Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
can-type
|
| gptkbp:compressor_type |
axial
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine_configuration |
turbojet
|
| gptkbp:first_flight |
gptkb:1954
|
| gptkbp:fuel_type |
JP-4
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney J60
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:operational_range |
high subsonic to low supersonic
|
| gptkbp:propulsion |
5,000 lbf
|
| gptkbp:successor |
gptkb:Pratt_&_Whitney_J75
|
| gptkbp:turbine_type |
single spool
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_F2_H_Banshee
|
| gptkbp:weight |
2,500 lb
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_J75
|
| gptkbp:bfsLayer |
5
|