Mil V-16

From Wikipedia, the free encyclopedia

The Mil V-16, was a heavy cargo/transport helicopter project of the late 1960's. The original sceme 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, both rear landing wheels mounted below the wings while the front wheel located below the cockpit area.

[edit] External links

Mil V-16 at www.aviastar.org