Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:Mitsubishi_MU-300_Diamond
gptkb:Cessna_Citation_I |
| gptkbp:bypassRatio |
2.3:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
two-stage fan, two axial stages, one centrifugal stage
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
19.6 in
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_Canada_JT15D
|
| gptkbp:firstFlight |
1967
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
61.4 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:thrust |
2,200 lbf
|
| gptkbp:turbineType |
two-stage axial
|
| gptkbp:weight |
395 lb
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_Canada_JT15D
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
JT15D-1
|