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__NOTOC__ The Mil V-16 was a Soviet heavy cargo/transport helicopter project of the late 1960s. The original scheme described a heavy side-by-side twin-rotor aircraft with two gas turbine engines below six-bladed rotors at the tips of heavily supported wings on each side of the fuselage and tricycle-type landing gear, with both rear landing wheels mounted below the wings while the front wheel was located below the cockpit area. A sample of V-16 has been on show at the Le Bourget-Paris "Salon de l'Aviation" in June, 1971. ==Variants== ;V-16: Proposed ''ultra-heavy'' version of the V-12, intended to lift . Originally envisaged in a three rotor layout, powered by six Soloviev D-25VF engines, but reverted to a two-rotor system similar to the V-12 powered by two large gas generators supplying a single large low pressure free-turbine driving a main gearbox each. ;Mi-16: The proposed VVS designation for the production V-16.〔 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Mil V-16」の詳細全文を読む スポンサード リンク
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