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gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:designated_as
|
military applications
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
single exhaust
|
|
gptkbp:engine
|
gptkb:helicopter
twin-spool
air start
flexible mount
air-start
1,400 shp
40,000 rpm
|
|
gptkbp:engine_type
|
gptkb:engine
single exhaust
free turbine
reduction gearbox
two-stage turbine
single-stage centrifugal compressor
T53-L-13
T53-L-703
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
20 in
300 lb
high
0.5 lb/hp/hr
40 in
14 in
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-25
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:operational_area
|
gptkb:aircraft
|
|
gptkbp:operational_range
|
up to 30,000 ft
|
|
gptkbp:power_output
|
1,400 shp
|
|
gptkbp:propulsion
|
4.67
4.67 hp/lb
|
|
gptkbp:torque
|
1,600 lb-ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:variant
|
T53-L-13
T53-L-703
|
|
gptkbp:weight
|
approximately 300 lb
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_T53-L-13
|
|
gptkbp:bfsLayer
|
6
|