Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:diameter |
68 in
3.0 ft |
| gptkbp:elevation |
37,000 ft
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:engine_type |
turbofan
|
| gptkbp:first_flight |
gptkb:1965
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
JT3 D-3 A
|
| gptkbp:length |
12.5 ft
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:number_of_stages |
8
|
| gptkbp:propulsion |
18,500 lbf
|
| gptkbp:related_aircraft |
gptkb:DC-8_family
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_DC-8
|
| gptkbp:weight |
3,500 lb
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_JT3_D
|
| gptkbp:bfsLayer |
5
|