Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:light_aircraft
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compression_ratio |
16:1
|
| gptkbp:configuration |
inline 4-cylinder
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
liquid-cooled
|
| gptkbp:diameter |
600 mm
|
| gptkbp:displacement |
4.2 L
|
| gptkbp:engine |
GE H75
|
| gptkbp:engine_type |
turbocharged
|
| gptkbp:first_introduced |
gptkb:2010
|
| gptkbp:fuel_economy |
0.4 lb/hp/hr
|
| gptkbp:fuel_type |
Jet-A or Jet-A1
|
| https://www.w3.org/2000/01/rdf-schema#label |
GE Aviation H80
|
| gptkbp:length |
1,200 mm
|
| gptkbp:manufacturer |
gptkb:GE_Aviation
|
| gptkbp:market_segment |
general aviation
|
| gptkbp:notable_feature |
high power-to-weight ratio
|
| gptkbp:power_output |
400 to 800 hp
|
| gptkbp:propeller |
variable pitch
|
| gptkbp:weight |
approximately 200 kg
|
| gptkbp:bfsParent |
gptkb:L-410_NG
|
| gptkbp:bfsLayer |
7
|