Statements (23)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:application |
gptkb:helicopter
|
gptkbp:combustorType |
annular
|
gptkbp:compressionStages |
5 axial, 1 centrifugal
|
gptkbp:countryOfOrigin |
gptkb:United_States
|
gptkbp:diameter |
approximately 28 inches
|
gptkbp:firstFlight |
2015 (on CH-53K prototype)
|
gptkbp:firstRun |
2011
|
gptkbp:fuelType |
gptkb:gasoline
|
https://www.w3.org/2000/01/rdf-schema#label |
General Electric T408
|
gptkbp:length |
approximately 67 inches
|
gptkbp:manufacturer |
gptkb:General_Electric
|
gptkbp:militaryDesignation |
gptkb:GE38-1B
|
gptkbp:numberOfAxles |
2
|
gptkbp:powerOutput |
7,500 shp
|
gptkbp:primaryUser |
gptkb:United_States_Marine_Corps
|
gptkbp:replacedBy |
gptkb:General_Electric_T64
|
gptkbp:status |
in production
|
gptkbp:type |
turboshaft
|
gptkbp:usedIn |
gptkb:Sikorsky_CH-53K_King_Stallion
|
gptkbp:weight |
approximately 1,200 lb
|
gptkbp:bfsParent |
gptkb:CH-53K_King_Stallion
|
gptkbp:bfsLayer |
6
|