3 Pratt & Whitney Canada PW535 E
GPTKB entity
Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:business_jet
|
| gptkbp:compressor_type |
axial
|
| gptkbp:configuration |
dual-spool
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
1,000 mm
1,200 mm |
| gptkbp:engine |
Brayton cycle
|
| gptkbp:first_flight |
gptkb:2001
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
3 Pratt & Whitney Canada PW535 E
|
| gptkbp:length |
1,500 mm
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:noise_level |
gptkb:Stage_4
|
| gptkbp:propulsion |
3,000 lbf
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:weight |
300 kg
|
| gptkbp:bfsParent |
gptkb:Dassault_Falcon_8_X
|
| gptkbp:bfsLayer |
5
|