Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Cessna_Citation_II
gptkb:Cessna_Citation_Bravo gptkb:Cessna_Citation_SII |
| gptkbp:bypassRatio |
2.8:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
two-stage fan, axial-centrifugal compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
20.8 in
|
| gptkbp:family |
Pratt & Whitney JT15D
|
| gptkbp:firstFlight |
1971
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney JT15D-5B
|
| gptkbp:length |
47.5 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:thrust |
3,045 lbf
|
| gptkbp:turbineType |
two-stage turbine
|
| gptkbp:weight |
430 lb
|
| gptkbp:bfsParent |
gptkb:Texan_T1_aircraft
|
| gptkbp:bfsLayer |
7
|