Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:manual
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine |
gptkb:J57_engine
air start |
| gptkbp:engine_configuration |
turbojet
|
| gptkbp:first_flight |
1950
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
J65 turbojet engine
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:operational_range |
high altitude
|
| gptkbp:power_output |
3,700 to 5,000 lbf
|
| gptkbp:propulsion |
5,000 lbf
|
| gptkbp:retirement_year |
1970s
|
| gptkbp:service_entry |
1951
|
| gptkbp:status |
retired
|
| gptkbp:turbine_type |
single spool
|
| gptkbp:used_in |
gptkb:Mc_Donnell_F2_H_Banshee
|
| gptkbp:variant |
J65-W-16
|
| gptkbp:weight |
1,800 lb
|
| gptkbp:bfsParent |
gptkb:B-57_Canberra
gptkb:Hughes_X-13 |
| gptkbp:bfsLayer |
6
|