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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:F-86_D
|
|
gptkbp:average_temperature
|
1,000 ° F
|
|
gptkbp:compression_ratio
|
5.5:1
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:developer
|
gptkb:J35_turbojet_engine
|
|
gptkbp:diameter
|
3 ft 3 in
|
|
gptkbp:emissions_standard
|
gptkb:mountain
|
|
gptkbp:engine
|
gptkb:J35
Brayton cycle
J100
J200
J300
J65
J120
J150
J85
J79
J57
J1000
J400
J500
J600
J700
J75
J800
J900
J93
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_capacity
|
0.8 lb/hp·h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
J47 turbojet engine
|
|
gptkbp:ignition_system
|
gptkb:park
|
|
gptkbp:length
|
14 ft 4 in
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:number_of_stages
|
gptkb:5
|
|
gptkbp:propulsion
|
5,000 lbf
|
|
gptkbp:retirement_year
|
1960s
|
|
gptkbp:services
|
1948
|
|
gptkbp:successor
|
gptkb:J79_turbojet_engine
|
|
gptkbp:supports
|
40 lb/s
|
|
gptkbp:used_in
|
gptkb:Douglas_A-4_Skyhawk
gptkb:Mc_Donnell_F2_H_Banshee
gptkb:Lockheed_F-94_Starfire
gptkb:North_American_F-86_Sabre
|
|
gptkbp:variant
|
J47-GE-27
J47-GE-17
J47-GE-25
J47-GE-13
J47-GE-19
|
|
gptkbp:weight
|
1,600 lb
|