|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
low-wing
|
|
gptkbp:armament
|
none
|
|
gptkbp:cockpit
|
tandem_seating
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:controls
|
ailerons
elevator
rudder
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Company
basic trainer
|
|
gptkbp:enginePower
|
200 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:fuelCapacity
|
200 L
|
|
gptkbp:headlights
|
T-tail
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi Kasei 21
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:numberOfEpisodes
|
1
|
|
gptkbp:operationalHistory
|
used in training missions
|
|
gptkbp:primaryUser
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:productionYears
|
1955-1960
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:relatedAircraft
|
gptkb:Mitsubishi_Kasei_23
Mitsubishi_Kasei_15
Mitsubishi_Kasei_18
Mitsubishi_Kasei_22
Mitsubishi_Kasei_24
|
|
gptkbp:retirementYear
|
1965
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:services
|
3,000 m
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:Mitsubishi_T-2
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:variant
|
Mitsubishi_Kasei_21A
Mitsubishi_Kasei_21B
|
|
gptkbp:weight
|
800 kg
|
|
gptkbp:wingspan
|
10.5 m
|