|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Thunderjet
|
|
gptkbp:aircraft_operated
|
gptkb:F-111_Aardvark
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:controls
|
gptkb:football_match
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:engine
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
Stage 3
variable geometry
|
|
gptkbp:engine
|
Brayton cycle
twin-spool
high bypass ratio
pylon-mounted
|
|
gptkbp:engine_type
|
2
8
|
|
gptkbp:fan_art
|
single stage fan
|
|
gptkbp:first_flight
|
gptkb:1954
|
|
gptkbp:fuel_capacity
|
high
1,000 gallons
3.81 m
1,360 kg
0.78 lb/hp/hr
1.02 m
|
|
gptkbp:fuel_type
|
JP-4
axial flow
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
P& W J48
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:introduced
|
gptkb:1954
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 2.2
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:notable_users
|
gptkb:aircraft
gptkb:battle
|
|
gptkbp:operational_history
|
gptkb:Vietnam_War
|
|
gptkbp:operational_range
|
long range
|
|
gptkbp:power_output
|
15,000 to 20,000 lbf
|
|
gptkbp:propulsion
|
gptkb:battle
20,000 lbf
88 k N
|
|
gptkbp:replaced_by
|
gptkb:F119
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:successor
|
gptkb:P&_W_J52
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
|
gptkbp:weight
|
3,000 lb
|