Pratt & Whitney Canada JT15D-5C turbofan
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Cessna_Citation_Ultra
|
| gptkbp:bypassRatio |
2.8:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
two-stage fan, axial-centrifugal compressor
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
27.6 in
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_Canada_JT15D
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada JT15D-5C turbofan
|
| gptkbp:introducedIn |
1994
|
| gptkbp:length |
61.4 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:thrust |
3045 lbf
|
| gptkbp:turbineType |
two-stage low-pressure, single-stage high-pressure
|
| gptkbp:type |
turbofan
|
| gptkbp:usedIn |
gptkb:Cessna_Citation_V_Ultra
gptkb:Cessna_Citation_Encore |
| gptkbp:weight |
476 lb
|
| gptkbp:bfsParent |
gptkb:Northrop_Grumman_X-47A
|
| gptkbp:bfsLayer |
7
|