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Mil Mi-40

Lighter-Than-Air Craft and Rotorcraft

The Mil Mi-40 was a projected armed troop transport helicopter, a kind of aerial infantry fighting vehicle meant to succeed the Mi-24 and the Mi-8 in the assault role. Work was first initiated in 1983, the project was announced in 1992 and a model was shown at the Moscow Airshow in 1993. It was to reuse the dynamic system of the Mi-28 attack helicopter, with two Klimov turboshaft engines of 1,863 kilowatts, a four-bladed main rotor, retractable tricycle landing gear and a 23 millimetre cannon, carrying seven or eight soldiers in an armoured cabin. The design was revived briefly in the 1990s with optimisation studies, but it never reached the prototype stage.

Facts
Year
1983 1
Engine Class
Turboshaft 2
Status
Design only (never built) 1
Top Speed (km/h)
314 1
Comparison
Body Style
Helicopter 1
Connections

Exemplifies

Aviation, Modes
Source Mi-40 and Mi-58 (GlobalSecurity.org)

Of Make

Source Mi-40 and Mi-58 (GlobalSecurity.org)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Mi-40 and Mi-58 (GlobalSecurity.org)Lead
Quote, Lead
The Mil Mi-40 was a projected utility version of the Mil Mi-28, first initiated in 1983, announced in 1992 and shown at the Moscow Airshow in 1993.
Sources
1. Mi-40 and Mi-58 (GlobalSecurity.org)
  • Lead
    The Mil Mi-40 was a projected utility version of the Mil Mi-28, first initiated in 1983, announced in 1992 and shown at the Moscow Airshow in 1993.
  • Opening paragraph
    The version of army troop-carrier helicopter obtained designation Mi-40, and purely passenger Mi-58.
  • Lead, outcome
    Although the Mi-40 design was resurrected for a short period in the 1990s, with optimisation studies being completed, it did not reach the prototype stage.
  • Second paragraph, engines
    It was planned to use two 1,863kW Kilmov TV-117VMA turboshaft engines, four-bladed main rotor, four-bladed Delta H tail rotor (both from the Mi-28), and retractable tricycle-type landing gear.
  • Second paragraph, estimated speed
    It was expected to weigh 11-12,000kg and estimated to attain a 3300m ceiling, a 314kph maximum speed and a 260kph cruise speed.
  • In Group: Military Transport and Utility Helicopters, Lead, role
    The Mil Mi-40 was primarily intended for the "Aerial Infantry Fighting Vehicle" [VBMP] category as a successor to the Mil Mi-24 and Mi-8 assault helicopters.
View the Source
2. Aviastar: Mil Mi-40
AviastarPower plant
Quote, Power plant
POWER PLANT: Two 1,863kW Klimov TV3-117VMA turboshafts.
View the Source
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