|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:air_support
|
100 lb/s
|
|
gptkbp:average_temperature
|
1500 ° F
|
|
gptkbp:check_in_time
|
optional
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compression_ratio
|
6:1
|
|
gptkbp:control_system
|
hydraulic
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:Allison_J35
2000 hours
|
|
gptkbp:development
|
1945-1950
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
Stage 3
|
|
gptkbp:engine
|
gptkb:Allison_engines
gptkb:Allison_J33
Brayton cycle
|
|
gptkbp:engine_configuration
|
axial-flow
pylon-mounted
|
|
gptkbp:engine_type
|
gptkb:J35-A-1
gptkb:J35-A-3
gptkb:J35-A-5
single-spool
J35-A-15
J35-A-17
|
|
gptkbp:exhaust_system
|
gptkb:straight
|
|
gptkbp:first_flight
|
1950
|
|
gptkbp:fuel_capacity
|
3.81 m
544 kg
1.02 m
|
|
gptkbp:fuel_economy
|
high
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Allison J35
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Allison_Engine_Company
|
|
gptkbp:max_speed
|
Mach 0.9
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:notable_users
|
gptkb:United_States_Navy
|
|
gptkbp:number_of_stages
|
gptkb:5
|
|
gptkbp:operational_history
|
used in military aircraft
|
|
gptkbp:operational_use
|
gptkb:military_aircraft
|
|
gptkbp:propulsion
|
no
5000 lbf
4.17:1
|
|
gptkbp:retired
|
1960s
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Allison_J71
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_F2_H_Banshee
|
|
gptkbp:water_requirement
|
100 gal/hr
|
|
gptkbp:weight
|
1200 lb
|
|
gptkbp:bfsParent
|
gptkb:Allison_J33
|
|
gptkbp:bfsLayer
|
5
|