|
gptkbp:instanceOf
|
gptkb:piston_engine
|
|
gptkbp:application
|
helicopters
fixed-wing aircraft
|
|
gptkbp:civilianDesignation
|
LTC1
|
|
gptkbp:configuration
|
single-spool axial-flow compressor
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
approximately 0.5 m
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:fuelType
|
gptkb:gasoline
|
|
gptkbp:introduced
|
1959
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:militaryDesignation
|
gptkb:T53
|
|
gptkbp:notableVariant
|
T53-L-11
T53-L-13
T53-L-703
|
|
gptkbp:numberBuilt
|
over 19,000
|
|
gptkbp:numberOfStages
|
5 axial, 1 centrifugal
|
|
gptkbp:powerOutput
|
up to 1,800 shp
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:Lycoming_T55
|
|
gptkbp:type
|
turboprop
turboshaft
|
|
gptkbp:usedIn
|
gptkb:Bell_205
gptkb:Kaman_HH-43_Huskie
gptkb:Bell_204
gptkb:Bell_212
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:weight
|
approximately 400 kg
|
|
gptkbp:bfsParent
|
gptkb:Bell_UH-1_Iroquois
gptkb:Grumman_OV-1_Mohawk
|
|
gptkbp:bfsLayer
|
6
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53
|