|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
general aviation
retired
monoplane
straight wing
|
|
gptkbp:armament
|
none
|
|
gptkbp:aspectRatio
|
7.0
|
|
gptkbp:cockpit
|
analog gauges
tandem_seating
|
|
gptkbp:constructionMaterial
|
1.5 m
|
|
gptkbp:controls
|
elevator, ailerons, rudder
|
|
gptkbp:covers
|
manual flaps
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Corporation
Mitsubishi_engineers
|
|
gptkbp:enginePower
|
200 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1956
|
|
gptkbp:fuelCapacity
|
200 L
|
|
gptkbp:hasSecurity
|
1956 Air Show
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi M-35
|
|
gptkbp:influencedBy
|
gptkb:Mitsubishi_M-15
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:nationalTeam
|
gptkb:Japan
|
|
gptkbp:notableFeature
|
low-wing design
|
|
gptkbp:numberOfEpisodes
|
1
|
|
gptkbp:operationalHistory
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:primaryUser
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:productionLocation
|
gptkb:Mitsubishi_Nagoya_Plant
|
|
gptkbp:productionYears
|
1956-1970
|
|
gptkbp:propulsion
|
fixed-pitch propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:relatedAircraft
|
gptkb:Cessna_172
|
|
gptkbp:retirementYear
|
1970
|
|
gptkbp:role
|
light aircraft
trainer aircraft
|
|
gptkbp:services
|
1957
4,500 m
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:Mitsubishi_M-60
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:totalGoals
|
100
|
|
gptkbp:type
|
military trainer
|
|
gptkbp:usedIn
|
pilot training
|
|
gptkbp:variant
|
M-35A
M-35B
|
|
gptkbp:weight
|
800 kg
|
|
gptkbp:wingArea
|
15 m²
|
|
gptkbp:wingspan
|
10.5 m
|