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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:Harrier_Jump_Jet
gptkb:Jim_Mc_Donnell
gptkb:Research_Institute
experimental
fly-by-wire
high maneuverability
private funding
aerodynamics research
advanced control systems
canard configuration
variable-sweep wing
1,134 kg
1972-1975
high stability in flight
innovative design principles
experimental VTOL aircraft
canard and tail
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gptkbp:cockpit
|
enclosed cockpit
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gptkbp:controls
|
fly-by-wire system
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|
gptkbp:date
|
gptkb:1965
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gptkbp:design
|
gptkb:V/_STOL
gptkb:Jim_Mc_Donnell
VTOL research
J. A. M. (Jim) Mc Donnell
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|
gptkbp:developer
|
1960s to 1970s
Vari Viggen Corporation
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gptkbp:engine
|
200 hp
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gptkbp:engine_type
|
piston engine
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|
gptkbp:features
|
variable geometry wings
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gptkbp:first_flight
|
gptkb:1972
gptkb:California
2 hours
conducted
1972-06-01
extensive testing conducted.
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gptkbp:fuel_capacity
|
200 L
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gptkbp:height
|
2.74 m
|
|
gptkbp:historical_context
|
post-Vietnam War era
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Vari Viggen
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|
gptkbp:influenced_by
|
NASA research
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|
gptkbp:inspiration
|
NASA's VTOL projects
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|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
influenced future VTOL designs
|
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gptkbp:length
|
8.23 m
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gptkbp:manufacturer
|
Vari Viggen Corporation
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|
gptkbp:max_speed
|
240 km/h
|
|
gptkbp:max_takeoff_weight
|
1,134 kg
|
|
gptkbp:notable_features
|
vertical takeoff and landing
|
|
gptkbp:number_built
|
gptkb:musical
|
|
gptkbp:operational_area
|
gptkb:none
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:propulsion
|
single engine
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
research and development
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:significance
|
VTOL technology advancement
|
|
gptkbp:speed
|
200 km/h
|
|
gptkbp:status
|
retired
|
|
gptkbp:surface
|
canard
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:wingspan
|
9.14 m
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gptkbp:bfsParent
|
gptkb:Vari_Eze
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gptkbp:bfsLayer
|
6
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