Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
electric aircraft
|
| gptkbp:aircraft |
high-wing
|
| gptkbp:batteryCapacity |
40 kWh
|
| gptkbp:category |
light aircraft
|
| gptkbp:climbRate |
3 m/s
|
| gptkbp:cockpit |
enclosed cockpit
|
| gptkbp:controls |
fly-by-wire
|
| gptkbp:crew |
2 hours
|
| gptkbp:debutYear |
2011
|
| gptkbp:design |
two-seat glider
|
| gptkbp:design_feature |
folding wings
|
| gptkbp:electrification |
electric motor
|
| gptkbp:environmental_impact |
low emissions
|
| gptkbp:firstFlight |
2011
|
| gptkbp:fuelType |
electric battery
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pipistrel Taurus Electro 2
|
| gptkbp:isATypeOf |
gptkb:EASA_CS-23
|
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:manufacturer |
Pipistrel
|
| gptkbp:market_segment |
general aviation
|
| gptkbp:marketedAs |
training aircraft
|
| gptkbp:maximum_speed |
200 km/h
|
| gptkbp:maxTakeoffWeight |
600 kg
|
| gptkbp:notable_feature |
advanced aerodynamics
lightweight construction user-friendly interface sustainable aviation high efficiency low noise levels easy handling quiet operation short takeoff and landing low operating costs modern avionics |
| gptkbp:origin |
gptkb:Slovenia
|
| gptkbp:passenger_traffic |
2
|
| gptkbp:propulsion |
variable pitch
|
| gptkbp:range |
300 km
|
| gptkbp:regulatoryCompliance |
EASA_regulations
FAA_regulations |
| gptkbp:safety_features |
parachute system
|
| gptkbp:service_ceiling |
3,000 m
|
| gptkbp:speed |
60 km/h
150 km/h |
| gptkbp:surface |
elevators
ailerons rudder |
| gptkbp:surrounding_area |
15 m²
|
| gptkbp:takeoffDistance |
150 m
200 m |
| gptkbp:userBase |
flying schools
private owners aeroclubs |
| gptkbp:weight |
300 kg
|
| gptkbp:wingspan |
15.5 m
|