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.

All labels observed (1)

Label Occurrences
Astazou II canonical 2

How this entity was disambiguated

Statements (26)

Predicate Object
instanceOf turboprop engine ⓘ
turboshaft engine ⓘ
application light aircraft ⓘ
light helicopters ⓘ
configuration free-turbine ⓘ
countryOfOrigin France ⓘ
developedBy Turbomeca ⓘ
era Cold War aviation technology ⓘ
familySuccessor Astazou XII ⓘ
Astazou XIV ⓘ
fuelType kerosene ⓘ
intendedFor turboprop applications ⓘ
turboshaft applications ⓘ
manufacturer Turbomeca ⓘ
marketRole early production variant of Astazou family ⓘ
notableCharacteristic widely used early variant of Turbomeca Astazou ⓘ
partOfEngineFamily Turbomeca Astazou ⓘ
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 ⓘ

How these facts were elicited

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.

Turbomeca Astazou → notableVariant → Astazou II ⓘ
Astazou III → predecessor → Astazou II ⓘ