|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Convair_F-102_Delta_Dagger
gptkb:Douglas_A-4_Skyhawk
gptkb:Republic_F-105_Thunderchief
gptkb:Boeing_B-17_Flying_Fortress
gptkb:Vought_F-8_Crusader
gptkb:Northrop_F-5_Freedom_Fighter
gptkb:Lockheed_A-12
gptkb:Mc_Donnell_F-101_Voodoo
|
|
gptkbp:average_temperature
|
1,200 ° F
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compression_ratio
|
7.5:1
|
|
gptkbp:compressor_type
|
centrifugal compressor
|
|
gptkbp:control_system
|
hydromechanical control system
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:engine
|
gptkb:military_aircraft
Brayton cycle
|
|
gptkbp:engine_configuration
|
axial-flow
turbojet engine design
|
|
gptkbp:engine_type
|
J75-P-5
J75-P-19
J75-P-21
J75-P-23
J75-P-6
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_capacity
|
4.7 m
1,450 kg
1.02 m
|
|
gptkbp:fuel_economy
|
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney J75
|
|
gptkbp:introduced
|
gptkb:1955
|
|
gptkbp:length
|
15 ft 4 in
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:notable_feature
|
afterburner
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:propulsion
|
5.3:1
17,000 lbf
|
|
gptkbp:range
|
1,500 miles
|
|
gptkbp:replaced_by
|
gptkb:Pratt_&_Whitney_F119
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:speed
|
Mach 2.2
|
|
gptkbp:successor
|
gptkb:Pratt_&_Whitney_J60
|
|
gptkbp:turbine_type
|
single-stage turbine
|
|
gptkbp:turbojet
|
yes
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:F-16_Fighting_Falcon
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
gptkb:North_American_F-100_Super_Sabre
|
|
gptkbp:weight
|
3,200 lb
|
|
gptkbp:bfsParent
|
gptkb:U-2_R
|
|
gptkbp:bfsLayer
|
4
|