Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
twin-spool
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.48 m
|
| gptkbp:family |
gptkb:LHTEC_CTS800
|
| gptkbp:firstFlight |
1995
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
LHTEC CTS800-4A turboshaft
|
| gptkbp:length |
1.1 m
|
| gptkbp:manufacturer |
gptkb:LHTEC
|
| gptkbp:powerOutput |
1372 shp
|
| gptkbp:relatedTo |
gptkb:Rolls-Royce
gptkb:Honeywell_Aerospace |
| gptkbp:usedIn |
gptkb:AgustaWestland_AW159_Wildcat
gptkb:T129_ATAK |
| gptkbp:weight |
200 kg
|
| gptkbp:bfsParent |
gptkb:T-129_ATAK_helicopter
gptkb:T129_ATAK |
| gptkbp:bfsLayer |
6
|