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gptkbp:instance_of
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gptkb:turbofan_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Cessna_Citation_II
gptkb:Beechcraft_1900
gptkb:Bombardier_Learjet_31
gptkb:Cessna_Citation_I
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|
gptkbp:application
|
gptkb:business_jet
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
axial-flow
|
|
gptkbp:diameter
|
approximately 2.5 ft
|
|
gptkbp:engine
|
bleed air start
JT15 family
|
|
gptkbp:engine_configuration
|
twin-spool
pylon-mounted
|
|
gptkbp:engine_type
|
JT15 D-1
JT15 D-10
JT15 D-11
JT15 D-12
JT15 D-13
JT15 D-14
JT15 D-15
JT15 D-16
JT15 D-17
JT15 D-18
JT15 D-19
JT15 D-20
JT15 D-21
JT15 D-22
JT15 D-23
JT15 D-24
JT15 D-25
JT15 D-26
JT15 D-27
JT15 D-28
JT15 D-29
JT15 D-30
JT15 D-4
JT15 D-5
JT15 D-6
JT15 D-7
JT15 D-8
JT15 D-9
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada JT15 D
|
|
gptkbp:length
|
approximately 4.5 ft
|
|
gptkbp:maintenance
|
3,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:produces
|
over 5,000 units
|
|
gptkbp:propulsion
|
3,000 to 3,500 lbf
6.0 lbf/lb
|
|
gptkbp:service_ceiling
|
41,000 ft
|
|
gptkbp:turbine_type
|
two-stage turbine
|
|
gptkbp:weight
|
approximately 500 lb
|
|
gptkbp:bfsParent
|
gptkb:Gulfstream_II
gptkb:Aero_AT-4
|
|
gptkbp:bfsLayer
|
6
|