Microturbo TRI 60-2 turbojet
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
gptkb:helicopter |
| gptkbp:combustionType |
annular
|
| gptkbp:compressionRatio |
centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:cycle |
single-shaft
|
| gptkbp:diameter |
0.33 m
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Microturbo TRI 60-2 turbojet
|
| gptkbp:length |
0.98 m
|
| gptkbp:manufacturer |
Microturbo
|
| gptkbp:numberOfStages |
1
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
3.7 kN
|
| gptkbp:usedIn |
Canadair CL-89
BAE Systems Phoenix Beechcraft MQM-107 Streaker Canadair CL-289 Nord Aviation CT20 |
| gptkbp:weight |
55 kg
|
| gptkbp:bfsParent |
gptkb:RBS-15_SSM
|
| gptkbp:bfsLayer |
6
|