Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:aircraft_type |
gptkb:transport_aircraft
|
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:design |
twin-spool
|
| gptkbp:diameter |
3.0 ft
|
| gptkbp:engine_configuration |
dual-engine
|
| gptkbp:first_flight |
gptkb:1961
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric TF39
|
| gptkbp:length |
12.5 ft
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:number_of_stages |
8 stages
|
| gptkbp:operational_use |
gptkb:United_States_Air_Force
|
| gptkbp:propulsion |
30,000 lbf
|
| gptkbp:replaced_by |
gptkb:General_Electric_F138
|
| gptkbp:turbine_type |
high-pressure turbine
|
| gptkbp:used_in |
gptkb:Lockheed_C-5_Galaxy
|
| gptkbp:weight |
4,500 lb
|
| gptkbp:bfsParent |
gptkb:C-5_Galaxy
|
| gptkbp:bfsLayer |
4
|