Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:capacity |
16 to 20 troops
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:crew |
2
|
| gptkbp:engine |
gptkb:Turbomeca_Turmo_IVC
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1974
|
| gptkbp:height |
4.97 meters
|
| gptkbp:improves |
gptkb:SA_330J
|
| gptkbp:introduced |
1974
|
| gptkbp:length |
18.15 meters
|
| gptkbp:mainRotorDiameter |
15 meters
|
| gptkbp:manufacturer |
gptkb:Aérospatiale
|
| gptkbp:maximumSpeed |
257 km/h
|
| gptkbp:maxTakeoffWeight |
7,400 kg
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:partOf |
Aérospatiale SA 330 Puma family
|
| gptkbp:powerplant |
2 × Turbomeca Turmo IVC turboshafts
|
| gptkbp:primaryUser |
gptkb:military_organization
|
| gptkbp:range |
580 km
|
| gptkbp:role |
transport helicopter
|
| gptkbp:serviceCeiling |
4,800 m
|
| gptkbp:bfsParent |
gptkb:Aérospatiale_Puma
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
SA 330L
|