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gptkbp:instance_of
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gptkb:military_aircraft
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|
gptkbp:aircraft_configuration
|
canard configuration
detailed specifications available.
|
|
gptkbp:aircraft_operated
|
1970s
yes
advanced aerodynamics
medium-sized aircraft
limited operational success
influenced future VTOL designs
complex systems integration
experimental VTOL aircraft
|
|
gptkbp:aircraft_trials
|
numerous flight trials
|
|
gptkbp:aircraft_type
|
gptkb:aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:challenges
|
stability in hover
|
|
gptkbp:cockpit
|
tandem cockpit
|
|
gptkbp:control_surfaces
|
elevons
|
|
gptkbp:control_system
|
fly-by-wire
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
LTV engineers
|
|
gptkbp:design_feature
|
tilting wings
|
|
gptkbp:design_purpose
|
gptkb:military_logistics
|
|
gptkbp:development
|
1960s
|
|
gptkbp:development_cost
|
high
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:Fort_Worth,_Texas
gptkb:1964
military evaluation
|
|
gptkbp:flight_style
|
VTOL and STOL
unique VTOL capabilities
|
|
gptkbp:fuel_capacity
|
1,500 lb
|
|
gptkbp:historical_significance
|
early VTOL development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
LTV XC-142
|
|
gptkbp:inspiration
|
military needs for vertical lift
|
|
gptkbp:is_tested_for
|
VTOL testing
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:LTV_Aerospace
|
|
gptkbp:max_speed
|
400 knots
|
|
gptkbp:notable_pilots
|
LTV test pilots
|
|
gptkbp:number_built
|
gptkb:5
|
|
gptkbp:operational_use
|
gptkb:none
|
|
gptkbp:project
|
XC-142
|
|
gptkbp:project_cancellation
|
1970s
|
|
gptkbp:propulsion
|
turbofan engines
|
|
gptkbp:range
|
1,000 miles
|
|
gptkbp:related_aircraft
|
LTV XC-142 A
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:status
|
retired
|
|
gptkbp:weight
|
6,000 lb
|
|
gptkbp:wingspan
|
14.63 m
|
|
gptkbp:bfsParent
|
gptkb:Ling-Temco-Vought
|
|
gptkbp:bfsLayer
|
6
|