|
gptkbp:instance_of
|
gptkb:military_aircraft
|
|
gptkbp:aircraft_configuration
|
tailless delta wing
|
|
gptkbp:aircraft_type
|
gptkb:aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modernized for training purposes
|
|
gptkbp:cockpit
|
glass cockpit
dual control
|
|
gptkbp:communication_system
|
secure radio
|
|
gptkbp:crew
|
2
pilot and weapons systems officer
|
|
gptkbp:decommissioned
|
gptkb:1997
|
|
gptkbp:design
|
vertical takeoff and landing
|
|
gptkbp:engine_type
|
gptkb:Rolls-Royce_Pegasus
|
|
gptkbp:first_flight
|
gptkb:1970
gptkb:1997
|
|
gptkbp:fuel_capacity
|
2,500 liters
|
|
gptkbp:fuselage_material
|
composite materials
|
|
gptkbp:has_radius
|
1,000 m
|
|
gptkbp:height
|
3.76 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Harrier T.4 S
|
|
gptkbp:introduced
|
gptkb:1970
|
|
gptkbp:landing_distance
|
300 m
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:length
|
14.63 m
|
|
gptkbp:manufacturer
|
gptkb:British_Aerospace
|
|
gptkbp:max_speed
|
1,200 km/h
|
|
gptkbp:max_takeoff_weight
|
6,000 kg
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:number_built
|
gptkb:30
|
|
gptkbp:operational_history
|
used in training roles
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:primary_user
|
gptkb:Royal_Air_Force
|
|
gptkbp:propulsion
|
0.9
|
|
gptkbp:range
|
2,000 km
|
|
gptkbp:release_date
|
gptkb:1970
|
|
gptkbp:retired
|
gptkb:1997
|
|
gptkbp:role
|
gptkb:trainer_aircraft
advanced trainer
|
|
gptkbp:roll_rate
|
30°/s
|
|
gptkbp:seating_capacity
|
gptkb:Martin-Baker_Mk.10
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:service_entry
|
gptkb:1970
|
|
gptkbp:stall_speed
|
120 km/h
|
|
gptkbp:successor
|
gptkb:BAe_Hawk
|
|
gptkbp:takeoff_distance
|
400 m
|
|
gptkbp:training
|
advanced jet training
|
|
gptkbp:used_by
|
gptkb:Royal_Air_Force
|
|
gptkbp:variant
|
gptkb:Harrier_Jump_Jet
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
9.12 m
|
|
gptkbp:bfsParent
|
gptkb:BAe_Harrier_II
|
|
gptkbp:bfsLayer
|
6
|