Teledyne CAE J402-CA-100 turbojet
GPTKB entity
Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:surface-to-air_missile
|
| gptkbp:compressionRatio |
centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
single-shaft
|
| gptkbp:diameter |
13 in
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
JP-10
|
| https://www.w3.org/2000/01/rdf-schema#label |
Teledyne CAE J402-CA-100 turbojet
|
| gptkbp:length |
45 in
|
| gptkbp:manufacturer |
gptkb:Teledyne_CAE
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
640 lbf
|
| gptkbp:usedIn |
gptkb:AGM-86_ALCM
gptkb:BGM-109_Tomahawk |
| gptkbp:weight |
100 lb
|
| gptkbp:bfsParent |
gptkb:JASSM_missile
gptkb:JASSM |
| gptkbp:bfsLayer |
6
|