|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
regional jets
|
|
gptkbp:average_temperature
|
1500 K
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:check_in_time
|
no
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compression_ratio
|
25:1
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
20,000 hours
|
|
gptkbp:diameter
|
0.9 m
1.2 m
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:A-series
A-family
A200-2
regional aircraft, business jets
|
|
gptkbp:engine_configuration
|
twin-spool
pylon-mounted
|
|
gptkbp:engine_power
|
high reliability
high thrust-to-weight ratio
|
|
gptkbp:engine_type
|
civil aviation engine
A200-1
A200-1, A200-2
|
|
gptkbp:exhaust_system
|
subsonic intake
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:fan_events
|
gptkb:1
|
|
gptkbp:first_flight
|
gptkb:1990
|
|
gptkbp:fuel_economy
|
0.5 kg/k N·h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
A200 engines
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:launch_window
|
electric starter
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
5000 hours
scheduled maintenance required.
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_range
|
2000 km
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:origin
|
gptkb:North_America
|
|
gptkbp:power_output
|
1500 k W
|
|
gptkbp:propulsion
|
6.67
2000 lbf
2200 lbf
|
|
gptkbp:service_ceiling
|
35,000 ft
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
turbofan
|
|
gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:water_requirement
|
0.4 kg/s
|
|
gptkbp:weight
|
250 kg
300 kg
|
|
gptkbp:bfsParent
|
gptkb:Continental_Motors
|
|
gptkbp:bfsLayer
|
7
|