|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:armament
|
none
|
|
gptkbp:aspectRatio
|
7.0
|
|
gptkbp:climbRate
|
3.5 m/s
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:conservationEfforts
|
in museums
|
|
gptkbp:constructionMaterial
|
wood and fabric
|
|
gptkbp:controls
|
elevators and ailerons
|
|
gptkbp:countryOfOrigin
|
gptkb:Germany
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
high-wing configuration
NAG_design_team
|
|
gptkbp:elevation
|
fin and rudder
|
|
gptkbp:engine
|
Hirth HM 504
|
|
gptkbp:firstFlight
|
1939
1960s
|
|
gptkbp:fuelCapacity
|
100 L
|
|
gptkbp:headlights
|
horizontal stabilizer
|
|
gptkbp:height
|
2.5 m
|
|
gptkbp:historicalSignificance
|
training_pilots_during_WWII
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
NAG Mk II
|
|
gptkbp:landingGear
|
tailwheel
conventional landing gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
NAG
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:nickname
|
NAG_Trainer
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:operationalHistory
|
used in flight schools
|
|
gptkbp:powers
|
140 hp
|
|
gptkbp:primaryUser
|
gptkb:German_Air_Force
|
|
gptkbp:productionLocation
|
gptkb:Germany
|
|
gptkbp:productionYears
|
1939-1945
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
600 km
|
|
gptkbp:relatedAircraft
|
gptkb:Bücker_Bü_131
gptkb:Focke-Wulf_Fw_44
Messerschmitt Bf 108
|
|
gptkbp:retired
|
gptkb:Luftwaffe
|
|
gptkbp:retirementYear
|
1950s
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:service_ceiling
|
4000 m
|
|
gptkbp:services
|
1940
|
|
gptkbp:setting
|
two-seat
|
|
gptkbp:speed
|
60 km/h
|
|
gptkbp:successor
|
gptkb:NAG_Mk_III
|
|
gptkbp:type
|
biplane
|
|
gptkbp:usedBy
|
gptkb:Luftwaffe
|
|
gptkbp:variant
|
gptkb:NAG_Mk_IIb
NAG Mk IIa
|
|
gptkbp:wingArea
|
15.5 m²
|
|
gptkbp:wingspan
|
10.5 m
|