AgustaWestland AW129 Mangusta
GPTKB entity
Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:armament |
gptkb:Hydra_70_rockets
gptkb:Stinger_missiles gptkb:TOW_anti-tank_missiles gptkb:Spike-ER_missiles 20 mm cannon |
| gptkbp:crew |
2
|
| gptkbp:engine |
gptkb:Rolls-Royce_Gem_2
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:exportedTo |
Turkey (as T129 ATAK, modified version)
|
| gptkbp:firstFlight |
1983
|
| gptkbp:height |
3.35 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
AgustaWestland AW129 Mangusta
|
| gptkbp:introduced |
1990
|
| gptkbp:length |
12.28 m
|
| gptkbp:mainRotorDiameter |
11.90 m
|
| gptkbp:manufacturer |
gptkb:AgustaWestland
gptkb:Agusta |
| gptkbp:maximumSpeed |
278 km/h
|
| gptkbp:maxTakeoffWeight |
5100 kg
|
| gptkbp:nickname |
gptkb:Mangusta
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:origin |
gptkb:Italy
|
| gptkbp:primaryUser |
gptkb:Italian_Army
|
| gptkbp:range |
510 km
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:status |
in service
|
| gptkbp:successor |
AW249
|
| gptkbp:bfsParent |
gptkb:Comando_Aviazione_dell'Esercito
|
| gptkbp:bfsLayer |
7
|