Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
8.6:1
|
| gptkbp:certification |
gptkb:EASA
gptkb:Russian_IAC |
| gptkbp:configuration |
two-shaft
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:Russia |
| gptkbp:developedBy |
gptkb:Snecma
gptkb:NPO_Saturn |
| gptkbp:enteredService |
2011
|
| gptkbp:firstFlight |
2008
|
| https://www.w3.org/2000/01/rdf-schema#label |
SaM146 engine
|
| gptkbp:intendedUse |
regional jets
|
| gptkbp:length |
2.47 m
|
| gptkbp:mainRotorDiameter |
1.22 m
|
| gptkbp:manufacturer |
gptkb:PowerJet
|
| gptkbp:marketedAs |
gptkb:PowerJet
|
| gptkbp:notableFeature |
modular design
low emissions FADEC controlled |
| gptkbp:numberOfStages |
1 (high pressure), 4 (low pressure)
3 (low pressure), 6 (high pressure) |
| gptkbp:thrust |
62 to 77 kN
|
| gptkbp:usedOn |
gptkb:Sukhoi_Superjet_100
|
| gptkbp:bfsParent |
gptkb:NPO_Saturn
|
| gptkbp:bfsLayer |
7
|