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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
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biplane
light aircraft
aerobatic biplane
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gptkbp:built
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over 100
modern era
|
|
gptkbp:cockpit
|
open cockpit
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gptkbp:colors
|
customizable
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gptkbp:constructionMaterial
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aluminum
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gptkbp:covers
|
none
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gptkbp:crew
|
1
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gptkbp:design
|
gptkb:Curtis_Pitts
|
|
gptkbp:engine
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Lycoming IO-540
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gptkbp:firstFlight
|
1990
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gptkbp:fuel_capacity
|
150 liters
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gptkbp:headlights
|
conventional tail
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|
https://www.w3.org/2000/01/rdf-schema#label
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Pitts S-45
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gptkbp:is_used_in
|
aerobatic competitions
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gptkbp:landing_gear
|
tailwheel
fixed gear
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gptkbp:length
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7.62 m
|
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gptkbp:manufacturer
|
gptkb:Pitts_Special_Aircraft
|
|
gptkbp:maximum_speed
|
300 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,200 kg
|
|
gptkbp:notable_feature
|
high power-to-weight ratio
high agility
stability in flight
good climb rate
excellent visibility
responsive controls
quick roll response
|
|
gptkbp:notableOperations
|
aerobatic teams
|
|
gptkbp:performance
|
highly maneuverable
|
|
gptkbp:productionYears
|
1990
|
|
gptkbp:propulsion
|
variable pitch
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
aerobatic aircraft
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:speed
|
80 km/h
|
|
gptkbp:succeededBy
|
360°/s
|
|
gptkbp:surface
|
ailerons
elevator
rudder
|
|
gptkbp:surrounding_area
|
15.5 m²
|
|
gptkbp:type
|
biplane
|
|
gptkbp:weight
|
680 kg
|
|
gptkbp:wingspan
|
8.23 m
|