Turbomeca Turmo IV turboshaft
GPTKB entity
Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:configuration |
axial-centrifugal flow
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:firstFlight |
1957
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Turmo IV turboshaft
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:powerOutput |
1,200 shp
|
| gptkbp:usedInAircraft |
gptkb:Aérospatiale_SA_321_Super_Frelon
gptkb:Aérospatiale_SA_330_Puma gptkb:Sud_Aviation_SE_3200_Frelon |
| gptkbp:bfsParent |
gptkb:IAR_330_Puma_SOCAT
|
| gptkbp:bfsLayer |
6
|