|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:air_support
|
1,000 lb/s
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
1,000 ° F
|
|
gptkbp:check_in_time
|
optional
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
hydromechanical
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:engine
|
gptkb:historical_significance
air start
post-WWII era
1950s technology
turbojet advancements
|
|
gptkbp:engine_configuration
|
available
conventional
inline
pylon-mounted
single engine
|
|
gptkbp:engine_heritage
|
Pratt & Whitney lineage
|
|
gptkbp:engine_legacy_aircraft
|
gptkb:F2_H_Banshee
|
|
gptkbp:engine_power
|
moderate
limited
decent
|
|
gptkbp:engine_replacement
|
gptkb:J79_turbojet
|
|
gptkbp:engine_technology_transfer
|
gptkb:military_aircraft
|
|
gptkbp:engine_type
|
turbojet
naval aircraft
J65-W-1
|
|
gptkbp:engine_usage
|
gptkb:military_aircraft
|
|
gptkbp:first_flight
|
1948
|
|
gptkbp:fuel_economy
|
low
0.85 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
J65 turbojet
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
|
gptkbp:impact
|
aeronautical engineering
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
not equipped
85 d B
|
|
gptkbp:operational_range
|
0 to 30,000 ft
|
|
gptkbp:propulsion
|
no
1.79
5,000 lbf
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:status
|
retired
|
|
gptkbp:turbine_type
|
single spool
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_F2_H_Banshee
|
|
gptkbp:weight
|
2,800 lb
|
|
gptkbp:bfsParent
|
gptkb:A-4_Skyhawk
|
|
gptkbp:bfsLayer
|
5
|