Pratt & Whitney Canada PW615F
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Cessna_Citation_Mustang
|
| gptkbp:bypassRatio |
2.8:1
|
| gptkbp:certification |
gptkb:FAA
gptkb:Transport_Canada |
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
fan, booster, high-pressure centrifugal compressor
|
| gptkbp:configuration |
two-spool
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
18.36 in
|
| gptkbp:family |
gptkb:PW600_series
|
| gptkbp:firstFlight |
2002
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW615F
|
| gptkbp:intendedUse |
very light jets
|
| gptkbp:length |
44.1 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:status |
in production
|
| gptkbp:thrust |
1,460 lbf
|
| gptkbp:turbineType |
single-stage high-pressure, single-stage low-pressure
|
| gptkbp:weight |
295 lb
|
| gptkbp:bfsParent |
gptkb:Cessna_Citation_Mustang
|
| gptkbp:bfsLayer |
7
|