gptkbp:instanceOf
|
aircraft
|
gptkbp:aircraft
|
military aircraft
trainer aircraft
training and reconnaissance
|
gptkbp:armament
|
none
|
gptkbp:cockpit
|
open cockpit
|
gptkbp:constructionMaterial
|
metal construction
|
gptkbp:controls
|
elevator and ailerons
|
gptkbp:covers
|
none
|
gptkbp:crew
|
2
|
gptkbp:design
|
gptkb:Mitsubishi
1930s
Mitsubishi_design_team
|
gptkbp:engine
|
gptkb:Mitsubishi_Kasei_engine
|
gptkbp:engineType
|
piston engine
|
gptkbp:financial_aid
|
good stability
|
gptkbp:firstFlight
|
1939
|
gptkbp:handles
|
easy handling
|
gptkbp:headlights
|
conventional tail
|
gptkbp:height
|
2.5 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi M-23
|
gptkbp:landingGear
|
tailwheel
|
gptkbp:length
|
8.5 m
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
gptkbp:maxSpeed
|
200 km/h
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
gptkbp:nickname
|
gptkb:Mitsubishi_Trainer
|
gptkbp:numberBuilt
|
approximately 100
|
gptkbp:numberOfEpisodes
|
1
|
gptkbp:operationalHistory
|
gptkb:World_War_II
|
gptkbp:primaryUser
|
gptkb:Imperial_Japanese_Army_Air_Service
|
gptkbp:produces
|
limited production
|
gptkbp:propulsion
|
two-bladed
|
gptkbp:range
|
600 km
|
gptkbp:relatedAircraft
|
gptkb:Mitsubishi_M-21
|
gptkbp:retirementYear
|
1945
|
gptkbp:role
|
trainer aircraft
military trainer
|
gptkbp:service_ceiling
|
4,500 m
|
gptkbp:services
|
1940
5 years
|
gptkbp:setting
|
biplane configuration
|
gptkbp:successor
|
gptkb:Mitsubishi_M-24
|
gptkbp:supportRole
|
pilot training
|
gptkbp:takeoffDistance
|
150 m
200 m
|
gptkbp:type
|
biplane
|
gptkbp:variant
|
gptkb:M-23B
M-23A
|
gptkbp:wingArea
|
fabric covered
|
gptkbp:wingspan
|
10.5 m
|