Turbomeca Astazou

E311266

The Turbomeca Astazou is a French-designed turboshaft and turboprop engine widely used in light helicopters and aircraft from the 1960s onward.

All labels observed (2)

Label Occurrences
Turbomeca Astazou canonical 1
Turbomeca Astazou turboprop 1

How this entity was disambiguated

Statements (48)

Predicate Object
instanceOf turboprop engine
turboshaft engine
application turboprop
turboshaft
compressorType axial-centrifugal
configuration single-shaft
countryOfOrigin France
designer Turbomeca
developedInDecade 1950s
enteredService early 1960s
firstRun 1957
fuelType kerosene
manufacturer Turbomeca
marketRole commuter aircraft powerplant
light helicopter powerplant
notableFeature axial-centrifugal compressor combination
compact size
modular design
notableVariant Astazou II
Astazou III
Astazou XIV
Astazou XVI
Astazou XX
powerOutputRange approximately 400 shp to 1000 shp
productionPeriod 1960s
1970s
1980s
successor Turbomeca Arriel
Turbomeca Arrius 2B1
surface form: Turbomeca Arrius
usedBy British Army
French Air Force
French Army
various civil operators
usedFor training aircraft
transport aircraft
utility helicopters
usedIn light aircraft
light helicopters
usedOnAircraft Aérospatiale Alouette II
Aérospatiale Alouette III
Aérospatiale SA 315 Lama
surface form: Aérospatiale SA 315B Lama

Gazelle helicopter
surface form: Aérospatiale SA 341 Gazelle

Aérospatiale SA 342 Gazelle
Aérospatiale SA 360 Dauphin
Aérospatiale N 262
surface form: Nord 262

Piaggio P.166
Potez 840
SOCATA TB 30 Epsilon

How these facts were elicited

Referenced by (2)

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

Gazelle helicopter engineModel Turbomeca Astazou
FMA IA 58 Pucará powerplant Turbomeca Astazou
this entity surface form: Turbomeca Astazou turboprop