J85 Engine

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:military_aircraft
gptkbp:certification military certification
gptkbp:combustor_type annular
gptkbp:compressor_type axial
gptkbp:control_system hydromechanical
gptkbp:cooling_system air-cooled
gptkbp:diameter 2.5 ft
gptkbp:engine gptkb:J79_Engine
gptkb:advanced_technology
gptkb:J60_Engine
gptkb:J75_Engine
gptkb:J85-13_Engine
ongoing development
air start
continuous innovation
significant legacy
gptkbp:engine_configuration pylon-mounted
upgradeable
gptkbp:engine_history long history
gptkbp:engine_market global market
gptkbp:engine_nozzle variable area
gptkbp:engine_power high performance
high reliability
high efficiency
long lifecycle
gptkbp:engine_type multiple variants
gptkbp:first_flight gptkb:1956
gptkbp:fuel_economy 0.85 lb/lbf/hr
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label J85 Engine
gptkbp:impact significant impact on aviation
gptkbp:is_tested_for extensive testing
gptkbp:length 3.8 ft
gptkbp:maintenance modular design
gptkbp:manufacturer gptkb:General_Electric
gptkbp:max_speed Mach 0.9
gptkbp:noise_level low noise
gptkbp:number_of_engines 1 or 2
gptkbp:operational_range 1,000 miles
gptkbp:propulsion 5:1
3,000 lbf
gptkbp:service_ceiling 50,000 ft
gptkbp:turbine_type single spool
gptkbp:type turbojet
gptkbp:used_in gptkb:Northrop_F-5
gptkbp:variant J85-GE-13
J85-GE-17
J85-GE-21
J85-GE-5
gptkbp:weight 600 lb
gptkbp:bfsParent gptkb:General_Electric's_aviation_division
gptkbp:bfsLayer 5