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gptkbp:instanceOf
|
floatplane
|
|
gptkbp:aircraft
|
biplane
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:cockpit
|
open cockpit
forward cockpit
|
|
gptkbp:constructionMaterial
|
wood and fabric
|
|
gptkbp:controls
|
manual controls
elevator and rudder
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gptkbp:countryOfOrigin
|
gptkb:Germany
|
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gptkbp:crew
|
2
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|
gptkbp:design
|
1920s
high-wing configuration
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|
gptkbp:designedBy
|
gptkb:Hansa-Brandenburg
|
|
gptkbp:engine
|
gptkb:BMW_IIIa
|
|
gptkbp:engineType
|
inline engine
|
|
gptkbp:financial_aid
|
good stability
|
|
gptkbp:firstFlight
|
1925
|
|
gptkbp:firstGeneration
|
1926
|
|
gptkbp:fuelCapacity
|
300 L
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:historicalContext
|
interwar period aviation
|
|
gptkbp:historicalSignificance
|
used in early naval aviation
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hansa-Brandenburg W.33
|
|
gptkbp:influenced
|
later floatplanes
|
|
gptkbp:influencedBy
|
gptkb:Hansa-Brandenburg_W.29
|
|
gptkbp:landingGear
|
float
water landing
|
|
gptkbp:length
|
9.5 m
|
|
gptkbp:manufacturer
|
gptkb:Hansa-Brandenburg
|
|
gptkbp:maxSpeed
|
180 km/h
|
|
gptkbp:maxTakeoffWeight
|
1500 kg
|
|
gptkbp:notableFeature
|
none documented
|
|
gptkbp:numberBuilt
|
approximately 100
|
|
gptkbp:primaryUser
|
Reichsmarine
|
|
gptkbp:productionYears
|
1925-1927
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retirementYear
|
1930s
|
|
gptkbp:role
|
training aircraft
reconnaissance aircraft
|
|
gptkbp:service_ceiling
|
4000 m
|
|
gptkbp:services
|
4000 m
|
|
gptkbp:successor
|
Hansa-Brandenburg W.34
|
|
gptkbp:type
|
biplane
|
|
gptkbp:usedBy
|
gptkb:German_Navy
|
|
gptkbp:variant
|
W.33a
W.33b
|
|
gptkbp:wingArea
|
40 m²
|
|
gptkbp:wingspan
|
12.5 m
|