Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb: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
|
| 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_(Sikorsky)
gptkb:CH-53K_King_Stallion |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric T408
|