Astazou XX
E1041248
The Astazou XX is an advanced, higher-powered variant of Turbomeca’s Astazou turboshaft engine series, used primarily in helicopters and light aircraft.
Statements (25)
| Predicate | Object |
|---|---|
| instanceOf |
gas turbine engine
ⓘ
turboshaft engine ⓘ |
| application |
fixed-wing aircraft propulsion
ⓘ
rotary-wing aircraft propulsion ⓘ |
| category |
aero engine
ⓘ
helicopter engine ⓘ light aircraft engine ⓘ |
| combustionType | continuous combustion ⓘ |
| configuration | free-turbine ⓘ |
| coolingMethod | air-cooled ⓘ |
| countryOfOrigin | France ⓘ |
| designedFor |
civil aviation
ⓘ
military aviation ⓘ |
| developedBy | Turbomeca engineering division NERFINISHED ⓘ |
| familyRole | advanced development of earlier Astazou models ⓘ |
| fuelType | aviation kerosene ⓘ |
| intendedUse | main propulsion engine ⓘ |
| manufacturer | Turbomeca NERFINISHED ⓘ |
| marketedAs | high-power variant of Astazou series ⓘ |
| notableFeature | higher power output than earlier Astazou variants ⓘ |
| partOfSeries | Astazou engine family NERFINISHED ⓘ |
| powerType | shaft power ⓘ |
| propulsionPrinciple | gas generator driving power turbine ⓘ |
| usedIn |
helicopters
ⓘ
light aircraft ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.