Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
2.5 m
3 ft 4 in |
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:first_flight |
gptkb:1983
|
| gptkbp:fuel_economy |
0.8 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce F405-RR-401
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:propulsion |
22,000 lbf
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
| gptkbp:weight |
1,500 lb
|
| gptkbp:bfsParent |
gptkb:T-45_Goshawk
|
| gptkbp:bfsLayer |
4
|