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Military


Mi-1 HARE

Specifications
Country of Origin Russia
Builder MIL
Role Utility, liaison
Similar Aircraft None
Rotor diameter 47 ft (14.36 m)
Length 39 ft, 8 in (12.2 m)
Height  
Weight  
Engine  
Maximum speed  
Cruising speed  
Range  
Service Ceiling  
Armament Usually none
Crew One
Cost  
User Countries
  • USSR
  • Albania
  • Algeria
  • Afghanistan
  • Bulgaria
  • Czechoslovakia
  • China
  • Cuba
  • Egypt
  • Finland
  • GDR
  • Hungary
  • Indonesia
  • Iraq
  • Mongolia
  • North Korea
  • Poland
  • Romania
  • Vietnam
  • Yemen
Variants
  • Mi-1U (GM-2, 1950) - double training, with double control.
  • Mi-1T (1953) - with an AI-26V engine and a resource increased to 300 hours, in 1954 an Arctic version was created for basing on icebreakers.
  • Mi-1KR (1956), Mi-1TCR - artillery spotters.
  • Mi-1H (1956, from 1959 had the name "Moskvich") is a national economic one. On its basis, representative versions were built on a piece-by-piece basis. So, in 1960-1968 he was used by the President of Finland Urho Kekkonen.
  • Mi-1A (1957) - with a resource aggregates, increased to 600 hours, and a node for attaching an additional fuel tank.
  • Mi-3 (1954) - sanitary modification with a four-bladed rotor, a more comfortable cabin, hanging gondolas for transporting the sick and wounded.
  • Mi-1M (1957) - modernized version with increased life, all-weather equipment and luggage compartment.
  • Mi-1MG (1958) - modification with a float chassis, was used on ships of the Soviet Antarctic whaling flotilla "Glory".
  • Mi-1MU, Mi-1MRK (1960) - training and reconnaissance and correction versions of Mi-1M.
  • Mi-1NX "Moskvich" Moscow Helicopter Plant them. M.L. Mile
  • Mi-1NX "Moskvich"




Main data GM-1 Mi-1 Mi-1T Mi-3 Mi-1À Mi-1M Mi-1MU armed
Year of manufacture 1948 1951 1953 1954 1957 1957 1961
Crew 1 1 1 1 1 1 2
Passengers 2 2 2 3 2 3 -
Power plant type AI-26GR AI-26GRF AI-26V AI-26V AI-26V AI-26VF AI-26VF
Take-off power, hp 550 575 575 575 575 615 615
Main rotor diameter, m 14,3 14,3 14,3 14,3 14,3 14,3 14,3
Empty weight, kg - 1700 1796 1715 1796 1900 2092
Take-off weight, kg
      normal 2065 2140 2230 2500 2300 2470 2550
      maximum - 2330 2300 - 2340 2550 2650
Payload, kg
      normal - - - 150 - 330 -
      maximum - - - 230 - - -
      on external sling - - - - - 500 -
Flight speed, km/h
      maximum 205 185 175 185 175 190 160
      cruising - - - 155 140 140 135
Hovering ceiling, m
      out of ground effect - - - - - 1200 -
      in ground effect 3300 2700 2700 - 2700 3450 -
Service ceiling, m - 3500 3500 4000 3000 4000 3000
Operational flight range, km 430 430 380 380 370 360 165



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