Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:Light_Helicopter_Turbine_Engine_Company
|
| gptkbp:diameter |
0.48 m
|
| gptkbp:firstFlight |
1985
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
LHTEC T800
|
| gptkbp:length |
1.1 m
|
| gptkbp:manufacturer |
gptkb:LHTEC
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
1,361 shp
|
| gptkbp:primaryUser |
military helicopters
|
| gptkbp:relatedTo |
gptkb:Rolls-Royce_Turbomeca_RTM322
|
| gptkbp:status |
in production
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:AgustaWestland_AW159_Wildcat
gptkb:AgustaWestland_Super_Lynx Boeing Sikorsky RAH-66 Comanche |
| gptkbp:weight |
140 kg
|
| gptkbp:bfsParent |
gptkb:LHTEC_CTS800-4N
gptkb:Light_Helicopter_Turbine_Engine_Company |
| gptkbp:bfsLayer |
7
|