Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:J47_turbojet_engine
|
| gptkbp:aircraft_operated |
F2 H Banshee family
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine |
turbojet
|
| gptkbp:engine_type |
axial
single-stage |
| gptkbp:first_flight |
1948
|
| gptkbp:fuel_type |
gptkb:Jet_A
annular combustion chamber |
| https://www.w3.org/2000/01/rdf-schema#label |
J35 turbojet engine
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:operational_range |
1,000 miles
|
| gptkbp:propulsion |
5,000 lbf
|
| gptkbp:successor |
gptkb:J79_turbojet_engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_F2_H_Banshee
|
| gptkbp:weight |
2,500 lb
|