originally had a 0.9 metre propeller, and the latest versions have a 1.0 metre propeller in the nose driven by an electric motor.

Variants

LAK-17A
Production flapped 15- or 18-metre wingspan sailplane.
LAK-17AT
Powered self-sustaining sailplane variant of the LAK-17A with a Solo 2350 two-cylinder air-cooled two-stroke retractable engine.
LAK-17A FES
A LAK-17A with a front electric sustainer.
LAK-17B
Improved variant with new wing profile and modified geometry.
LAK-17BT
Powered self-sustaining sailplane variant of the LAK-17B with a Solo 2350 retractable engine.
LAK-17B FES
A LAK-17B with a front electric sustainer.
LAK-17C FES
Improved variant with aerodynamic changes as well as a raised undercarriage to provide increased ground clearance for the folding propeller and increased battery capacity for self launching.

Specifications (LAK-17A with 15 metre wingspan)

Data from

General characteristics

  • Crew: one
  • Capacity: 188 kg (414 lb) water ballast
  • Length: 6.53 m (21 ft 5 in)
  • Wingspan: 15.00 m (49 ft 2 in)
  • Height: 1.29 m (4 ft 3 in)
  • Wing area: 9.06 m2 (97 sq ft)
  • Aspect ratio: 24.63
  • Empty weight: 245 kg (540 lb)
  • Gross weight: 500 kg (1,102 lb)

Performance

  • Maximum speed: 275 km/h (171 mph, 149 kn)
  • Maximum glide ratio: 45
  • Rate of sink: 0.53 m/s (104 ft/min)

References

External links

  • Official website

LAK LAK17 Gliders Recreational Flying

LAK17C FES LZ Design FES

LAK 17 Alchetron, The Free Social Encyclopedia

LAK 17 Alchetron, The Free Social Encyclopedia

LAK 17 Alchetron, The Free Social Encyclopedia