LHTEC CTS800-4A turboshaft

GPTKB entity

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	0.48 m
gptkbp:family	gptkb:LHTEC_CTS800
gptkbp:firstFlight	1995
gptkbp:fuelType	gptkb:gasoline
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	7
https://www.w3.org/2000/01/rdf-schema#label	LHTEC CTS800-4A turboshaft