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LAK-17
The LAK-17 is a Lithuanian single-seat sailplane that was designed at the Lithuanian Aero Club ((リトアニア語: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 wingspan but a wing with span increased to 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.〔〔
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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