Pratt & Whitney Canada JT15D-4
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Cessna_Citation_II
gptkb:Cessna_Citation_SII |
| gptkbp:bypassRatio |
2.47:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
axial-centrifugal
two-stage fan |
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
27.6 in
|
| gptkbp:family |
gptkb:JT15D
|
| gptkbp:firstFlight |
1971
|
| gptkbp:hasTower |
two-stage
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada JT15D-4
|
| gptkbp:introducedIn |
1971
|
| gptkbp:length |
61.4 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:thrust |
2,500 lbf
|
| gptkbp:weight |
1,040 lb
|
| gptkbp:bfsParent |
gptkb:Cessna_Citation_II
gptkb:Cessna_550 |
| gptkbp:bfsLayer |
6
|