Mil Mi-40: Difference between revisions
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#REDIRECT [[Mil Mi-28#Mi-40]] |
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The '''Mil Mi-40''' is a projected utility version of the [[Mi-28]], first initiated in [[1983]], but announced in [[1992]] and shown at the [[Moscow]] Airshow in [[1993]]. It was planned to use two 1,863kW [[Kilmov TV-117VMA]] turboshaft engines, four-bladed main rotor, four-bladed Delta H tail rotor (both main and tail rotors used on [[Mi-28]]), and retractable tricycle-type landing gear. It was also planned to use a mast-mounted device, similar to that seen on the [[Mi-28N]], undernose 23mm gun turret, rear defensive 12.3mm gun on a flexible turret, and a maximum of eight [[air-to-air]] or [[air-to-surface]] missiles on outboard pylons. The '''Mi-40''' lost out to the [[Mil Mi-42|Mi-42]] project, which featured the [[NOTAR]] concept. |
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==External links== |
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[http://www.aviastar.org/helicopters_eng/mi-40.php ''Mil Mi-40'' at www.aviastar.org] |
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Latest revision as of 00:06, 16 June 2023
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