Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:airlines |
90 lb/s
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:developer |
gptkb:Rolls-Royce
|
| gptkbp:diameter |
1.1 m
|
| gptkbp:engineConfiguration |
dual-spool
|
| gptkbp:engineType |
2
3 |
| gptkbp:firstFlight |
1983
|
| gptkbp:fuel_capacity |
0.85 lb/hp/hr
|
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce F405
|
| gptkbp:is_used_in |
gptkb:McDonnell_Douglas_F/A-18_Hornet
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notable_feature |
F405-RR-400
|
| gptkbp:operational_status |
military aviation
|
| gptkbp:propulsion |
22,000 lbf
|
| gptkbp:related_engine |
Rolls-Royce F119
|
| gptkbp:type |
turbofan engine
|
| gptkbp:weight |
1,200 kg
|