Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
military and civil helicopters
|
| gptkbp:certification |
gptkb:EASA
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_Kingdom |
| gptkbp:developedBy |
military helicopters
|
| gptkbp:diameter |
0.48 m
|
| gptkbp:firstFlight |
1990
|
| gptkbp:fuelType |
gptkb:Jet-A1
|
| gptkbp:length |
1.36 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Turbomeca |
| gptkbp:numberOfStages |
2 axial, 1 centrifugal
|
| gptkbp:powerOutput |
2100 to 2700 shp
|
| gptkbp:successor |
gptkb:Safran_Aneto
|
| gptkbp:type |
twin-spool turboshaft
|
| gptkbp:usedIn |
gptkb:NHIndustries_NH90
gptkb:AgustaWestland_AW101 Apache AH-64E Guardian (UK variant) |
| gptkbp:weight |
276 kg
|
| gptkbp:bfsParent |
gptkb:Avio_S.p.A._(aviation_business)
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca RTM322
|