Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
engine
|
| gptkbp:application |
Eurocopter_EC175
|
| gptkbp:compressionRatio |
30:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:designedFor |
aircraft
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:emissionsStandard |
ICAO_Chapter_4
|
| gptkbp:firstFlight |
2010
|
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Makila engine
|
| gptkbp:length |
1.8 m
|
| gptkbp:maintenance |
3,500 hours
|
| gptkbp:manufacturer |
gptkb:Safran
|
| gptkbp:noise_level |
low noise
|
| gptkbp:numberOfStudents |
10
|
| gptkbp:powerOutput |
up to 1,000 kW
|
| gptkbp:propulsion |
up to 15,000 lbf
|
| gptkbp:type |
turbofan engine
|
| gptkbp:weight |
approximately 400 kg
|