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gptkbp:instance_of
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gptkb:fighter_aircraft
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gptkbp:armament
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gptkb:cannon
missiles
|
|
gptkbp:avionics
|
analog
|
|
gptkbp:ceiling
|
17,000 m
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|
gptkbp:cockpit
|
tandem seating
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|
gptkbp:combat_experience
|
limited
|
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gptkbp:combat_radius
|
600 km
|
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gptkbp:crew
|
2
|
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gptkbp:current_status
|
retired from active service
|
|
gptkbp:design
|
dual-role trainer
|
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gptkbp:engine_type
|
turbojet
|
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gptkbp:exported_to
|
many countries
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gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuselage_material
|
aluminum
|
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gptkbp:height
|
4.13 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mi G-21 UM
|
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gptkbp:influenced
|
future aircraft designs
|
|
gptkbp:influenced_by
|
gptkb:Mi_G-15
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
14.76 m
|
|
gptkbp:manufacturer
|
gptkb:Mikoyan
|
|
gptkbp:max_speed
|
2,175 km/h
|
|
gptkbp:max_takeoff_weight
|
6,500 kg
|
|
gptkbp:nickname
|
Fishbed
|
|
gptkbp:notable_case
|
various accidents
|
|
gptkbp:number_built
|
over 1,000
|
|
gptkbp:operating_countries
|
gptkb:Egypt
gptkb:India
gptkb:Soviet_Union
gptkb:Czechoslovakia
|
|
gptkbp:operational_cost
|
low
|
|
gptkbp:operator
|
gptkb:India
|
|
gptkbp:payload_capacity
|
3,000 kg
|
|
gptkbp:propulsion
|
0.9
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retired
|
many air forces
|
|
gptkbp:retirement
|
1990s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:roll_rate
|
30°/s
|
|
gptkbp:seating_capacity
|
K-36
|
|
gptkbp:service
|
1965-1990s
|
|
gptkbp:service_entry
|
gptkb:1965
|
|
gptkbp:successor
|
gptkb:X-23
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:upgrades
|
various modernization programs
|
|
gptkbp:variant
|
gptkb:Mi_G-21
|
|
gptkbp:weight
|
3,500 kg
|
|
gptkbp:wing_configuration
|
delta wing
|
|
gptkbp:wingspan
|
7.15 m
|
|
gptkbp:bfsParent
|
gptkb:Mi_G-21
|
|
gptkbp:bfsLayer
|
5
|