Venturi VFE-31

GPTKB entity

Statements (56)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:aircraft_operated gptkb:light_aircraft
varies by owner
ultralight aircraft
gptkbp:aspect_ratio 7:1
gptkbp:cockpit enclosed
gptkbp:control_stick center-mounted
gptkbp:control_surfaces elevators and ailerons
gptkbp:control_system fly-by-wire
gptkbp:country_of_origin gptkb:France
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