|
gptkbp:instanceOf
|
military aircraft
|
|
gptkbp:aircraft
|
gptkb:Mikoyan_MiG_family
single-engine
low-wing
straight wing
150 kg/m²
|
|
gptkbp:armament
|
cannons
missiles
|
|
gptkbp:avionics
|
analog
|
|
gptkbp:built
|
over 1,000
|
|
gptkbp:climbRate
|
20 m/s
|
|
gptkbp:cockpit
|
single-seat
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:crew
|
1
|
|
gptkbp:crew_size
|
yes
|
|
gptkbp:design
|
gptkb:Mikoyan-Gurevich
|
|
gptkbp:engine
|
RD-500
|
|
gptkbp:engineType
|
jet engine
|
|
gptkbp:exportedTo
|
gptkb:China
gptkb:Egypt
gptkb:Hungary
gptkb:India
gptkb:North_Korea
gptkb:Poland
gptkb:Czechoslovakia
|
|
gptkbp:firstFlight
|
1950
|
|
gptkbp:fuel_capacity
|
1,500 L
|
|
gptkbp:hasExperienceIn
|
gptkb:Vietnam_War
1,000 km
|
|
gptkbp:headlights
|
T-tail
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
M-39
|
|
gptkbp:introduced
|
1951
|
|
gptkbp:is_used_in
|
gptkb:Soviet_Union
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mikoyan
|
|
gptkbp:maximum_speed
|
1,100 km/h
|
|
gptkbp:maxTakeoffWeight
|
4,500 kg
|
|
gptkbp:nickname
|
Fagot
|
|
gptkbp:primaryUser
|
gptkb:Soviet_Air_Force
|
|
gptkbp:productionYears
|
1950-1955
|
|
gptkbp:propulsion
|
0.9
|
|
gptkbp:radar
|
no
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:retirementYear
|
1995
|
|
gptkbp:role
|
fighter aircraft
interceptor
|
|
gptkbp:safety_features
|
none
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:serviceHistory
|
gptkb:Cold_War
|
|
gptkbp:speed
|
120 km/h
|
|
gptkbp:succeededBy
|
30°/s
|
|
gptkbp:successor
|
gptkb:Mikoyan_MiG-21
|
|
gptkbp:surrounding_area
|
20 m²
|
|
gptkbp:takeoffDistance
|
500 m
600 m
150 km/h
|
|
gptkbp:team
|
air superiority
|
|
gptkbp:variant
|
M-39A
M-39B
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:wingspan
|
8.0 m
|