gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
|
gptkb:light_aircraft
varies by owner
ultralight aircraft
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gptkbp:aspect_ratio
|
7:1
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gptkbp:cockpit
|
enclosed
|
gptkbp:control_stick
|
center-mounted
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gptkbp:control_surfaces
|
elevators and ailerons
|
gptkbp:control_system
|
fly-by-wire
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gptkbp:country_of_origin
|
gptkb:France
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gptkbp:cruise_speed
|
150 km/h
|
gptkbp:design
|
Jean-Marie Lemaire
Venturi design team
|
gptkbp:design_date
|
gptkb:1989
|
gptkbp:design_philosophy
|
aerodynamic efficiency
|
gptkbp:design_purpose
|
performance and efficiency
|
gptkbp:engine
|
Rotax 912
|
gptkbp:engine_type
|
four-stroke engine
|
gptkbp:financial_stability
|
good stability characteristics
|
gptkbp:first_flight
|
gptkb:1990
|
gptkbp:first_introduced
|
gptkb:1990
|
gptkbp:flaps
|
slotted flaps
|
gptkbp:fuel_capacity
|
100 liters
|
gptkbp:fuselage_material
|
monocoque
composite
|
gptkbp:has_authority_over
|
high control authority
|
https://www.w3.org/2000/01/rdf-schema#label
|
Venturi VFE-31
|
gptkbp:inspiration
|
Formula 1 racing technology
|
gptkbp:landing_distance
|
65 km/h
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
8.0 m
|
gptkbp:manufacturer
|
Venturi Aircraft
|
gptkbp:market_segment
|
recreational aviation
|
gptkbp:marketed_as
|
enthusiasts and pilots
VFE-31
|
gptkbp:max_speed
|
200 km/h
|
gptkbp:max_takeoff_weight
|
600 kg
|
gptkbp:notable_feature
|
low drag design
|
gptkbp:number_built
|
limited production
|
gptkbp:passenger_capacity
|
2
|
gptkbp:production_status
|
out of production
|
gptkbp:propeller
|
variable pitch propeller
|
gptkbp:range
|
800 km
|
gptkbp:role
|
gptkb:light_aircraft
|
gptkbp:safety_features
|
parachute recovery system
|
gptkbp:stall_speed
|
55 km/h
|
gptkbp:tail_type
|
T-tail
|
gptkbp:takeoff_distance
|
200 m
|
gptkbp:type
|
gptkb:aircraft
|
gptkbp:weight
|
300 kg
|
gptkbp:wing_area
|
15 m²
|
gptkbp:wing_configuration
|
high-wing
20 kg/m²
|
gptkbp:wingspan
|
10.5 m
|
gptkbp:bfsParent
|
gptkb:Venturi_Racing
|
gptkbp:bfsLayer
|
5
|