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KAI-14
The KAI-14 was a Standard Class sailplane designed and built in the USSR in the 1960s. Two participated in the World Gliding Championships of 1965.
==Design and development==
The Standard Class (single seat, span) KAI-14 was an all-metal aircraft designed and built at the Kazan Aviation Institute by a team led by M.P. Simonov in the USSR in the early 1960s. It was a shoulder wing, cantilever monoplane. The leading edge had a forward sweep of 2° and its trailing edge was compound tapered. The wing terminated with small streamlined bodies known as salmons and was rigged with 4° of dihedral. Its inset hinged ailerons were each divided into two sections and small area airbrakes were mounted inboard.〔 A braking parachute was deployed when landing.〔
The metal semi-monocoque fuselage had a forward section which contained the cockpit ahead of the wing leading edge but became markedly slimmer aft, in pod and boom style.〔 The KAI-14 had a 90° butterfly tail with straight tapered surfaces, squared tips and externally mass-balanced elevators.〔 It landed on a fixed monowheel, faired into the fuselage underside, which had a brake operated via the airbrake lever. The rear fuselage was protected by a tail bumper.〔
The KAI-14's cockpit could be configured in two ways, either with the pilot reclining under a long, fuselage contour following, one piece canopy or sitting upright under a shorter, raised canopy.〔 The first arrangement gave lower drag, the second better vision; the latter is sometimes referred to as the "trainer canopy".〔
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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