Pratt & Whitney J52-P-8 A

URI: https://gptkb.org/entity/Pratt_%26_Whitney_J52-P-8_A
GPTKB entity
Statements (89)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:aircraft_operated gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
gptkbp:application gptkb:military_aircraft
gptkbp:average_temperature 1,200 ° F
gptkbp:combustor_type annular
gptkbp:compressor_type axial
gptkbp:control_system hydromechanical
gptkbp:cooling_system air-cooled
gptkbp:design_date gptkb:1952
gptkbp:diameter 3 ft 4 in
gptkbp:emissions_standard Stage 3
gptkbp:engine gptkb:military_aircraft
gptkb:fighter_aircraft
modular design
widely available
Brayton cycle
over 10,000 units
air start
produced in large numbers
J52
afterburner option
major overhaul every 1,500 hours
J52 family
gptkbp:engine_configuration gptkb:Pratt_&_Whitney
turbojet
designed for carrier operations
single engine
single spool
detailed specifications available.
J52-8 A
gptkbp:engine_power high reliability
3,000 hours
high thrust-to-weight ratio
gptkbp:engine_type afterburning turbojet
multiple variants available
J52
J52-P-8 B
J52-P-8 A-16
J52-P-8 A-18
J52-P-8 A-20
J52-P-8 A-22
J52-P-8 A-24
J52-P-8 A-26
J52-P-8 A-28
J52-P-8 A-30
J52-P-8 A-32
J52-P-8 A-34
J52-P-8 A-36
J52-P-8 A-38
J52-P-8 A-40
J52-P-8 A-42
J52-P-8 A-44
J52-P-8 A-46
J52-P-8 A-48
J52-P-8 A-50
gptkbp:exhaust_system gptkb:straight
gptkbp:first_flight gptkb:1954
gptkb:1956
gptkbp:fuel_economy 0.85 lb/lbf/hr
0.8 lb/hp/hr
gptkbp:fuel_type JP-4
hydromechanical fuel control
https://www.w3.org/2000/01/rdf-schema#label Pratt & Whitney J52-P-8 A
gptkbp:ignition_system gptkb:spark_plug
gptkbp:is_tested_for static test
gptkbp:length 12 ft 6 in
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:max_speed Mach 0.9
gptkbp:noise_level 85 d B
gptkbp:notable_users gptkb:United_States_Navy
gptkbp:number_of_stages 8
gptkbp:operational_history used in various naval aircraft
used by US Navy
gptkbp:operational_range 1,000 miles
gptkbp:propulsion 1.79
5,000 lbf
5,000 lbf at sea level
gptkbp:related_aircraft gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
A-4 Skyhawk family
gptkbp:replaced_by Pratt & Whitney F404
gptkbp:service_ceiling 45,000 ft
40,000 ft
gptkbp:successor Pratt & Whitney J52-P-8 B
gptkbp:turbine_type single spool
gptkbp:type gptkb:turbofan_engine
gptkbp:used_in gptkb:Douglas_A-4_Skyhawk
gptkbp:variant J52-P-8 B
gptkbp:weight 2,800 lb