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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:A-4_B_Skyhawk
|
|
gptkbp:aircraft_operated
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gptkb:horse_race
straight wing
subsonic jet
|
|
gptkbp:armament
|
various bombs and missiles
|
|
gptkbp:avionics
|
advanced training systems
|
|
gptkbp:brakes
|
gptkb:battle
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:color
|
various camouflage patterns
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
gptkb:1999
|
|
gptkbp:design
|
low-wing monoplane
training and light attack
|
|
gptkbp:engine
|
J65-W-16
|
|
gptkbp:exported_to
|
several countries
|
|
gptkbp:first_flight
|
gptkb:1960
2000s
|
|
gptkbp:flaps
|
slotted flaps
|
|
gptkbp:fuel_capacity
|
1,800 liters
|
|
gptkbp:height
|
4.57 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TA-4 B Skyhawk
|
|
gptkbp:introduced
|
gptkb:1961
|
|
gptkbp:is_used_by
|
gptkb:battle
|
|
gptkbp:landing_gear
|
retractable
tricycle gear
|
|
gptkbp:length
|
12.19 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:material
|
aluminum
|
|
gptkbp:max_speed
|
1,050 km/h
|
|
gptkbp:max_takeoff_weight
|
4,500 kg
5,400 kg
|
|
gptkbp:nickname
|
gptkb:Skyhawk
|
|
gptkbp:notable_battle
|
limited
|
|
gptkbp:notable_users
|
gptkb:battle
|
|
gptkbp:number_built
|
over 300
|
|
gptkbp:operational_range
|
1,200 km
|
|
gptkbp:range
|
2,000 km
|
|
gptkbp:replaced_by
|
gptkb:T-45_Goshawk
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
30°/s
|
|
gptkbp:seating_capacity
|
gptkb:Martin-Baker_Mk._5
|
|
gptkbp:service_ceiling
|
12,500 m
|
|
gptkbp:speed
|
110 knots
|
|
gptkbp:successor
|
gptkb:A-4_M_Skyhawk
|
|
gptkbp:surface
|
elevators and ailerons
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
pilot training
advanced jet training
|
|
gptkbp:variant
|
gptkb:A-4_Skyhawk
|
|
gptkbp:wing_area
|
27.87 m²
|
|
gptkbp:wingspan
|
8.38 m
|