Pratt & Whitney Canada PW150A
GPTKB entity
Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Bombardier_Dash_8_Q400
|
| gptkbp:certification |
gptkb:Transport_Canada
|
| gptkbp:combustion |
annular combustor
|
| gptkbp:compressionRatio |
two-axial compressor
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
0.6 m
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_Canada_PW100
|
| gptkbp:firstFlight |
1994
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasTower |
three-stage power turbine
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW150A
|
| gptkbp:length |
2.5 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:marketedAs |
regional airliners
|
| gptkbp:notableFeature |
low noise
high efficiency FADEC control |
| gptkbp:powerOutput |
5000 shp
|
| gptkbp:type |
turboprop
|
| gptkbp:weight |
750 kg
|
| gptkbp:bfsParent |
gptkb:Bombardier_DHC-8-Q400
gptkb:DHC-8-400 gptkb:De_Havilland_Canada_Dash_8-Q400 gptkb:Bombardier_Dash_8_Q400 gptkb:Dash_8_Q400 gptkb:Dash_8-Q400 gptkb:de_Havilland_Canada_DHC-8-400_(Q400) gptkb:Bombardier_Q400 |
| gptkbp:bfsLayer |
6
|