Statements (47)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine
|
| gptkbp:airlines |
40 kg/s
|
| gptkbp:application |
gptkb:Antonov_An-148
gptkb:Antonov_An-140 regional aircraft Yakovlev Yak-42 |
| gptkbp:climate |
up to 1,500 °C
|
| gptkbp:compressionRatio |
5.5:1
|
| gptkbp:controls |
FADEC
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
1.2 m
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissionsStandard |
ICAO_Chapter_4
|
| gptkbp:engine |
2
1,200 kg modular design 1,200 mm 3,500 mm high bypass ratio |
| gptkbp:engineConfiguration |
twin-engine
|
| gptkbp:engineType |
2
10 fuel efficiency high reliability environmentally friendly low noise levels low maintenance costs dual-spool |
| gptkbp:fanBase |
wide-chord fan
|
| gptkbp:firstFlight |
1990
|
| gptkbp:fuel_capacity |
0.5 kg/kN·h
1,600 kg/h |
| gptkbp:fuelType |
gptkb:Jet_A-1
annular combustor |
| gptkbp:hasArea |
ground testing
EASA_certified |
| https://www.w3.org/2000/01/rdf-schema#label |
D-436TP turbofan engine
|
| gptkbp:launchSite |
electric starter
|
| gptkbp:length |
3.5 m
|
| gptkbp:maintenance |
4,000 hours
|
| gptkbp:manufacturer |
Motor Sich
|
| gptkbp:noise_level |
Stage 3
|
| gptkbp:operationalRange |
up to 10,000 m
|
| gptkbp:propulsion |
16,000 lbf
13.33:1 |
| gptkbp:services |
20,000 hours
|
| gptkbp:weight |
1,200 kg
|