Astazou II
E1041247
The Astazou II is an early, widely used variant of Turbomeca’s Astazou turboshaft/turboprop engine, powering various light helicopters and aircraft in the 1960s and 1970s.
Statements (26)
| Predicate | Object |
|---|---|
| instanceOf |
turboprop engine
ⓘ
turboshaft engine ⓘ |
| application |
light aircraft
ⓘ
light helicopters ⓘ |
| configuration | free-turbine ⓘ |
| countryOfOrigin | France ⓘ |
| developedBy | Turbomeca NERFINISHED ⓘ |
| era | Cold War aviation technology ⓘ |
| familySuccessor |
Astazou XII
NERFINISHED
ⓘ
Astazou XIV NERFINISHED ⓘ |
| fuelType | kerosene ⓘ |
| intendedFor |
turboprop applications
ⓘ
turboshaft applications ⓘ |
| manufacturer | Turbomeca NERFINISHED ⓘ |
| marketRole | early production variant of Astazou family ⓘ |
| notableCharacteristic | widely used early variant of Turbomeca Astazou ⓘ |
| partOfEngineFamily | Turbomeca Astazou NERFINISHED ⓘ |
| powerClass | low-power turboshaft ⓘ |
| serviceEntryDecade | 1960s ⓘ |
| technologyType | gas turbine engine ⓘ |
| typicalUseCase |
civil utility helicopters
ⓘ
military light helicopters ⓘ |
| usedAs |
aircraft engine
ⓘ
helicopter engine ⓘ |
| usedInPeriod |
1960s
ⓘ
1970s ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.