Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
twin-spool
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.5 m
|
| gptkbp:family |
gptkb:LHTEC_CTS800
|
| gptkbp:firstFlight |
1995
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
1.1 m
|
| gptkbp:manufacturer |
gptkb:LHTEC
|
| gptkbp:powerOutput |
1,362 shp
|
| gptkbp:usedIn |
gptkb:HAL_Light_Utility_Helicopter
|
| gptkbp:weight |
200 kg
|
| gptkbp:bfsParent |
gptkb:AW159_Wildcat_AH1
gptkb:AgustaWestland_AW159_Wildcat gptkb:AW159 gptkb:Wildcat_HMA2_helicopter |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
LHTEC CTS800-4N turboshaft
|