gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:T-33_Shooting_Star
gptkb:Lockheed_T-33_Shooting_Star
|
gptkbp:aircraft_operated
|
straight wing
114.5 kg/m²
|
gptkbp:allows
|
+6/-3 g
|
gptkbp:armament
|
gptkb:none
|
gptkbp:avionics
|
basic navigation and communication systems
|
gptkbp:climb_rate
|
15 m/s
|
gptkbp:cockpit
|
two-seat tandem
|
gptkbp:color
|
various military and civilian schemes
|
gptkbp:crew
|
2
|
gptkbp:design
|
low-wing monoplane
|
gptkbp:engine
|
gptkb:Allison_J33
|
gptkbp:engine_type
|
gptkb:engine
|
gptkbp:first_flight
|
1948
|
gptkbp:fuel_capacity
|
1,200 L
|
gptkbp:height
|
3.81 m
|
gptkbp:historical_significance
|
first jet trainer for the USAF
|
https://www.w3.org/2000/01/rdf-schema#label
|
T-33 D
|
gptkbp:introduced
|
1950
|
gptkbp:is_used_by
|
gptkb:aircraft
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
12.77 m
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
gptkbp:material
|
metal construction
|
gptkbp:max_speed
|
1,000 km/h
|
gptkbp:max_takeoff_weight
|
3,175 kg
|
gptkbp:military_technology
|
aerobatic performances
|
gptkbp:modifications
|
various upgrades over the years
|
gptkbp:nickname
|
T-Bird
|
gptkbp:notable_users
|
Canada, Japan, South Korea
|
gptkbp:number_built
|
6,500
|
gptkbp:propulsion
|
turbojet
0.3
|
gptkbp:range
|
2,000 km
|
gptkbp:retired
|
1990s
|
gptkbp:retirement_year
|
replacement by more advanced trainers
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:roll_rate
|
10°/s
|
gptkbp:service_ceiling
|
12,500 m
|
gptkbp:service_history
|
used in various air forces worldwide
|
gptkbp:services
|
1950s to 1990s
|
gptkbp:speed
|
110 km/h
|
gptkbp:status
|
some still in use by private owners.
|
gptkbp:successor
|
gptkb:T-38_Talon
|
gptkbp:tail_type
|
T-tail
|
gptkbp:training
|
pilot training
|
gptkbp:variant
|
gptkb:Lockheed_P-80_Shooting_Star
|
gptkbp:wing_area
|
27.87 m²
|
gptkbp:wingspan
|
11.43 m
|