Properties (51)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbojet engine
|
| gptkbp:application |
helicopters
|
| gptkbp:built |
1950s
|
| gptkbp:controls |
manual control
|
| gptkbp:coolingSystem |
air-cooled
direct air cooling |
| gptkbp:diameter |
0.3 m
|
| gptkbp:displacement |
significant impact on helicopter design.
|
| gptkbp:emissionsStandard |
low emissions
|
| gptkbp:engine |
120 kg
0.3 m 1.2 m military helicopters influenced future designs innovative design features single engine early turbojet technology pod-mounted |
| gptkbp:engineConfiguration |
30 seconds
turbojet developed_in_France |
| gptkbp:engineType |
axial
single-stage turbojet engine air start compatible with various airframes Artouste IIB |
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuel_capacity |
high efficiency
0.5 kg/s |
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| gptkbp:hasArea |
certified for flight use
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Artouste II
|
| gptkbp:is_used_in |
gptkb:Aérospatiale_Alouette_III
gptkb:Aérospatiale_Alouette_II |
| gptkbp:length |
1.2 m
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:maximum_speed |
250 km/h
|
| gptkbp:noise_level |
85 dB
|
| gptkbp:operationalHistory |
part of aviation history
|
| gptkbp:operationalRange |
500 km
|
| gptkbp:performances |
high reliability
good performance 1500 hours |
| gptkbp:powerOutput |
370 kW
|
| gptkbp:propulsion |
500 lbf
|
| gptkbp:service_ceiling |
3000 m
|
| gptkbp:type |
turbojet
|
| gptkbp:updates |
various modifications available
|
| gptkbp:weight |
120 kg
|