|
gptkbp:instanceOf
|
fighter aircraft
|
|
gptkbp:aircraft
|
gptkb:MiG_family
air superiority
jet aircraft
straight wing
|
|
gptkbp:armament
|
2 × 23 mm Nudelman-Rikhter NR-23 cannons
2 × 37 mm Nudelman N-37 cannons
|
|
gptkbp:built
|
approximately 600
1945-1946
|
|
gptkbp:cockpit
|
pressurized
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
gptkb:Mikoyan-Gurevich_design_bureau
|
|
gptkbp:design_feature
|
twin-engine
|
|
gptkbp:engine
|
RD-500
|
|
gptkbp:engineType
|
turbojet
|
|
gptkbp:firstFlight
|
1946
1960
|
|
gptkbp:hasExperienceIn
|
600 km
|
|
gptkbp:height
|
3.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
MiG-9P
|
|
gptkbp:is_used_in
|
gptkb:China
gptkb:Poland
gptkb:Soviet_Union
gptkb:Czechoslovakia
|
|
gptkbp:landing_gear
|
tricycle
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mikoyan-Gurevich
|
|
gptkbp:maximum_speed
|
1,050 km/h
|
|
gptkbp:maxRange
|
1,200 km
|
|
gptkbp:maxTakeoffWeight
|
6,000 kg
|
|
gptkbp:operational_status
|
1949
|
|
gptkbp:origin
|
gptkb:Soviet_Union
|
|
gptkbp:propulsion
|
2,500 kgf
|
|
gptkbp:retired
|
1955
|
|
gptkbp:retirementYear
|
1955
|
|
gptkbp:role
|
interceptor
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:services
|
gptkb:Soviet_Air_Forces
1949
|
|
gptkbp:speed
|
150 km/h
|
|
gptkbp:succeededBy
|
10°/s
|
|
gptkbp:successor
|
MiG-15
|
|
gptkbp:surrounding_area
|
20 m²
|
|
gptkbp:variant
|
gptkb:MiG-9P
MiG-9
MiG-9K
|
|
gptkbp:wingspan
|
8.5 m
|