|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
high temperature
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:configuration
|
free turbine
|
|
gptkbp:control_system
|
electronic control
digital control system
|
|
gptkbp:cooling_system
|
gptkb:oil
air-cooled
air cooling
|
|
gptkbp:diameter
|
22 in
|
|
gptkbp:emissions_standard
|
EPA Tier 4
|
|
gptkbp:engine
|
air start
|
|
gptkbp:engine_configuration
|
pylon-mounted
twin-shaft
1000 shp
free turbine configuration
|
|
gptkbp:engine_power
|
5000 hours
1000 shp
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:exhaust_system
|
straight exhaust
|
|
gptkbp:first_flight
|
1960s
|
|
gptkbp:fuel_capacity
|
300 lb
22 in
48 in
dry sump
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:gasoline
gptkb:Jet_A
gptkb:full_authority_digital_engine_control_(FADEC)
dual fuel system
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TPE331-10 R
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:launch_platform
|
starter-generator
|
|
gptkbp:length
|
48 in
|
|
gptkbp:maintenance
|
2000 hours
|
|
gptkbp:manufacturer
|
gptkb:Honeywell
|
|
gptkbp:max_speed
|
40,000 rpm
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:power_output
|
1000 shp
|
|
gptkbp:propeller
|
4.5 ft
variable pitch
|
|
gptkbp:propulsion
|
3.33
3.33 hp/lb
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:turbine_type
|
single stage
|
|
gptkbp:weight
|
300 lb
|
|
gptkbp:bfsParent
|
gptkb:Honeywell_TPE331-10_GD
|
|
gptkbp:bfsLayer
|
5
|