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gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
cantilever wing
|
|
gptkbp:armament
|
none
|
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gptkbp:climbRate
|
5 m/s
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|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:constructionMaterial
|
metal construction
NACA 2412
|
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gptkbp:controls
|
elevator, ailerons, rudder
dual control
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|
gptkbp:countryOfOrigin
|
gptkb:Germany
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
gptkb:Wolfgang_Bücker
simple construction
|
|
gptkbp:engine
|
Hirth HM 504
|
|
gptkbp:firstFlight
|
1945
|
|
gptkbp:fuelCapacity
|
100 liters
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:height
|
2.3 m
|
|
gptkbp:historicalSignificance
|
post-war training aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bücker Bü 182
|
|
gptkbp:influencedBy
|
gptkb:Bücker_Bü_181
|
|
gptkbp:introduced
|
1945
|
|
gptkbp:landingGear
|
tailwheel
fixed landing gear
|
|
gptkbp:length
|
7.5 m
|
|
gptkbp:manufacturer
|
gptkb:Bücker_Flugzeugbau
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
900 kg
|
|
gptkbp:nickname
|
gptkb:Bücker_Jungmann
|
|
gptkbp:notableFeature
|
Hans-Joachim Marseille
|
|
gptkbp:numberBuilt
|
approximately 200
|
|
gptkbp:productionLocation
|
gptkb:Germany
|
|
gptkbp:productionYears
|
1945-1947
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
600 km
|
|
gptkbp:relatedAircraft
|
gptkb:Bücker_Bü_133
gptkb:Bücker_Bü_181
|
|
gptkbp:retired
|
1950s
|
|
gptkbp:role
|
training aircraft
aerobatic training
|
|
gptkbp:services
|
4000 m
1945-1950s
|
|
gptkbp:setting
|
high-wing monoplane
|
|
gptkbp:speed
|
60 km/h
|
|
gptkbp:succeededBy
|
360° in 3 seconds
|
|
gptkbp:successor
|
gptkb:Bücker_Bü_133
|
|
gptkbp:supportRole
|
pilot training
|
|
gptkbp:type
|
single-engine aircraft
|
|
gptkbp:usedBy
|
gptkb:Luftwaffe
|
|
gptkbp:usedIn
|
aerobatic competitions
|
|
gptkbp:variant
|
gptkb:Bücker_Bü_182A
gptkb:Bücker_Bü_182B
|
|
gptkbp:weight
|
600 kg
|
|
gptkbp:wingspan
|
9.5 m
|