Pratt & Whitney J75-P-19W turbojet
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustorType |
annular
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
39 in
|
| gptkbp:firstRun |
1955
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney J75-P-19W turbojet
|
| gptkbp:length |
220 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:numberOfStages |
17
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
24,500 lbf
|
| gptkbp:type |
axial-flow turbojet
|
| gptkbp:usedInAircraft |
gptkb:Lockheed_U-2
gptkb:Convair_F-106_Delta_Dart |
| gptkbp:weight |
5,875 lb
|
| gptkbp:bfsParent |
gptkb:F-105D
gptkb:F-105F gptkb:F-105G_Wild_Weasel gptkb:F-105B_Thunderchief gptkb:F-105D_Thunderchief gptkb:F-105F_Thunderchief gptkb:F-105G_Thunderchief |
| gptkbp:bfsLayer |
7
|