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The Mil V-16 was a Soviet heavy cargo/transport helicopter project of the late 1960s. The Mil V-16 was designed by Mil Design Bureau, a Moscow helicopter plant. The original scheme described a heavy side-by-side twin-rotor aircraft with two Soloviev D-25VF 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, as well as located directly under the wings.

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  • ميل في-16 (ar)
  • Mil V-16 (en)
  • V-16 (航空機) (ja)
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  • ميل في-16 كانت مشروع مروحية نقل سوفيتية في آخر عام 1960م. المخطط الرئيسي وصف بأنها ثقيلة ذات محركين طائرة جنبًا إلى جنب بمحركي العنفة الغازية. (ar)
  • V-16は1960年代後半のソビエト連邦の貨物・輸送用の重ヘリコプター計画。胴体から左右に広がった厚い翼の両端にそれぞれ6枚羽のローターとガスタービンエンジンを持ち、着陸装置は3脚の降着輪で、後輪2つは翼の下に取り付けられ前輪はコクピットの下におかれる計画であった。 (ja)
  • The Mil V-16 was a Soviet heavy cargo/transport helicopter project of the late 1960s. The Mil V-16 was designed by Mil Design Bureau, a Moscow helicopter plant. The original scheme described a heavy side-by-side twin-rotor aircraft with two Soloviev D-25VF 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, as well as located directly under the wings. (en)
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  • Heavy transport helicopter project (en)
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  • ميل في-16 كانت مشروع مروحية نقل سوفيتية في آخر عام 1960م. المخطط الرئيسي وصف بأنها ثقيلة ذات محركين طائرة جنبًا إلى جنب بمحركي العنفة الغازية. (ar)
  • The Mil V-16 was a Soviet heavy cargo/transport helicopter project of the late 1960s. The Mil V-16 was designed by Mil Design Bureau, a Moscow helicopter plant. The original scheme described a heavy side-by-side twin-rotor aircraft with two Soloviev D-25VF 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, as well as located directly under the wings. Designed to be capable of transporting large numbers of combat units, the V-16 was also intended as a Soviet military vehicle transportation aircraft. This aircraft was one of the first for the USSR to begin using operational based algorithms within its controlling systems. (en)
  • V-16は1960年代後半のソビエト連邦の貨物・輸送用の重ヘリコプター計画。胴体から左右に広がった厚い翼の両端にそれぞれ6枚羽のローターとガスタービンエンジンを持ち、着陸装置は3脚の降着輪で、後輪2つは翼の下に取り付けられ前輪はコクピットの下におかれる計画であった。 (ja)
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