Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:cooling_system |
air-cooled
fan air cooling |
| gptkbp:design |
high bypass ratio
|
| gptkbp:diameter |
3 ft 9 in
|
| gptkbp:first_flight |
gptkb:1980s
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric GE38-1 B
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:operational_use |
gptkb:military_logistics
|
| gptkbp:propulsion |
38,000 lbf
|
| gptkbp:turbine_type |
high-pressure turbine
|
| gptkbp:weight |
3,000 lb
|
| gptkbp:bfsParent |
gptkb:CH-53_K_King_Stallion
|
| gptkbp:bfsLayer |
5
|