Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:civilianDesignation |
gptkb:JT4A
|
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
39 in
|
| gptkbp:firstFlight |
1955
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney J75
|
| gptkbp:length |
191 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:militaryDesignation |
gptkb:J75
|
| gptkbp:notableFeature |
high thrust for its era
|
| gptkbp:numberOfStages |
17
3 |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Pratt_&_Whitney_JT3D
|
| gptkbp:thrust |
17,000 lbf
24,500 lbf |
| gptkbp:usedFor |
power generation (industrial version)
marine propulsion (industrial version) |
| gptkbp:usedInAircraft |
gptkb:Convair_B-58_Hustler
gptkb:Republic_F-105_Thunderchief gptkb:Lockheed_U-2 gptkb:North_American_XB-70_Valkyrie_(prototype) gptkb:Convair_F-106_Delta_Dart gptkb:Martin_RB-57F_Canberra |
| gptkbp:weight |
4,800 lb
|
| gptkbp:bfsParent |
gptkb:IHI_J75_engine
gptkb:F-105_Thunderchief |
| gptkbp:bfsLayer |
6
|