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gptkbp:instance_of
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gptkb:helicopter
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:crew
|
2
|
|
gptkbp:design_feature
|
gptkb:helicopter
low operating costs
two-bladed main rotor
open cabin
retractable landing gear
high-mounted rotor system
high payload capacity
versatile mission capabilities
good maneuverability
skid landing gear
large side doors
reliable engine performance
good stability in flight
large windows for visibility
rear loading ramp
simple maintenance requirements
low noise levels during operation
good performance at high altitudes
fuselage made of metal
pilot's cabin with dual controls
|
|
gptkbp:engine
|
gptkb:Klimov_VK-1
|
|
gptkbp:first_flight
|
1948
|
|
gptkbp:height
|
3.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mil Mi-1
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mikhail_Mil
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:notable_users
|
gptkb:Polish_Air_Force
gptkb:East_German_Air_Force
gptkb:Soviet_Army
gptkb:Hungarian_Air_Force
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:passenger_capacity
|
gptkb:6
|
|
gptkbp:produces
|
over 1,000
|
|
gptkbp:production_years
|
gptkb:1960
1948
|
|
gptkbp:range
|
500 km
|
|
gptkbp:role
|
cargo transport
medical evacuation
transport helicopter
VIP transport
|
|
gptkbp:service_entry
|
1951
|
|
gptkbp:successor
|
gptkb:Mil_Mi-4
|
|
gptkbp:used_by
|
gptkb:Soviet_Air_Force
|
|
gptkbp:variant
|
Mil Mi-1 A
Mil Mi-1 B
Mil Mi-1 D
|
|
gptkbp:weight
|
2,800 kg
|
|
gptkbp:weight_limit
|
4,000 kg
|
|
gptkbp:wingspan
|
12.5 m
|
|
gptkbp:bfsParent
|
gptkb:Mikhail_Mil
gptkb:Moscow_Mil_Design_Bureau
|
|
gptkbp:bfsLayer
|
7
|