|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:crew
|
2
|
|
gptkbp:debutYear
|
1965
|
|
gptkbp:design
|
twin-engine
skid landing gear
two-blade tail rotor
two-blade main rotor
low rotor system
high-mounted tail rotor
|
|
gptkbp:engine
|
2 × WSK PZL-3S
|
|
gptkbp:firstFlight
|
1961
|
|
gptkbp:fuelCapacity
|
600 L
|
|
gptkbp:height
|
3.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mil Mi-2
|
|
gptkbp:length
|
13.3 m
|
|
gptkbp:manufacturer
|
gptkb:Mikhail_Mil
|
|
gptkbp:maximumDepth
|
1,000 kg
|
|
gptkbp:maxSpeed
|
220 km/h
|
|
gptkbp:maxTakeoffWeight
|
3,200 kg
|
|
gptkbp:militaryRank
|
Mil Mi-2T
Mil_Mi-2B
Mil_Mi-2M
Mil_Mi-2P
Mil_Mi-2R
Mil_Mi-2S
|
|
gptkbp:notableUsers
|
gptkb:Soviet_Air_Force
gptkb:Czech_Air_Force
gptkb:Polish_Army
gptkb:Hungarian_Air_Force
|
|
gptkbp:operationalRange
|
600 km
|
|
gptkbp:passengerCapacity
|
8
2.5 m³
|
|
gptkbp:politicalParty
|
Mil Mi-2A
|
|
gptkbp:powerOutput
|
2 × 450 hp
|
|
gptkbp:productionCompany
|
1965-1985
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retirementYear
|
1990s
|
|
gptkbp:role
|
utility helicopter
|
|
gptkbp:services
|
1965
4,500 m
|
|
gptkbp:successor
|
Mil Mi-8
Mil Mi-8T
|
|
gptkbp:totalGoals
|
over 1,000
|
|
gptkbp:usedBy
|
gptkb:Hungary
gptkb:Poland
gptkb:Soviet_Union
gptkb:Czechoslovakia
|
|
gptkbp:variant
|
Mil Mi-2A
Mil Mi-2T
Mil_Mi-2B
Mil_Mi-2M
Mil_Mi-2P
Mil_Mi-2R
Mil_Mi-2S
|