|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Convair_F-102_Delta_Dagger
gptkb:Douglas_F4_D_Skyray
gptkb:Mc_Donnell_F3_H_Demon
gptkb:North_American_F-100_Super_Sabre
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:General_Electric_Aircraft_Engine_Group
|
|
gptkbp:development
|
gptkb:J35_engine_family
1945-1948
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:engine
|
gptkb:General_Electric_J79
gptkb:Pratt_&_Whitney_J57
gptkb:General_Electric_J47
gptkb:Rolls-Royce_Avon
Brayton cycle
|
|
gptkbp:engine_configuration
|
single spool
|
|
gptkbp:engine_type
|
J35-GE-1
J35-GE-3
J35-GE-5
J35-GE-11
J35-GE-13
J35-GE-15
J35-GE-17
J35-GE-19
J35-GE-7
J35-GE-9
|
|
gptkbp:first_flight
|
1948
|
|
gptkbp:fuel_economy
|
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric J35
|
|
gptkbp:ignition_system
|
spark plug ignition
|
|
gptkbp:inspired_by
|
Whittle engine design
|
|
gptkbp:length
|
14 ft 6 in
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:notable_feature
|
high thrust-to-weight ratio
|
|
gptkbp:operational_range
|
0.8 to 1.2 Mach
|
|
gptkbp:operational_use
|
gptkb:United_States_Air_Force
gptkb:United_States_Navy
|
|
gptkbp:propulsion
|
3,000 lbf
|
|
gptkbp:retirement
|
1960s
|
|
gptkbp:service_entry
|
1950
|
|
gptkbp:successor
|
gptkb:General_Electric_J79
|
|
gptkbp:turbine_type
|
axial turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_F2_H_Banshee
gptkb:Lockheed_F-94_Starfire
|
|
gptkbp:weight
|
1,500 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_J47
|
|
gptkbp:bfsLayer
|
5
|