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gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
biplane configuration
|
|
gptkbp:armament
|
none
|
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gptkbp:climbRate
|
3.5 m/s
|
|
gptkbp:cockpit
|
open cockpit
single-seat
|
|
gptkbp:constructionMaterial
|
gptkb:NACA_airfoil
wood and fabric
|
|
gptkbp:controls
|
elevator, ailerons, rudder
|
|
gptkbp:countryOfOrigin
|
gptkb:Netherlands
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
gptkb:Hendrik_Fokker
|
|
gptkbp:engine
|
Fokker_F.VII_engine
|
|
gptkbp:enginePower
|
200 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1928
|
|
gptkbp:fuelCapacity
|
150 liters
|
|
gptkbp:headlights
|
wood and fabric
conventional tail
|
|
gptkbp:height
|
2.60 m
|
|
gptkbp:historicalSignificance
|
used for pilot training
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fokker S.17
|
|
gptkbp:landingGear
|
fixed landing gear
|
|
gptkbp:length
|
8.20 m
|
|
gptkbp:manufacturer
|
gptkb:Fokker
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:predecessor
|
Fokker S.14
|
|
gptkbp:productionYears
|
1928-1935
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retirementYear
|
1935
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:services
|
1929
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:Fokker_S.11
|
|
gptkbp:type
|
biplane
|
|
gptkbp:usedBy
|
gptkb:Royal_Netherlands_Air_Force
|
|
gptkbp:variant
|
Fokker S.17A
Fokker_S.17B
|
|
gptkbp:wingArea
|
25 m²
|
|
gptkbp:wingspan
|
10.50 m
|