Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:business_jet
|
| gptkbp:certification |
CAEP/6
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
2.5 ft
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:first_flight |
gptkb:1996
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Williams FJ44-1 AP-21
|
| gptkbp:length |
4.5 ft
|
| gptkbp:manufacturer |
gptkb:Williams_International
|
| gptkbp:noise_level |
gptkb:Stage_4
|
| gptkbp:propulsion |
3,400 lbf
|
| gptkbp:turbine_type |
single spool
|
| gptkbp:weight |
400 lb
|
| gptkbp:bfsParent |
gptkb:Cessna_Citation_M2
gptkb:Cessna_525_B_Citation_Jet_M2 |
| gptkbp:bfsLayer |
7
|